Aerosoft CRJ-700 Quick Reference Guide

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-1

02-May-2017

Rev #

Date

Author

Change

Version

001

21-Sept-2015

MK

Start of project

0.90

002

08-Jan-2016

DJ

Data check

0.91

003

27-Dec-2016

MK

Reformatting / completing

0.92

004

18-Apr-2017

MK

Final checks and corrections

1.00

005

02-May-2017

MK

Final formatting

1.00

On behalf of Authority

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TABLE OF CON TENTS

INTRODUCTION .................................................................................................................................................. 5

PROCEDURES ...................................................................................................................................................... 6

NORMAL TAKE-OFF ........................................................................................................................................ 6

ILS APPROACH ................................................................................................................................................ 7

NON-PRECISION-APPROACH........................................................................................................................... 8

VISUAL APPROACHES ..................................................................................................................................... 9

CIRCLING APPROACH .................................................................................................................................... 10

GO-AROUND ................................................................................................................................................ 11

TOUCH-AND-GO ........................................................................................................................................... 12

CHECKLISTS ...................................................................................................................................................... 13

PRIOR TO START ........................................................................................................................................... 13

SAFETY CHECK .......................................................................................................................................... 13

CABIN INSPECTION ................................................................................................................................... 13

EXTERNAL WALKAROUND ........................................................................................................................ 13

ORIGINATING CHECK ................................................................................................................................ 14

BEFORE START CHECK .............................................................................................................................. 15

CLEARED TO START CHECK ....................................................................................................................... 15

PRIOR TO TAKE-OFF...................................................................................................................................... 16

AFTER START CHECK ................................................................................................................................. 16

TAXI CHECK .............................................................................................................................................. 16

BEFORE TAKE-OFF CHECK ......................................................................................................................... 16

AFTER TAKE-OFF ........................................................................................................................................... 17

CLIMB CHECK ........................................................................................................................................... 17

PRIOR TO LANDING ...................................................................................................................................... 17

DESCENT CHECK ....................................................................................................................................... 17

APPROACH CHECK .................................................................................................................................... 17

BEFORE LANDING CHECK ......................................................................................................................... 17

GO-AROUND PROCEDURE ............................................................................................................................ 18

AFTER LANDING ........................................................................................................................................... 18

AFTER LANDING CHECK ............................................................................................................................ 18

SHUTDOWN CHECK .................................................................................................................................. 18

TERMINATING CHECK ............................................................................................................................... 19

LIMITATIONS .................................................................................................................................................... 20

STRUCTURAL WEIGHT LIMITATIONS ............................................................................................................. 20

OPERATING LIMITATIONS (ALTITUDE AND TERMPERATURE) ........................................................................ 20

OPERATION IN ICING CONDITIONS ............................................................................................................... 21

COWL ANTI-ICE SYSTEM ............................................................................................................................... 21

WING ANTI-ICE SYSTEM................................................................................................................................ 21

RUNWAY SLOPES .......................................................................................................................................... 21

TAILWIND CONDITIONS ................................................................................................................................ 21

MINIMUM FLIGHT CREW .............................................................................................................................. 21

MAXIMUM OCCUPANTS ............................................................................................................................... 21

CARGO ......................................................................................................................................................... 21

POWER PLANT .............................................................................................................................................. 21

ENGINES INDICATIONS ............................................................................................................................. 21

THRUST MANAGEMENT DATA ................................................................................................................. 22

ENGINE WARM-UP ................................................................................................................................... 23

CONTINUOUS ENGINE IGNITION .............................................................................................................. 24

STARTER CRANKING LIMITS ...................................................................................................................... 24

ENGINE RELIGHT ...................................................................................................................................... 25

FUEL ............................................................................................................................................................. 25

FUEL TEMPERATURE ................................................................................................................................ 26

FUEL CROSSFLOW .................................................................................................................................... 26

AUXILLIARY POWER UNIT, APU ..................................................................................................................... 26

APU BLEED AIR ......................................................................................................................................... 27

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APU GENERATOR ..................................................................................................................................... 27

APU INDICATIONS .................................................................................................................................... 27

ENGINE OPERATING PROCEDURE LIMITS DUE TO WIND ............................................................................... 28

OPERATING SPEEDS ...................................................................................................................................... 28

RVSM MAXIMUM CRUISE MACH NUMBER ............................................................................................... 28

DESIGN MANEUVERING SPEED................................................................................................................. 28

FLAPS EXTENDED SPEED ........................................................................................................................... 29

MAXIMUM LANDING GEAR OPERATING SPEED ........................................................................................ 29

TIRE LIMIT SPEED ..................................................................................................................................... 29

MAXIMUM AIRSPEED FOR ADG OPERATION ............................................................................................ 29

TURBULENCE PENETRATION SPEED .......................................................................................................... 29

MINIMUM OPERATING LIMIT SPEED ........................................................................................................ 29

WINDSHIELD WIPER OPERATION ............................................................................................................. 29

MANEUVERING LOADS ............................................................................................................................. 29

SYSTEM LIMITATIONS ................................................................................................................................... 30

AIR-CONDITIONING & PRESSURIZATION .................................................................................................. 30

AUTOMATIC FLIGHT CONTROL SYSTEM.................................................................................................... 30

ELECTRICAL SYSTEMS ............................................................................................................................... 30

FLIGHT CONTROLS – LIFT / DRAG DEVICES ............................................................................................... 31

STALL PROTECTION SYSTEM ..................................................................................................................... 31

THRUST REVERSERS ................................................................................................................................. 31

TAXI LIGHTS ............................................................................................................................................. 31

MINIMUM DESCENT ALTITUDE, MDA ....................................................................................................... 31

TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) ................................................................... 31

INTEGRATED STANDBY INSTRUMENT (ISI) ................................................................................................ 32

PNEUMATIC SYSTEM ................................................................................................................................ 32

FLIGHT DECK DOOR .................................................................................................................................. 32

CRJ 700 ............................................................................................................................................................. 33

LOADSHEET .................................................................................................................................................. 33

PERFORMANCE ............................................................................................................................................ 36

V-SPEED-TABLES....................................................................................................................................... 36

STABILIZER TRIM TAKE-OFF SETTING - FLAPS 8 ......................................................................................... 61

STABILIZER TRIM TAKE-OFF SETTING - FLAPS 20 ....................................................................................... 62

NORMAL TAKE-OFF THRUST SETTINGS (ALL ENGINES OPERATING) %N1 – STATIC TO 65KIAS ................... 63

GO-AROUND THRUST SETTINGS (ALL ENGINES OPERATING) %N1 ............................................................. 65

GO-AROUND THRUST SETTINGS (ONE ENGINE INOPERATIVE) %N1 .......................................................... 67

MAXIMUM CONTINUOUS THRUST (ONE ENGINE INOPERATIVE), %N1 – 170KIAS ..................................... 69

MAXIMUM CONTINUOUS THRUST (ONE ENGINE INOPERATIVE), %N1 – 230 KIAS .................................... 70

V2 GO-AROUND SPEEDS, FLAPS 8 ............................................................................................................. 72

LANDING DATA, LANDING GEAR DOWN, FLAPS 45 ................................................................................... 73

LANDING DATA, LANDING WITH FLAPS OTHER THAN FLAPS 45 ................................................................ 74

FLIGHT PLANNING ........................................................................................................................................ 75

CLIMB (FL-050 TO FL-190) ........................................................................................................................ 75

CLIMB (FL-200 TO FL-290) ........................................................................................................................ 76

CLIMB (FL-300 TO FL-390) ........................................................................................................................ 77

CRUISE (FL-100 TO FL-240) ....................................................................................................................... 78

CRUISE (FL-250 TO FL-390) ....................................................................................................................... 79

DESCENT (FL-050 TO FL-190) .................................................................................................................... 80

DESCENT (FL-200 TO FL-290) .................................................................................................................... 81

DESCENT (FL-300 TO FL-390) .................................................................................................................... 82

CRJ 900 ............................................................................................................................................................. 83

LOADSHEET .................................................................................................................................................. 83

PERFORMANCE ............................................................................................................................................ 87

V-SPEED-TABLES....................................................................................................................................... 87

STABILIZER TRIM TAKE-OFF SETTING – FLAPS 8 ...................................................................................... 118

STABILIZER TRIM TAKE-OFF SETTING – FLAPS 20 .................................................................................... 119

NORMAL TAKE-OFF THRUST SETTINGS (ALL ENGINES OPERATING), %N1 - STATIC TO 65 KIAS ................ 120

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GO-AROUND THRUST SETTINGS %N1 ALL ENGINES OPERATING - 140 KIAS ............................................ 121

GO-AROUND THRUST SETTINGS %N1 (ONE ENGINE INOPERATIVE) – 140 KIAS ....................................... 123

MAXIMUM CONTINUOUS THRUST SETTINGS %N1 (ONE ENGINE INOPERATIVE) – 170 KIAS ................... 125

MAXIMUM CONTINUOUS THRUST SETTINGS %N1 (ONE ENGINE INOPERATIVE) – 230 KIAS ................... 126

V2 Go-Around Speeds, FLAPS 8 ............................................................................................................... 128

LANDING DATA, LANDING GEAR DOWN, FLAPS 45 (IMPERIAL) .............................................................. 129

LANDING DATA, LANDING GEAR DOWN, FLAPS 45 (METRIC) ................................................................. 130

LANDING DATA, LANDING WITH FLAPS OTHER THAN FLAPS 45 (IMPERIAL) ........................................... 131

LANDING DATA, LANDING WITH FLAPS OTHER THAN FLAPS 45 (METRIC) .............................................. 132

FLIGHT PLANNING ...................................................................................................................................... 133

CLIMB (FL-050 TO FL-190) ...................................................................................................................... 133

CLIMB (FL-200 TO FL-290) ...................................................................................................................... 134

CLIMB (FL-300 TO FL-370) ...................................................................................................................... 135

CRUISE (FL-100 TO FL-230) ..................................................................................................................... 136

CRUISE (FL-240 TO FL-370) ..................................................................................................................... 137

DESCENT (FL-050 TO FL-190) ................................................................................................................. 138

DESCENT (FL-200 TO FL-290) ................................................................................................................. 139

DESCENT (FL-300 TO FL-370) ................................................................................................................. 140

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INT R ODUCTION

This Quick Reference Handbook, (QRH), contains checklists and performance tables to be used with
Aerosoft / Digital Aviation’s representation of the CRJ. This QRH is basically split up in 4 major parts:

• Procedures: Graphical representations of how you are supposed to fly a certain set of
procedures,

• Checklists: The checklists for normal operations,

• Limitations: Describes the limitations for the CRJ700 and 900 in one chapter. In case

different limitations are valid both are provided in the QRH,

• Aircraft-specific information: This chapter will be split up in CRJ 700 and CRJ 900-specific
information like performance charts.

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PROCEDURES

NORMAL TAKE-OFF

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ILS APPROACH

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NON- PRECISION -APPROACH

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VISUAL APPROACHES

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CIRCLING APPROACH

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GO-AROUND

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TOUCH-AND-GO

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CHE CKLISTS

PRIOR TO STA RT

SAFE TY CHECK

1 Circuit breakers ....................................CLOSED

2 N/W steering switch ............................OFF

3 Hydraulic pumps ..................................OFF

4 Landing gear lever................................DOWN

5 flight spoiler lever ................................0

6 Slats / flaps lever ..................................SET (TO ACTUAL FLAP POSITION)

7 radar .....................................................OFF

8 ADG manual release ............................STOWED

9 Emergency flap switch .........................NORMAL

10 Battery master switch ..........................ON

Note: To prevent BLEED MISCONFIG caution messages during APU start, ensure that the
wing and cowl anti-ice switches are OFF prior to APU START.

11 APU / AC electrics ................................AS REQUIRED / ESTABLISHED

12 IRS ........................................................NAV

13 Emergency Equipment .........................CHECKED

14 Gear and safety pins ............................ON-BOARD

15 Airplane documents.............................CHECKED

16 Hydraulic 3A pump ..............................AS REQUIRED

17 FMS initialization .................................COMPLETE

CABIN INSPECTION

1 Cabin inspection ..................................ACCOMPLISH

EXTERNAL WALK AROUND

1 walk around inspection .......................ACCOMPLISH

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ORIGINATING CHECK

1 Internal and external

prefight checks .....................................COMPLETE

2 Pedals, seat and harness......................ADJUSTED

3 Crew oxygen and masks .......................CHECKED / QUANTITY

only first flight of the day

4 Audio warning panel ............................CHECKED

5 Electrical power panel .........................CHECKED

6 Fire detection / firex monitor test .......COMPLETE

only first flight of the day

7 External lights panel ............................CHECKED

8 Fuel panel ............................................CHECKED

9 Bleed air panel .....................................CHECKED

10 APU panel ............................................AS REQUIRED

11 Start panel............................................CHECKED

12 Hydraulic panel ....................................CHECKED

13 ELT switch .............................................ARM / RESET

14 CABIN PRESS panel ..............................CHECKED

15 Air conditioning panel..........................CHECKED

16 Ice detector tests .................................COMPLETE

only first flight of the day

17 WSHLD switches ..................................LOW

18 EMER LTS switch ..................................ARM

19 Standby compass .................................CHECKED

20 STALL test .............................................COMPLETE

only first flight of the day

21 N/W STRG switch .................................OFF

22 Clocks ...................................................SET

23 EFIS Control panels ..............................CHECKED

24 Instrument panels ................................CHECKED

25 EICAS and Standby instrument ............CHECKED

26 Anti-Skid test........................................COMPLETE

only first flight of the day

27 MLG BAY OVHT TEST ............................COMPLETE

only first flight of the day

28 Upper pedestal ....................................CHECKED

29 Thrust lever quadrant ..........................CHECKED

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30 Avionics ................................................CHECKED

31 Trims ....................................................CHECKED

32 YAW DAMPER .......................................ENGAGE

33 Source Select panel ..............................NORM

34 Lower pedestal.....................................CHECKED

BEFORE START CHECK

1 PASS SIGNS ...........................................ON

2 LDG ELEV ..............................................SET

3 BOOST PUMPS .....................................ON / Checked

Monitor centre tank quantity for not less than 10 minutes’ centre tank fuel

quantity must not increase by more than 68kg (150lb) after both boost pumps are

selected on

4 Altimeters ............................................SET

5 FMS / IRS ..............................................SET

6 Radios and Nav aids .............................SET FOR DEPARTURE

7 take-off briefing ...................................COMPLETE

CLE A RED TO START CHECK

1 APU / AC electrics ................................ON / CHECKED

2 Papers ..................................................ON BOARD

3 Take-off data ........................................SET

4 Doors ....................................................CLOSED / LOCKED

5 Beacon .................................................ON

6 Fuel pumps and quantity .....................ON (QTY)

7 Hydraulic pumps ..................................AUTO / ON

8 Parking brake .......................................AS REQUIRED

Note: Releasing the parking brake and turn off nose wheel steering if push-back is required.
Audio and visual communications with the ground crew must be maintained always during
push-back.

9 Engines .................................................START

10 Fuel Feed Check Valve test ..................COMPLETE

First flight of the day

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PRIOR TO TAKE -OFF

AFTER START CHECK

Note: Do not accelerate engine until oil pressure is in the normal operating range.

1 GEN 1 and GEN 2 .................................AUTO

2 BLEED valves and packs .......................AUTO / ON

3 Anti-Ice .................................................AS REQUIRED

4 Probes ..................................................ON

5 Electrics ................................................CHECKED

6 Rudder .................................................CHECKED

7 N/W STRG ............................................ARMED

TAX I CHECK

Note: At airports where runway structural repair or debris is known to exist, use thrust
reversers with extreme caution to preclude the possibility of foreign object damage (fod)
from occurring.

1 Flaps .....................................................___ ° INDICATING

2 Flight controls ......................................CHECKED

3 Trims ....................................................GREEN AND ____°

4 Thrust reversers ...................................ARMED

5 Flight instruments ................................CHECKED

6 FMS ......................................................AUTOTUNE

7 BRAKE TEMP ........................................CHECKED

BEFORE TAKE-OFF CHECK

1 Lights and strobes ................................AS REQUIRED

2 Fuel, XFLOW .........................................MAN AND OFF

3 IGNITION / ANTI-ICE ............................AS REQUIRED

4 Flight attendant ...................................ADVISED

5 Transponder / TCAS .............................ON / AS REQUIRED

6 Radar / terrain display .........................AS REQUIRED

7 CAS .......................................................CHECKED AND CLEARED

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AFTER TAKE-OFF

CLI MB CHECK

1 Fuel, XLFOW .........................................AUTO

2 Bleeds and APU ....................................SET

3 Lights and PASS SIGNS .........................AS REQUIRED

4 Thrust reversers ...................................OFF

5 CAS .......................................................CHECKED AND CLEARED

PRIOR TO LAN DING

DESCENT CHECK

1 LDG ELEV ..............................................SET

2 Fuel ......................................................CHECKED

3 TCAS .....................................................AS REQUIRED

4 Radar ....................................................AS REQUIRED

5 Terrain display ......................................AS REQUIRED

6 CAS .......................................................CHECKED AND CLEARED

7 Landing data ........................................SET

8 Approach briefing ................................COMPLETE

APPROACH CHECK

1 Altimeters ............................................___ . ___ SET

2 APU and Bleeds ....................................SET

3 Lights and PASS SIGNS .........................AS REQUIRED

BEFORE LANDING CHECK

1 Flight attendant ...................................ADVISED

2 PASS SIGNS ...........................................ON

3 Thrust reversers ...................................ARMED

4 LDG GEAR .............................................DN / DOWN

5 Flaps .....................................................___ ° INDICATING

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GO-AROUND PROCEDURE

Caution: A go-around manoeuvre should not be attempted after the thrust reverser have
been deployed.

Note: The minimum fuel quantity for go-around is 272kg (600lb) per wing (with the airplane
level) and assuming a maximum airplane climb attitude of 10° nose up.

1 Radios and nav aids .............................SET FOR GO AROUND

2 Thrust Levers / TOGA switch ................ADVANCE TO TOGA / PRESS

Advance thrust levers to the TOGA detent, then press TOGA switch

3 Airplane ................................................ROTATE SMOOTHLY TOWARDS THE FLIGHT

DIRECTOR BAR

4 Flaps .....................................................8

5 Pitch attitude ........................................ADJUST TO ACHIEVE AN AIRSPEED OF

V

2GA

+10 OR HIGHER AS FLAPS ARE RETRACTED TO 8°
When positive rate of climb is achieved:

6 Landing gear.........................................RETRACT / UP

7 Airspeed ...............................................MAINTAIN V

2GA

+10 OR HIGHER

8 Normal climb out procedures ..............ACCOMPLISH

AFTER LANDING

AFTER LANDING CHECK

1 APU ......................................................AS REQUIRED

2 Transponder / radar .............................STBY / OFF

3 Flaps .....................................................UP

4 Lights and strobes ................................AS REQUIRED

5 Probes ..................................................OFF

SHUTDOWN CHECK

Caution: Inform ground crew of 'hot' brakes condition as soon as possible.

Note: Thrust reversers must be stowed prior to engine shutdown.

1 Chocks and Brakes ...............................AS REQUIRED

2 Electrics ................................................SET

3 Fuel and Check valve test ....................COMPLETE

3 Thrust levers ........................................SHUT OFF

4 Seat Belts .............................................OFF

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5 ANTI ICE ...............................................OFF

6 Fuel pumps ..........................................OFF

7 Hydraulic 3A pump ..............................AS REQUIRED

8 Beacon .................................................OFF

9 N/W STRG switch .................................OFF

TERMINATING CHECK

1 Chocks and Brakes ...............................IN / OFF

2 IRS ........................................................OFF

3 Thrust levers ........................................OFF

4 EMER LTS switch ..................................OFF

5 WSHLD switch ......................................OFF

6 AFT CARGO switch ...............................OFF

7 HYDRALIC pumps .................................OFF

8 EXTERNAL LTS switches ........................OFF

9 APU START / STOP ................................OFF

10 APU PWR FUEL .....................................OFF

11 DC SERVICE switch ...............................OFF

12 BATTERY MASTER switch .....................OFF

13 DOME LIGHT switch .............................OFF

14 Boarding lights .....................................OFF

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LIMITATIONS

The CRJ is certified for day and night operation, VFR, IFR and flight in icing conditions.

STRUCTURAL WEIGHT LIMITATIONS

The simulated aircraft in this package are the CRJ700ER and CRJ900ER.

CRJ700ER

CRJ900ER

Maximum passengers

70

90

Dry Operating Weight

20‘290kg

44‘731lbs

22‘131kg

48‘790lbs

Maximum zero fuel weight
(MZFW)

28‘259kg

62‘300lbs

31‘751kg

70‘000lbs

Maximum Payload

8‘190kg

18‘055lbs

9‘907kg

21‘840lbs

Cargo Weight

2‘438kg

5‘375lbs

2‘756kg

6‘075lbs

Maximum Ramp Weight

34‘133kg

75‘250lbs

37‘735kg

82‘750lbs

Maximum take-off weight
(MTOW)

34‘019kg

75‘000lbs

37‘421kg

82‘500lbs

Maximum landing weight (MLW)

30‘391kg

67‘000lbs

33‘340kg

73‘500lbs

OPERATING LIMITATIONS (ALTITUDE AN D TEMPERATURE)

• Maximum airport pressure altitude for take-off and landing is 8‘000 feet.

• Maximum operating altitude is 41’000 feet.

• Maximum ambient air temperature approved for take-off and landing is ISA+35°C

• Minimum ambient temperature approved for take-off is -40°C (-40 °F).

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OPERATION IN ICING CONDITIONS

The anti-ice system must be activated when encountering icing conditions. Ice being detected by the
ice detector or visible moisture like fog, clouds, any form of precipitation and TAT of 10°C and less
require the activation of the anti-ice systems, except the SAT is -40°C (-40°F) or below.

COWL ANTI-ICE SYSTEM

Ground Operations: OAT of 10°C (50°F) or below and visible moisture in any form (fog with visibility
of 1,500 meters (one mile) or less, rain, precipitation), or operating on contaminated (snow, rain,
slush, …) runways/aprons/taxiways require the COWL anti-ice system to be activated.

Flight Operations: The cowl anti-ice system must be activated in the following two cases; when in
icing conditions, or in case ICE accumulation is annunciate by the ice detection system.

WING ANTI-ICE SYSTEM

Ground Operations: OAT of 5°C (41°F) or below and visible moisture in any form (fog with visibility
of 1,500 meters (one mile) or less, rain, precipitation), or operating on contaminated (snow, rain,
slush, …) runways/aprons/taxiways require the WING anti-ice system to be activated.

Flight Operations: The wing anti-ice system must be ON when ICE is annunciated by the ice
detection system, or when in icing conditions and the airspeed is less than 230 KIAS.

Do not hold in icing conditions with the flaps / slats extended.

RUNWAY SLOPES

The maximum runway slopes approved for take-off and landing are: +2% (uphill) -2% (downhill).

TAILWIND CON D ITIONS

The maximum tailwind component approved for take-off and landing is 10kts.

MINIMUM FLIGHT CREW

The minimum flight crew is one Captain and one First Officer.

MAXIMUM OCCUPANTS

The total number of passengers carried shall not exceed: 70 (CRJ-700) 90 (CRJ-900).

CARGO

Flight must be within 60 minutes of a suitable airport, if cargo is carried in either cargo compartment

POWER PLANT

Type: General Electric CF34-8C5B1

ENGINES INDICATIONS

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The engine limit display markings on the EICAS must be adhered to in any case.
Depending on the customer and the respective settings displayed on the EICAS might differ and be
more conservative from the limitations described here. The indications on the EICAS must be used
nevertheless.

RED – indicates maximum and minimum Limitations

AMBER - caution range

GREEN - Normal operating range

CF34-8C5B1

Indication

Red

Amber

Green

N1 % RPM

99,5

-

0 to 99,4

N2 % RPM

99,4

-

0 to 99,3

ITT ˚C

Variable*

-

Variable*

OIL TEMP˚C

164

156 to 163

-40 to 155

OIL PRESS psi

0 to 24

Variable

Variabe

*The respective ITT limit will be calculated automatically and displayed on the EICAS.

THRUST MANAGEMENT DAT A

The crew must verify, that the target N1 values stay within ±1.0% tolerance of the values provided on
the thrust setting charts. See the respective sections in the performance chapter of this QRH.

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ENGINE WARM-UP

The engine is supposed to be run in IDLE until oil pressure reaches the normal operating range.

The following 2 minutes after engine start N1 may not exceed 75% unless all operating indications
are in normal range already.

Engine operating limits

Limit

Ground

Start

Assisted Air

Start

Windmill

Start

Idle

Max.

Continuous

Normal

Take-off

(TOGA)

APR (Max

Power)

N1 - -

-

20 - 25%

99,50%

99,50%

99,50%

ITT

815°C

815°C

927°C

-

960°C

923°C (2

min)

1‘006°C (2

min)

N2

0-45%

0-45%

55-65%

98,00%

99,40%

99,40%

Oil Temp

-40°C

(minimum)

155°C

163°C (15

min)

163°C (15

min)

Oil Press

182 psi

95 psi (after

10 min)

182 psi

95 psi (after

10 min)

182 psi

95 psi (after

10 min)

25-60 psi

25--95 psi

(oil temp <

60 °C)

45-95 psi

45-95 psi

45-95 psi

Minimum Oil

Level for

Flight

40%

minimum

with

affected

engine not

started

- - - - -

-

[1] Normal take-off power and Maximum power (two engines) is limited to 5 minutes.
[2] APR power (one engine) is limited to 10 minutes.
[3] ITT must be below 120°C before attempting to ground start engine.
[4] Maximum oil pressure is limited to 156 psi when oil temperature transient is less than 60°C.
[5] Oil pressures (above IDLE) between 25 psi and 45 psi require oil temperature monitoring.
[6] Oil pressure should show positive value during start and may peak beyond 182 psi (max display
value). Oil pressures above 182 psi are displayed as amber dashes. Oil pressure may be greater than 95
psi for a maximum of 10 minutes.
[7] For further details, refer to the Airplane Operating Manual
[8] ITT must be below 90°C before attempting to air start engine.

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CON T INUOUS ENGINE IG NITION

Continuous engine ignition must be activated when encountering either of the following conditions:

• Take-offs and landings on contaminated runways

• Flight through moderate or heavier intensity rain

• Flight through moderate or heavier intensity turbulence

• Flight near thunderstorms.

STARTER CRAN KING LIMIT S

The starter may not be used if indicated N2 rpm exceeds 45%. The engine starters may not be
activated longer than certain time limits. The time limits are shown on the following tables.

ENGINE START (GROUND)

START

MAX TIME ON

FOLLOWED BY

1 & 2

90 seconds

10 seconds cool down
3 through 5

90 seconds

5 minutes cool down

ENGINE START OR MOTORING (IN FLIGHT)

START

MAX TIME ON

FOLLOWED BY

1

120 seconds

10 seconds cool down
2 through 5

60 seconds

5 minutes cool down

MOTORING (GROUND)

START

MAX TIME ON

FOLLOWED BY

1

90 seconds

5 minutes cool down
2 through 5

30 seconds

5 minutes cool down

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ENGINE RELIGHT

RELIGHT TYPE

ENVELOPE

CRJ700

CRJ900

Wind milling

Altitude from 21’000 feet to 10’000 feet:
Speed 290 KIAS to VMO and 7.2% N2 minimum.

Altitude from 25’000

feet to sea level:
Speed 250 KIAS to VMO
and 7.2% N2 minimum.

Wind milling

Altitude from 10’000 feet to sea level:
Speed 250 KIAS to VMO and 7.2% N2 minimum.

Starter-assisted

Altitude from 21’000 feet to sea level:
Speed from V

REF

up to VMO and from 0 to 45% N2.

All-Engine-Out Rapid Relight

Altitude from 10’000 feet to sea level:
FADEC rapid relight capability has been demonstrated at 200 KIAS for up
to 15-second fuel interruptions

FUE L

The maximum permissible fuel imbalance between main left tank and the main right tank:

• During Take-off: 136 kg (300 lb)

• All other phases of flight: 363 kg (800 lb)

As soon as a tank’s quantity indicator reads zero fuel, the remaining fuel is not useable.
The following table shows the maximum useable fuel quantity per tank (based on 6.75 lb per US gal,
and 2’046 lb per kg conversion factors):

Pressure Refueling

Gravity Refueling

Left main tain

3‘398 kg (7,492 lb)

3‘306 kg (7,290 lb)

Right main tank

3‘398 kg (7,492 lb)

3‘306 kg (7,290 lb)

Centre tank

2‘091 kg (4,610 lb)

Total

8‘887 kg (19‘594 lb)

6‘612 kg (14‘580 lb)

Take-off with a fuel load more than 227 kg (500 lb) in the centre tank is only permitted under
certain conditions:

• each main wing tank is above 1‘996 kg (4‘400 lb), or

• each main wing tank is above 907 kg (2’000 lb), and

• the allowable zero fuel weight is reduced by the weight of the fuel in the centre tank more

than 227 kg (500 lb); and

• the centre of gravity (CG) in this configuration is verified to be within the allowable CG
envelope as calculated from the Load sheet.

The minimum fuel quantity for go-around is 272 kg (600 lb) per wing (with the aircraft level) and
assuming a maximum aircraft climb attitude of 10 degrees nose up.

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FUE L TEMPERATURE

• Take-off with engine fuel temperature indications below 5°C (41 °F) is prohibited.

• Take-off with bulk fuel temperature indications below the limits stated is prohibited.

• During flight, bulk fuel temperature must remain above the applicable bulk fuel freezing

point.

FUEL

BULK FUEL TAKE-OFF LIMIT
MINIMUM TEMPERATURE

BULK FUEL FREEZING POINT
ASTM D 1‘655 Jet A

-30°C

-40°C

ASTM D 1‘655 JET A1

-37°C

-47°C

FUE L CROSSFLOW

Powered crossflow and gravity crossflow must be off for take-off.

AUXILLIARY POWER UNIT, A PU

TYPE: Allied Signal RE 220 (RJ)
MAXIMUM RPM: 106%

STARTING:

1. Minimum ambient temperature for starting a cold soaked APU on the ground is -40°C

2. Maximum EGT (dependent upon altitude and temperature): 692 °C to 1‘038 °C

3. Maximum amount of start attempts in one hour: 3

A two-minute delay must be observed between cranking attempts to allow for cooling of starter

and starter contactor and for APU drainage.

OPERATING RANGE:

• Maximum EGT on ground: 682°C to 789 °C

• Maximum EGT in flight: 773 °C to 806 °C

• Maximum EGT: 1‘038°C (not to be exceeded under any conditions).

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APU BLEED AIR

APU BLEED AIR LIMITATIONS

System / Condition

Limitation

Bleed air extraction

not permitted above 25’000.

Engine-start during ground operations

No bleed air extraction limitation.
Each engine may be started using the APU as a bleed
air source.

APU GENERATOR

The maximum permissible load on the APU generator is 40 kVA.

APU INDICATIONS

The APU limit display markings on the EICAS must be used to determine compliance with the
maximum limit and precautionary ranges. If EICAS markings show more conservative limitation those
specified below, the limit markings on the EICAS should be used.

INDICATION

RED

GREEN

APU EGT °C

807

0 to 806

APU % RPM

107

0 to 106

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ENGINE OPERATING PROCEDURE LIMITS DUE TO WIND

Wind and fan speed limitations as shown in the illustration below must be observed:

Wind Condition

Limitation

NOTE 1

Within 30° on either direction of the
airplane nose; no wind speed limit OR
>30° in either direction of the airplane
nose; <5 knots wind speed.

No limitation – TOGA thrust may be
applied before brakes released.

NOTE 2

>30° in either direction of the airplane
nose, between 5 and 30 knots wind speed

Apply maximum of 75% N1 before brakes
released, then TOGA thrust.

NOTE 3

>30° in either direction of the airplane
nose; >30 knots wind speed

Apply maximum of idle / taxi thrust before
brakes released, then TOGA thrust.

OPERATING SPE EDS

The maximum operating speed is not to be exceeded during any phase off light (i.e. climb, cruise,
descent).

RVSM MAXIMUM CRUISE MACH NUMBER

The maximum cruise MACH number when operating in RVSM airspace: 0.83.

DESIGN MANEUVERING SPEED

Full deflection of rudder and aileron, or manoeuvres that involve angles of attack near the stall, must
be performed at speeds below VA.

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Avoid large and alternating control inputs, especially in combination with large changes in pitch, roll,

or yaw large side slip angles) as they may cause structural failure at any speed, including below VA.

FLAPS EXTENDED SPEED

The maximum speeds at which the flaps may be extended are:

• FLAPS 1: 230 KIAS

• FLAPS 8: 230 KIAS

• FLAPS 20: 230 KIAS

• FLAPS 30: 185 KIAS

• FLAPS 45: 170 KIAS

MAXIMUM LAND ING GEAR OPERATING SPEED

• Maximum speed to extend the landing gear is: 220 KIAS.

• Maximum speed to fly with landing gear extended and locked: 220 KIAS

• Maximum speed at which the landing gear needs to be retracted: 200 KIAS

TIRE LIMIT SPEED

The tire limit on the ground is 182 kts (CRJ700)
The tire limit on the ground is 195 kts (CRJ900)

MAXIMUM AIRSPEED FOR ADG OPERATION

The maximum speed to operate the Air Driven Generator, ADG VMO / MMO.

TURBULENCE PENETRATION SPEED

The maximum airspeed for turbulence penetration: 280 KIAS or 0.75 Mach, (whichever is higher.)

MINIMUM OPERATING LIMIT SPEED

As soon as the stick shaker is activated a further speed reduction is prohibited.

WIND SHIELD WIPER OPERATION

Maximum windshield wiper operation speed: 250 KIAS.
In case the windshield wiper has failed in a non-parked position, the airplane speed must not exceed
250 KIAS.
To prevent the wipers from jamming using the INT mode is prohibited.

MANEUVERING LOADS

MANEUVERING LIMIT LOAD FACTORS

Maximum load factor during manoeuvres, turns etc - Flaps up: -1.0G to 2.5G
Maximum load factor during manoeuvres, turns etc - Flaps down: 0.0G to 2.0G

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SIDE SLIP MANUEVERS

Avoid unnecessary and large side slips during low speed high altitude cruise.

SYST E M LIMITATIONS

AIR-CONDITIONING & PR E SSURIZATION

• Maximum relief differential pressure 8.7psi

• Maximum negative differential pressure -0.5psi

• Max. pressure differential during taxi, take-off and landing 0.1psi

• CRJ700 Maximum altitude for single pack operation 31’000 feet

• CRJ900 Maximum altitude for single pack operation 25’000 feet

The airplane must be completely depressurized prior to opening any of the airplane doors.

The EMER DEPRESS button may not be used above 15’000ft to prevent possible harm to crew

and/or passenger ‘s ears

AUTOMATIC FLIGHT CONTROL SYSTEM

The following tables shows the minimum heights to which autopilot usage is approved depending on
the flight phase and glide path angle respectively.

FLIGHT PHASE

GLIDEPATH ANGLE
Airport elevation

MINIMUM USE
HEIGHT

≤ 4‘000 feet

> 4‘000 feet

Take-off

- - -

600 feet AGL

Non-precision approach

-

Approved

Approved

400 feet AGL

Precision appoach

≤ 3.5°

Approved

Approved

80 feet AGL

> 3.5°
≤ 4.0°

Approved

Approved

120 feet AGL

ELECTRICAL SYSTEMS

PERMISSIBLE LOADS ON AC SYSTEM

The following table shows the maximum individual AC generator loading:

AC LOAD LIMIT (KVA)

ALTITUDE (FEET)

MAIN GENERATOR (EACH)

APU GENERATOR

0 – 41’000

40

40

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PERMISSIBLE LOADS ON DC SYSTEMS

• In Flight: Maximum continuous load on each TRU 120 amps.

• Ground Operation: Maximum time for ground operations with DC power only 5 minutes

(to protect the CRT displays from damage)

FLIG HT CONTR OLS – LIFT / DRAG DEVI CES

SLATS / FLAPS

• En-route use of slats / flaps is prohibited.

• Flight with slats / flaps extended at altitudes above 15’000 feet is prohibited.

FLIGHT SPOILER

• Do not extend the flight spoilers below 300ft AGL.

• Furthermore, do not extend the flight spoiler at airspeeds below the recommended

approach speed plus 10 KIAS.

STALL PROTECTION SYSTEM

Both stall protection systems switches must remain on for all phases of flight.

THRUST REVERSERS

• Thrust reversers may not be activated during flight – they are approved for ground use only

• The thrust levers may not be activated during touch and go – only on full stop landings.

• Display of any thrust reverser icons or EICAS warnings before takeoff is a no-go-item

• CRJ700: The thrust revers may be used with maximum thrust until passing 75 kts

• CRJ700: Below 75 kts only idle reverser is allowed

• CRJ900: The thrust revers may be used with maximum thrust until passing 60 kts

• CRJ900: Below 60 kts only idle reverser is allowed

• Backing up / power push with the revers is prohibited

TAX I LIGHTS

As soon as the aircraft is not moving for 10 minutes or longer the TAXI lights must be switched OFF.

MINIMUM DESCENT ALTITUDE, MDA

In case the given Minimum descent altitude, MDA may not be dialled in using the DH/MDA knob,
please select the next highest 10-foot increment.

TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS)

In order to comply with a resolution advisory (RA) from the TCAS system, the pilots are authorized to
deviate from air traffic control’s clearance.

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INT EGRATED STANDBY IN STRUMENT (ISI)

In case NAV 1 is tuned to a valid ILS frequency, the ISI will display localizer and glideslope deviation
on the back-course approach. The use of the ISI localizer and back course information is not allowed
for back course approaches.

PNEUMATIC SY STEM

IN FLIGHT: In case the APU as selected as a bleed source in manual mode, using the WING and / or
COWL anti-ice is prohibited.

ON THE GROUND: To prevent an engine stall or engine instability during taxi please comply to the
following items:

• APU running, prior and during taxi:

• BLEED SOURCE must be switched to BOTH ENG

• BLEED VALVES must be switched to MANUAL

• Prior to takeoff (before advancing the thrust levers further than ground idle)

• BLEED VALVES must be switched to AUTO

FLIG HT DECK D OOR

The flight deck door must be closed and locked always during the flight.

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CRJ 700

LOA D SHEET

CRJ 700 TAKEOFF AND LANDING DATA CARD

WEIGHT AND BALANCE

PAYLOAD

Maximum CRJ700ER: 8‘190kg / 18‘055lbs Maximum CRJ900ER: 9‘907kg / 21‘840lbs

Description

Maximum Weight

Passenger count

Arm

Weight

Moment

[kg]

[lbs]

Max

Actual

[in]

[ft]

[kg or lbs]

Dry Operation
Weight

20.290

44.731

789,6

65,80

Pilots

95ea

209ea 2

255

21,25

Forward Flight
Attendant

75ea

165ea 1

312

26,00

Aft Flight
Attendant

75ea

165ea 1

962

80,17

Passengers
Rows 1-3

84ea

185ea

10

439

36,58

Passengers
Rows 4-6

84ea

185ea

12

530

44,17

Passengers
Rows 7-9

84ea

185ea

12

623

51,92

Passengers
Rows 10-12

84ea

185ea

12

716

59,67

Passengers
Rows 14-16

84ea

185ea

12

819

68,25

Passengers
Rows 18-20

84ea

185ea

12

912

76,00

Forward Cargo
compartment

454

1.001

557

46,42

Aft Cargo
compartment

1.497

3.003

1.049

87,42

Zero Fuel
Weight (ZFW)

28.259

62.300

FUEL

Fuel Wing
tanks (left +
right)

6.832

15.062

777

64,75
Fuel Center
tank

2.115

4.663

745

62,08

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TAKEOFF

Description

Maximum Weight

Passenger count

Arm

Weight

Moment

[kg]

[lbs]

Max

Actual

[in]

[ft]

[kg or lbs]

Takeoff
Weight = Zero
Fuel Weight +
Est. Fuel at
Takeoff

34.019

75.000
Center of
Gravity [%
MAC]

0.00%

5.00%

10.00%

15.00%

20.00%

25.00%

30.00%

35.00%

762 767 772 777 782 787

CoG [% MAC]

Arm [in]

CoG (CRJ700)

0.00%

5.00%

10.00%

15.00%

20.00%

25.00%

30.00%

35.00%

861 866 871 876

CoG [% MAC]

Arm [in]

CoG (CRJ900)

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TAKEOFF

Airport

Field Elev.

QNH

RWY.

C.G. & Trim

Temp.

V1

VR

V2

Flaps 20 → Flaps 8

Flaps 8 → Flaps 1

Flaps 1 → Flaps 0

LANDING

Est. Rem. Fuel

Landing Weight = Zero Fuel Weight + Est. Rem. Fuel

Max. Landing Weight

CRJ700ER: 30.391kg / 67.000lbs CRJ900ER: 33.340kg / 73.500lbs

Airport

Field Elev.

QNH

RWY.

C.G. & Trim

Temp.

V

Ref

V

2GA

Flaps 20 → Flaps 8

Flaps 8 → Flaps 1

Flaps 1 → Flaps 0

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PERFORMANCE

V-SPEED-TABLE S

50’000LBS / 22‘680KG

50’000lbs / 22‘680 kgs

Landing

Flaps

0°

1°

8°

20°

30°

45°

Min Maneuvering

166

150

144

138

134

126

V

REF

156

140

134

128

124

116

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

113

113

113

114

114

114

114

113

113

112

20°C

112

113

113

113

114

114

113

113

112

112

30°C

112

113

114

114

115

114

113

113

112

112

40°C

113

114

115

38° /
115

34° /
115

113

112

112

38° /
112

34° /
112

MAX TEMP

50° / 115

46° / 115

42° / 115

50° / 112

46° / 112

42° / 112

VR

≤ 10°C

116

116

116

116

116

114

114

113

113

112

20°C

116

116

116

116

116

114

113

113

112

112

30°C

116

116

116

116

116

114

113

113

112

112

40°C

116

116

116

38° /
116

34° /
116

113

112

112

38° /
112

34° /
112

MAX TEMP

50° / 116

46° / 116

42° / 116

50° / 112

46° / 112

42° / 112 V2

/ V

2GA

132 / 123

129

Flap

Retraction

144

(Flaps 1)

148

(Flaps 0)

131

(Flaps 8)

149

(Flaps 1)

149

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL310

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

163

165

168

171

173

175

177

180

182

185

188

VMD/Min Hold

177

186

187

188

190

193

195

197

200

202

205

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52’000LBS / 23‘587 KGS

52’000lbs / 23‘587 kgs

Landing

Flaps

0°

1°

8°

20°

30°

45°

Min Maneuvering

169

153

147

141

137

129

V

REF

159

143

137

131

127

119

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

113

114

114

114

115

114

113

113

112

112

20°C

113

113

114

114

115

113

113

113

112

112

30°C

113

114

114

115

115

114

113

112

112

112

40°C

114

115

115

38° /
116

34° /
115

113

112

112

38° /
112

34° /
112

MAX TEMP

50° / 115

46° / 116

42° / 115

50° / 112

46° / 112

42° / 112

VR

≤ 10°C

116

116

116

116

116

114

113

113

112

112

20°C

116

116

116

116

116

113

113

113

112

112

30°C

116

116

116

116

116

113

113

112

112

112

40°C

116

116

116

38° /
116

34° /
116

113

112

112

38° /
112

34° /
112

MAX TEMP

50° / 116

46° / 116

42° / 116

50° / 112

46° / 112

42° / 112

V2 / V

2GA

131 / 126

128

Flap

Retraction

143

(Flaps 1)

151

(Flaps 0)

140

(Flaps 8)

148

(Flaps 1)

151

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL310

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

166

168

171

175

177

179

181

184

186

189

192

VMD/Min Hold

180

190

191

193

195

198

200

202

205

207

208

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53’000LBS / 24‘040 KGS

53’000lbs / 24‘040 kgs

Landing

Flaps

0°

1°

8°

20°

30°

45°

Min Maneuvering

170

154

148

142

138

130

V

REF

160

144

138

132

128

120

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

113

114

114

114

115

114

113

113

112

112

20°C

113

113

114

114

115

113

113

113

112

112

30°C

113

114

114

115

115

113

113

112

112

111

40°C

114

115

115

38° /
116

34° /
115

113

112

112

38° /
111

34° /
111

MAX TEMP

50° / 115

46° / 116

42° / 115

50° / 112

46° / 112

42° / 112

VR

≤ 10°C

116

116

116

116

116

114

113

113

112

112

20°C

116

116

116

116

116

113

113

113

112

112

30°C

116

116

116

116

116

113

113

112

112

111

40°C

116

116

116

38° /
116

34° /
116

113

112

112

38° /
111

34° /
111

MAX TEMP

50° / 116

46° / 116

42° / 116

50° / 112

46° / 112

42° / 112

V2 / V

2GA

130 / 127

127

Flap

Retraction

142

(Flaps 1)

152

(Flaps 0)

139

(Flaps 8)

147

(Flaps 1)

152

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL310

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

167

170

173

176

178

181

183

186

188

191

194

VMD/Min Hold

18

192

193

195

197

200

202

205

207

209

209

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54’000LBS / 24‘494 KGS

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

114

114

114

115

115

114

113

113

112

112

20°C

114

114

114

115

115

113

113

113

112

112

30°C

113

114

115

115

116

113

113

112

112

111

40°C

115

115

115

38° /
116

34° /
116

113

112

112

38° /
111

34° /
111

MAX TEMP

50° / 116

46° / 116

42° / 116

50° / 112

46° / 112

42° / 112

VR

≤ 10°C

116

116

116

116

116

114

113

113

112

112

20°C

116

116

116

116

116

113

113

113

112

112

30°C

116

116

116

116

116

113

112

112

112

111

40°C

116

116

116

38° /
116

34° /
116

113

112

112

38° /
111

34° /
111

MAX TEMP

50° / 116

46° / 116

42° / 116

50° / 112

46° / 112

42° / 112

V2 / V

2GA

130 / 128

127

Flap

Retraction

142

(Flaps 1)

154

(Flaps 0)

139

(Flaps 8)

147

(Flaps 1)

154

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL310

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

169

172

175

178

180

182

185

187

190

193

196

VMD/Min Hold

184

194

195

197

200

202

205

207

209

212

211

54’000lbs / 24‘494 kgs

Landing

Flaps

0°

1°

8°

20°

30°

45°

Min Maneuvering

171

155

149

143

139

131

V

REF

161

145

139

133

129

121

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-40

02-May-2017

55’000LBS / 24‘948 KGS

55’000lbs / 24‘948 kgs

Landing

Flaps

0°

1°

8°

20°

30°

45°

Min Maneuvering

172

156

150

144

140

132

V

REF

162

146

140

134

130

122

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

114

114

114

115

115

113

113

113

112

112

20°C

114

114

114

115

115

113

113

113

112

112

30°C

113

114

115

115

116

113

113

112

112

111

40°C

115

115

115

38° /
116

34° /
116

113

112

112

38° /
111

34° /
111

MAX TEMP

50° / 116

46° / 116

42° / 116

50° / 112

46° / 112

42° / 112

VR

≤ 10°C

116

116

116

116

116

113

113

113

112

112

20°C

116

116

116

116

116

113

113

113

112

112

30°C

116

116

116

116

116

113

113

112

112

111

40°C

116

116

116

38° /
116

34° /
116

113

112

112

38° /
111

34° /
111

MAX TEMP

50° / 116

46° / 116

42° / 116

50° / 112

46° / 112

42° / 112

V2 / V

2GA

130 / 129

127

Flap

Retraction

142

(Flaps 1)

155

(Flaps 0)

139

(Flaps 8)

147

(Flaps 1)

155

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL310

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

170

174

177

180

182

184

186

189

192

195

198

VMD/Min Hold

185

196

197

199

202

205

207

209

212

214

212

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-41

02-May-2017

56’000LBS / 25‘401 KGS

56’000lbs / 25‘401 kgs

Landing

Flaps

0°

1°

8°

20°

30°

45°

Min Maneuvering

173

157

151

145

141

133

V

REF

163

147

141

135

131

123

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

114

115

115

116

117

114

113

113

112

112

20°C

114

114

115

116

117

113

113

113

112

112

30°C

114

115

116

117

119

114

113

112

112

112

40°C

115

116

117

38° /
118

34° /
118

113

112

112

38° /
112

34° /
112

MAX TEMP

50° / 117

46° / 117

42° / 117

50° / 112

46° / 112

42° / 112

VR

≤ 10°C

116

116

116

116

117

113

113

113

112

112

20°C

116

116

116

117

117

113

113

113

112

112

30°C

116

116

117

117

118

113

113

112

112

112

40°C

116

117

117

38° /
118

34° /
118

113

112

112

38° /
112

34° /
112

MAX TEMP

50° / 117

46° / 117

42° / 117

50° / 112

46° / 112

42° / 112

V2 / V

2GA

130 / 130

127

Flap

Retraction

142

(Flaps 1)

157

(Flaps 0)

139

(Flaps 8)

147

(Flaps 1)

157

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL310

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

172

175

178

182

184

186

188

191

194

197

200

VMD/Min Hold

187

198

200

202

204

207

209

212

214

216

213

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-42

02-May-2017

57’000LBS / 25‘855 KGS

57’000lbs / 25‘855 kgs

Landing

Flaps

0°

1°

8°

20°

30°

45°

Min Maneuvering

174

158

152

146

142

134

V

REF

164

148

142

136

132

124

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

114

115

115

116

117

113

113

113

112

112

20°C

114

114

115

116

117

113

113

112

112

112

30°C

114

115

116

117

119

113

113

112

112

113

40°C

115

116

118

38° /
119

34° /
119

112

112

112

38° /
113

34° /
113

MAX TEMP

50° / 117

46° / 118

42° / 118

50° / 112

46° / 112

42° / 112

VR

≤ 10°C

116

116

116

116

117

113

113

113

112

112

20°C

116

116

116

117

118

113

113

112

112

112

30°C

116

116

117

118

119

113

113

112

112

113

40°C

116

117

118

38° /
119

34° /
119

112

112

112

38° /
113

34° /
113

MAX TEMP

50° / 117

46° / 118

42° / 118

50° / 112

46° / 112

42° / 112

V2 / V

2GA

129 / 131

126

Flap

Retraction

141

(Flaps 1)

158

(Flaps 0)

138

(Flaps 8)

146

(Flaps 1)

158

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL310

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

173

177

180

183

185

188

190

193

195

198

202

VMD/Min Hold

189

200

202

204

207

209

212

214

216

218

214

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-43

02-May-2017

58’000LBS / 26‘308 KGS

58’000lbs / 26‘308 kgs

Landing

Flaps

0°

1°

8°

20°

30°

45°

Min Maneuvering

175

159

153

147

143

135

V

REF

165

149

143

137

133

125

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

115

116

117

118

118

113

113

112

113

113

20°C

115

116

117

118

11

113

113

112

113

114

30°C

115

116

117

119

120

113

113

113

113

114

40°C

117

118

119

38° /
120

34° /
120

112

113

113

38° /
114

34° /
114

MAX TEMP

50° / 118

46° / 119

42° / 119

50° / 113

46° / 113

42° / 113

VR

≤ 10°C

116

116

117

118

119

113

113

113

113

113

20°C

117

117

117

118

119

113

113

113

113

114

30°C

117

117

118

119

120

113

113

113

113

114

40°C

117

118

119

38° /
120

34° /
120

112

113

113

38° /
114

34° /
114

MAX TEMP

50° / 118

46° / 119

42° / 119

50° / 113

46° / 113

42° / 113

V2 / V

2GA

130 / 133

126

Flap

Retraction

142

(Flaps 1)

160

(Flaps 0)

138

(Flaps 8)

146

(Flaps 1)

160

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL280

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

175

178

182

185

187

189

192

194

197

200

204

VMD/Min Hold

190

202

204

206

209

211

214

216

219

219

215

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-44

02-May-2017

59’000LBS / 26‘762 KGS

59’000lbs / 26‘762 kgs

Landing

Flaps

0°

1°

8°

20°

30°

45°

Min Maneuvering

176

160

154

148

144

136

V

REF

166

150

144

138

134

126

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

116

117

118

119

119

113

113

112

113

114

20°C

116

117

118

119

120

113

113

112

113

115

30°C

115

116

119

120

121

113

112

113

114

115

40°C

118

119

120

38° /
121

34° /
121

112

113

114

38° /
115

34° /
115

MAX TEMP

50° / 119

46° / 120

42° / 120

50° / 114

46° / 115

42° / 114

VR

≤ 10°C

117

117

118

119

120

113

113

112

114

114

20°C

117

118

118

119

120

113

113

113

114

115

30°C

117

118

119

120

121

113

112

113

114

115

40°C

118

119

120

38° /
121

34° /
121

112

113

114

38° /
115

34° /
115

MAX TEMP

50° / 119

46° / 120

42° / 120

50° / 114

46° / 115

42° / 114

V2 / V

2GA

130 / 134

125

Flap

Retraction

142

(Flaps 1)

161

(Flaps 0)

137

(Flaps 8)

145

(Flaps 1)

161

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL280

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

176

180

183

187

189

191

193

196

199

202

206

VMD/Min Hold

192

204

206

208

211

214

216

218

221

220

216

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-45

02-May-2017

60’000LBS / 27‘216 KGS

60’000lbs / 27‘216 kgs

Landing

Flaps

0°

1°

8°

20°

30°

45°

Min Maneuvering

177

161

155

149

145

137

V

REF

167

151

145

139

135

127

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

117

118

119

120

121

113

114

113

114

115

20°C

117

118

118

120

122

113

114

113

114

115

30°C

117

118

120

122

123

113

113

115

116

117

40°C

119

120

121

38° /
123

34° /
123

114

115

116

38° /
117

34° /
117

MAX TEMP

50° / 121

46° / 121

42° / 121

50° / 115

46° / 116

42° / 116

VR

≤ 10°C

118

119

120

120

121

113

114

114

114

115

20°C

118

119

120

121

122

113

114

114

115

116

30°C

118

119

120

122

123

114

114

115

116

117

40°C

119

120

121

38° /
123

34° /
123

114

115

116

38° /
117

34° /
117

MAX TEMP

50° / 121

46° / 122

42° / 121

50° / 115

46° / 116

42° / 116

V2 / V

2GA

131 / 135

125

Flap

Retraction

143

(Flaps 1)

163

(Flaps 0)

137

(Flaps 8)

145

(Flaps 1)

163

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL270

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

178

181

185

189

191

193

195

198

201

204

208

VMD/Min Hold

194

206

208

211

214

216

218

221

223

222

217

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-46

02-May-2017

61’000LBS / 27‘669 KGS

61’000lbs / 27‘669 kgs

Landing

Flaps

0°

1°

8°

20°

30°

45°

Min Maneuvering

178

162

156

150

146

138

V

REF

168

152

146

140

136

128

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

118

119

120

121

122

113

114

115

115

116

20°C

118

119

120

121

123

113

114

115

116

117

30°C

118

120

121

123

124

113

114

116

117

118

40°C

120

121

122

38° /
124

34° /
124

115

116

117

38° /
118

34° /
118

MAX TEMP

50° / 122

46° / 123

42° / 122

50° / 116

46° / 117

42° / 117

VR

≤ 10°C

119

120

121

121

122

113

114

115

115

116

20°C

119

120

121

122

123

113

114

115

116

117

30°C

119

120

121

123

124

114

115

116

117

118

40°C

120

121

122

38° /
124

34° /
124

115

116

117

38° /
118

34° /
118

MAX TEMP

50° / 122

46° / 123

42° / 122

50° / 116

46° / 117

42° / 117

V2 / V

2GA

132 / 136

125

Flap

Retraction

144

(Flaps 1)

164

(Flaps 0)

137

(Flaps 8)

145

(Flaps 1)

164

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL270

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

179

183

186

190

192

195

197

200

203

206

210

VMD/Min Hold

196

208

210

213

216

218

221

223

225

223

218

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-47

02-May-2017

62’000LBS / 28‘123 KGS

62’000lbs / 28‘123 kgs

Landing

Flaps

0°

1°

8°

20°

30°

45°

Min Maneuvering

179

163

157

151

147

139

V

REF

169

153

147

14

137

129

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

120

121

122

123

124

114

115

116

117

118

20°C

120

121

122

123

124

114

115

116

117

118

30°C

120

121

123

124

125

114

116

117

118

119

40°C

122

123

124

38° /
125

34° /
125

116

117

118

38° /
119

34° /
119

MAX TEMP

50° / 123

46° / 125

42° / 124

50° / 117

46° / 118

42° / 118

VR

≤ 10°C

120

121

122

123

124

114

115

116

117

118

20°C

121

121

122

123

124

115

115

116

117

118

30°C

121

122

123

124

125

115

116

117

118

119

40°C

121

123

124

38° /
125

34° /
125

116

117

118

38° /
119

34° /
119

MAX TEMP

50° / 123

46° / 125

42° / 124

50° / 117

46° / 118

42° / 118

V2 / V

2GA

133 / 137

126

Flap

Retraction

145

(Flaps 1)

166

(Flaps 0)

138

(Flaps 8)

146

(Flaps 1)

166

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL310

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

181

184

188

192

194

196

199

202

205

208

211

VMD/Min Hold

199

210

212

215

218

220

223

225

227

224

219

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-48

02-May-2017

63’000LBS / 28‘576 KGS

63’000lbs / 28‘576 kgs

Landing

Flaps

0°

1°

8°

20°

32‘270°

45°

Min Maneuvering

180

164

158

152

148

140

V

REF

170

154

148

142

138

130

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

121

122

123

124

125

115

116

117

118

119

20°C

121

122

123

124

125

115

116

117

118

119

30°C

121

122

124

125

126

115

117

118

119

120

40°C

123

124

125

38° /
126

34° /
126

117

118

119

38° /
120

34° /
120

MAX TEMP

50° / 124

46° / 126

42° / 125

50° / 118

46° / 119

42° / 119

VR

≤ 10°C

121

122

123

124

125

115

116

117

118

119

20°C

122

122

123

124

125

116

116

117

118

119

30°C

122

123

124

125

126

116

117

118

119

120

40°C

121

124

125

38° /
126

34° /
126

117

118

119

38° /
120

34° /
120

MAX TEMP

50° / 124

46° / 126

42° / 125

50° / 118

46° / 119

42° / 119

V2 / V

2GA

133 / 138

127

Flap

Retraction

145

(Flaps 1)

167

(Flaps 0)

139

(Flaps 8)

147

(Flaps 1)

167

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL310

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

182

186

189

193

195

198

200

203

206

209

213

VMD/Min Hold

201

212

214

217

220

222

225

227

228

225

219

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

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VOL

2

2-1-49

02-May-2017

64’000LBS / 29‘030 KGS

64’000lbs / 29‘030 kgs

Landing

Flaps

0°

1°

8°

20°

30°

45°

Min Maneuvering

182

166

160

154

150

142

V

REF

172

156

150

144

140

132

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

122

123

124

125

126

116

118

118

119

120

20°C

122

123

124

125

127

116

117

118

120

121

30°C

122

124

125

126

128

116

118

119

120

122

40°C

124

125

127

38° /
128

34° /
128

118

119

120

38° /
121

34° /
122

MAX TEMP

50° / 126

46° / 127

42° / 127

50° / 120

46° / 121

42° / 120

VR

≤ 10°C

123

123

124

125

126

117

118

118

119

120

20°C

123

124

124

125

127

117

118

118

120

121

30°C

123

124

125

126

128

117

118

119

120

122

40°C

123

125

127

38° /
128

34° /
128

118

119

120

38° /
121

34° /
122

MAX TEMP

50° / 126

46° / 127

42° / 127

50° / 120

46° / 121

42° / 120

V2 / V

2GA

134 / 139

128

Flap

Retraction

146

(Flaps 1)

169

(Flaps 0)

140

(Flaps 8)

148

(Flaps 1)

169

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL260

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

184

187

191

195

197

199

202

205

208

211

215

VMD/Min Hold

203

214

217

220

222

225

227

230

230

226

-

Aerosoft – Digital Aviation

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VOL

2

2-1-50

02-May-2017

65’000LBS / 29‘484 KGS

65’000lbs / 29‘484 kgs

Landing

Flaps

0°

1°

8°

20°

30°

45°

Min Maneuvering

183

167

161

155

151

143

V

REF

173

157

151

145

141

133

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

123

124

125

126

127

117

119

119

120

121

20°C

123

124

125

126

128

117

118

119

121

122

30°C

123

125

126

127

129

117

119

120

121

123

40°C

125

126

128

38° /
129

34° /
129

119

120

121

38° /
122

34° /
123

MAX TEMP

50° / 127

46° / 128

42° / 128

50° / 121

46° / 122

42° / 121

VR

≤ 10°C

124

124

125

126

127

118

119

119

120

121

20°C

124

125

125

126

128

118

119

119

121

122

30°C

124

125

126

127

129

118

119

120

121

123

40°C

125

126

128

38° /
129

34° /
129

119

120

121

38° /
122

34° /
123

MAX TEMP

50° / 127

46° / 128

42° / 128

50° / 121

46° / 122

42° / 121

V2 / V

2GA

135 / 140

129

Flap

Retraction

147

(Flaps 1)

170

(Flaps 0)

141

(Flaps 8)

149

(Flaps 1)

170

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL310

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

185

189

192

196

198

201

204

207

210

213

217

VMD/Min Hold

206

216

219

222

224

227

229

232

231

227

-

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

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VOL

2

2-1-51

02-May-2017

66’000LBS / 29‘937 KGS

66’000lbs / 29‘937 kgs

Landing

Flaps

0°

1°

8°

20°

30°

45°

Min Maneuvering

184

168

162

156

152

144

V

REF

174

158

152

146

142

134

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

125

126

127

128

129

119

120

120

121

123

20°C

125

126

127

128

129

119

120

121

122

123

30°C

125

126

128

129

130

119

120

121

123

124

40°C

126

128

129

38° /
130

34° /
130

120

121

123

38° /
124

34° /
124

MAX TEMP

50° / 128

46° / 130

42° / 129

50° / 122

46° / 123

42° / 123

VR

≤ 10°C

125

126

127

128

129

119

120

120

121

123

20°C

125

126

127

128

129

119

120

121

122

123

30°C

125

126

128

129

130

119

120

121

123

124

40°C

126

128

129

38° /
130

34° /
130

120

121

123

38° /
124

34° /
124

MAX TEMP

50° / 128

46° / 130

42° / 129

50° / 122

46° / 123

42° / 123

V2 / V

2GA

136 / 142

130

Flap

Retraction

136

(Flaps 1)

142

(Flaps 0)

142

(Flaps 8)

150

(Flaps 1)

172

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL250

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

187

190

194

198

200

203

206

209

212

215

219

VMD/Min Hold

208

218

221

224

226

229

231

234

232

228

-

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-52

02-May-2017

67’000LBS / 30‘391 KGS

67’000lbs / 30‘391 kgs

Landing

Flaps

0°

1°

8°

20°

30°

45°

Min Maneuvering

185

169

163

157

153

145

V

REF

175

159

153

147

143

135

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

126

127

128

129

130

120

121

121

122

124

20°C

126

127

128

129

130

120

121

122

123

124

30°C

126

127

129

130

131

120

121

122

124

125

40°C

127

129

130

38° /
131

34° /
131

121

122

124

38° /
125

34° /
125

MAX TEMP

50° / 129

46° / 131

42° / 130

50° / 123

46° / 124

42° / 124

VR

≤ 10°C

126

127

128

129

130

120

121

121

122

124

20°C

126

127

128

129

130

120

121

122

123

124

30°C

126

127

129

130

131

120

121

122

124

125

40°C

127

129

130

38° /
131

34° /
131

121

122

124

38° /
125

34° /
125

MAX TEMP

50° / 129

46° / 131

42° / 130

50° / 123

46° / 124

42° / 124

V2 / V

2GA

137 / 143

130

Flap

Retraction

149

(Flaps 1)

173

(Flaps 0)

142

(Flaps 8)

150

(Flaps 1)

173

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL310

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

188

192

195

199

202

205

207

210

213

217

220

VMD/Min Hold

210

220

223

226

228

231

233

236

233

228

-

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-53

02-May-2017

68’000LBS / 30‘844 KGS

68’000lbs / 30‘844 kgs

Landing (overweight)

Flaps

0°

1°

8°

20°

30°

45°

Min Maneuvering

186

170

164

158

154

146

V

REF

176

160

154

148

144

136

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

127

128

129

130

131

121

122

123

124

125

20°C

127

128

129

130

132

121

122

123

124

125

30°C

127

128

130

131

133

121

122

124

125

126

40°C

129

130

131

38° /
133

34° /
133

123

124

125

38° /
126

34° /
126

MAX TEMP

50° / 131

46° / 132

42° / 131

50° / 124

46° / 125

42° / 125

VR

≤ 10°C

127

128

129

130

131

121

122

123

124

125

20°C

127

128

129

130

132

121

122

123

124

125

30°C

128

129

130

131

133

121

122

124

125

126

40°C

129

130

131

38° /
133

34° /
133

123

124

125

38° /
126

34° /
126

MAX TEMP

50° / 131

46° / 132

42° / 131

50° / 124

46° / 125

42° / 125

V2 / V

2GA

138 / 144

131

Flap

Retraction

150

(Flaps 1)

175

(Flaps 0)

143

(Flaps 8)

151

(Flaps 1)

175

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL310

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

190

193

197

201

203

206

209

212

215

218

222

VMD/Min Hold

213

222

225

228

230

233

235

237

234

229

-

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

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VOL

2

2-1-54

02-May-2017

69’000LBS / 31‘298 KGS

69’000lbs / 31‘298 kgs

Landing (overweight)

Flaps

0°

1°

8°

20°

30°

45°

Min Maneuvering

187

171

165

159

155

147

V

REF

177

161

155

149

145

137

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

128

129

130

131

132

122

123

124

125

126

20°C

128

129

130

131

133

122

123

124

125

126

30°C

128

129

131

132

134

122

123

125

126

127

40°C

130

131

132

38° /
134

34° /
134

124

125

126

38° /
127

34° /
127

MAX TEMP

50° / 132

46° / 133

42° / 132

50° / 125

46° / 126

42° / 126

VR

≤ 10°C

128

129

130

131

132

122

123

124

125

126

20°C

128

129

130

131

133

122

123

124

125

126

30°C

129

130

131

132

134

122

123

125

126

127

40°C

130

131

132

38° /
134

34° /
134

124

125

126

38° /
127

34° /
127

MAX TEMP

50° / 132

46° / 133

42° / 132

50° / 125

46° / 126

42° / 126

V2 / V

2GA

139 / 145

132

Flap

Retraction

151

(Flaps 1)

176

(Flaps 0)

144

(Flaps 8)

152

(Flaps 1)

176

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL240

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

191

195

197

202

205

208

210

213

216

220

224

VMD/Min Hold

215

224

227

230

233

235

238

239

235

230

-

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-55

02-May-2017

70’000LBS / 31‘751 KGS

70’000lbs / 31‘751 kgs

Landing (overweight)

Flaps

0°

1°

8°

20°

30°

45°

Min Maneuvering

188

172

166

160

156

148

V

REF

178

162

156

150

146

138

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

129

130

131

132

133

123

124

125

126

127

20°C

129

130

131

133

134

123

124

125

126

128

30°C

129

131

132

134

135

123

125

126

127

128

40°C

131

132

134

38° /
135

34° /
135

125

126

127

38° /
128

34° /
128

MAX TEMP

50° / 133

46° / 134

42° / 134

50° / 126

46° / 128

42° / 127

VR

≤ 10°C

129

130

131

132

133

123

124

125

126

127

20°C

130

130

131

133

134

123

124

125

126

127

30°C

130

131

132

134

135

123

125

126

127

128

40°C

131

132

134

38° /
135

34° /
135

125

126

127

38° /
128

34° /
128

MAX TEMP

50° / 133

46° / 134

42° / 134

50° / 126

46° / 128

42° / 127

V2 / V

2GA

140 / 146

133

Flap

Retraction

152

(Flaps 1)

177

(Flaps 0)

145

(Flaps 8)

153

(Flaps 1)

177

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL310

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

192

196

200

204

206

209

212

215

218

222

226

VMD/Min Hold

217

226

230

232

235

237

240

240

236

231

-

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-56

02-May-2017

71’000LBS / 32‘205 KGS

71’000lbs / 32‘205 kgs

Landing (overweight)

Flaps

0°

1°

8°

20°

30°

45°

Min Maneuvering

189

173

167

161

157

149

V

REF

179

163

157

151

147

139

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

130

131

132

133

134

124

125

126

127

128

20°C

130

131

132

134

135

124

125

126

127

129

30°C

130

132

133

135

136

124

126

127

128

129

40°C

132

133

135

38° /
136

34° /
136

126

127

128

38° /
129

34° /
129

MAX TEMP

50° / 134

46° / 135

42° / 135

50° / 127

46° / 129

42° / 128

VR

≤ 10°C

130

131

132

133

134

124

125

126

127

128

20°C

131

131

132

134

135

124

125

126

127

128

30°C

131

132

133

135

136

124

126

127

128

129

40°C

132

133

135

38° /
136

34° /
136

126

127

128

38° /
128

34° /
129

MAX TEMP

50° / 134

46° / 135

42° / 135

50° / 127

46° / 129

42° / 128

V2 / V

2GA

141 / 147

134

Flap

Retraction

153

(Flaps 1)

178

(Flaps 0)

146

(Flaps 8)

154

(Flaps 1)

178

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL310

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

193

198

201

205

208

211

214

217

220

224

227

VMD/Min Hold

219

229

232

234

237

239

242

241

237

231

-

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-57

02-May-2017

72’000LBS / 32‘659 KGS

72’000lbs / 32‘659 kgs

Landing (overweight)

Flaps

0°

1°

8°

20°

30°

45°

Min Maneuvering

190

174

168

162

158

150

V

REF

180

164

158

152

148

140

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

132

132

134

135

136

125

126

127

128

129

20°C

132

133

134

135

136

125

126

128

129

130

30°C

132

133

135

136

137

126

127

128

129

130

40°C

133

135

136

38° /
137

34° /
137

127

128

129

38° /
130

34° /
130

MAX TEMP

50° / 135

46° / 137

42° / 136

50° / 127

46° / 130

42° / 129

VR

≤ 10°C

132

132

134

135

136

125

126

127

128

129

20°C

132

133

134

135

136

125

126

128

129

130

30°C

132

133

135

136

137

126

127

128

129

130

40°C

133

135

136

38° /
137

34° /
137

127

128

129

38° /
129

34° /
130

MAX TEMP

50° / 135

46° / 137

42° / 136

50° / 129

46° / 130

42° / 129

V2 / V

2GA

142 / 148

135

Flap

Retraction

154

(Flaps 1)

180

(Flaps 0)

147

(Flaps 8)

155

(Flaps 1)

180

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL220

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

195

199

203

207

209

212

215

218

222

225

229

VMD/Min Hold

222

231

233

236

239

241

244

242

238 - -

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

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VOL

2

2-1-58

02-May-2017

73’000LBS / 33‘112 KGS

73’000lbs / 33‘112 kgs

Landing (overweight)

Flaps

0°

1°

8°

20°

30°

45°

Min Maneuvering

191

175

169

163

159

151

V

REF

181

165

159

153

149

141

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

133

133

135

136

137

126

127

128

129

130

20°C

133

134

135

136

137

126

127

129

130

131

30°C

133

134

136

137

138

127

128

129

130

131

40°C

134

136

137

38° /
138

34° /
138

128

129

130

38° /
130

34° /
131

MAX TEMP

50° / 136

46° / 138

42° / 137

50° / 130

46° / 131

42° / 130

VR

≤ 10°C

133

133

135

136

137

126

127

128

129

130

20°C

133

134

135

136

137

126

127

129

130

131

30°C

133

134

136

137

138

127

128

129

130

131

40°C

134

136

137

38° /
138

34° /
138

128

129

130

38° /
130

34° /
131

MAX TEMP

50° / 136

46° / 138

42° / 137

50° / 130

46° / 131

42° / 130

V2 / V

2GA

143 / 149

136

Flap

Retraction

155

(Flaps 1)

181

(Flaps 0)

148

(Flaps 8)

156

(Flaps 1)

181

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL220

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

196

200

204

208

211

214

217

220

223

227

231

VMD/Min Hold

223

233

235

238

241

243

246

244

239 - -

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

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VOL

2

2-1-59

02-May-2017

74’000LBS / 33‘566 KGS

74’000lbs / 33‘566 kgs

Landing (overweight)

Flaps

0°

1°

8°

20°

30°

45°

Min Maneuvering

192

176

170

164

160

152

V

REF

182

166

160

154

150

142

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

134

135

136

137

138

127

129

129

130

131

20°C

134

135

136

137

139

128

130

130

131

132

30°C

134

135

137

138

139

128

130

130

132

132

40°C

136

137

138

38° /
139

34° /
139

129

131

131

38° /
132

34° /
132

MAX TEMP

50° / 138

46° / 139

42° / 138

50° / 131

46° / 131

42° / 131

VR

≤ 10°C

134

135

136

137

138

127

128

129

130

131

20°C

134

135

136

137

139

128

129

130

131

132

30°C

134

135

137

138

139

128

129

130

132

132

40°C

136

137

138

38° /
139

34° /
139

129

130

131

38° /
132

34° /
132

MAX TEMP

50° / 138

46° / 139

42° / 138

50° / 131

46° / 131

42° / 131

V2 / V

2GA

144 / 150

137

Flap

Retraction

156

(Flaps 1)

186

(Flaps 0)

149

(Flaps 8)

157

(Flaps 1)

183

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL220

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

198

202

206

210

212

215

218

221

225

229

233

VMD/Min Hold

225

235

237

240

243

245

248

245

240 - -

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

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VOL

2

2-1-60

02-May-2017

75’000LBS / 34‘019 KGS

75’000lbs / 34‘019 kgs

Landing (overweight)

Flaps

0°

1°

8°

20°

30°

45°

Min Maneuvering

193

177

171

165

161

153

V

REF

183

167

161

155

151

143

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

135

136

137

138

139

128

129

130

131

132

20°C

135

136

137

138

140

129

130

131

132

133

30°C

135

136

138

139

140

129

130

131

133

133

40°C

137

138

139

38° /
140

34° /
140

130

131

132

38° /
133

34° /
133

MAX TEMP

50° / 139

46° / 140

42° / 139

50° / 132

46° / 131

42° / 132

VR

≤ 10°C

135

136

137

138

139

128

129

130

131

132

20°C

135

136

137

138

140

129

130

131

132

133

30°C

135

136

138

139

140

129

130

131

132

133

40°C

137

138

139

38° /
140

34° /
140

130

131

132

38° /
133

34° /
133

MAX TEMP

50° / 139

46° / 140

42° / 139

50° / 132

46° / 131

42° /
1‘132

V2 / V

2GA

144 / 151

137

Flap

Retraction

156

(Flaps 1)

186

(Flaps 0)

149

(Flaps 8)

157

(Flaps 1)

184

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL210

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

199

203

207

211

214

217

220

223

226

230

234

VMD/Min Hold

226

237

239

242

244

247

249

246

240 - -

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

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VOL

2

2-1-61

02-May-2017

STABILIZER T R IM TAKE-OFF SETTING - FLAPS 8

C.G

[%MAC]

Trim Setting

[Units]

22‘680kg

24‘267kg

25‘855kg

26‘000kg

27‘259kg

28‘259kg

30‘000kg

32‘000kg

34‘000kg

50‘000lbs

53‘500lbs

57‘000lbs

61‘300lbs

62‘300lbs

65‘000lbs

69‘000lbs

72‘000lbs

75‘000lbs

14

6,7

7,2

7,7

8,4

8,4

8,6

8,8

8,9

9,1

15

6,6

7,0

7,5

8,2

8,2

8,5

8,6

8,7

8,9

17

6,3

6,7

7,1

7,8

7,8

8,1

8,2

8,3

8,5

19

6,0

6,4

6,8

7,5

7,5

7,7

7,8

8,0

8,1

21

5,7

6,1

6,5

7,1

7,1

7,4

7,5

7,6

7,7

23

5,4

5,8

6,1

6,7

6,7

6,9

7,1

7,2

7,2

25

5,1

5,4

5,8

6,1

6,4

6,6

6,7

6,8

6,8

27

4,8

5,1

5,5

6,0

6,0

6,2

6,3

6,4

6,4

29

4,5

4,8

5,1

5,6

5,6

5,8

5,9

6,0

6,0

31

4,2

4,5

4,8

5,3

5,3

5,4

5,5

5,6

5,6

33

3,9

4,2

4,4

4,9

4,9

5,0

5,1

5,2

5,2

35

3,6

3,9

4,1

4,5 - - - -

-

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

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VOL

2

2-1-62

02-May-2017

STABILIZER T R IM TAKE-OFF SETTING - FLAPS 20

C.G

[%MAC]

Trim Setting

[Units]

22‘680kg

24‘267kg

25‘855kg

26‘000kg

27‘259kg

28‘259kg

30‘000kg

32‘000kg

34‘000kg

50‘000lbs

53‘500lbs

57‘000lbs

61‘300lbs

62‘300lbs

65‘000lbs

69‘000lbs

72‘000lbs

75‘000lbs

14

5,8

6,3

6,7

6,8

7,9

7,9

8,6

9,3

9,7

15

5,6

6,1

6,5

6,6

7,6

7,6

8,4

9,0

9,4

17

5,3

5,8

6,2

6,2

7,2

7,2

8,0

8,5

8,9

19

5,0

5,5

5,8

5,9

6,8

6,8

7,5

8,0

8,4

21

4,7

5,1

5,5

5,5

6,4

6,4

7,1

7,5

7,9

23

4,4

4,8

5,1

5,2

6,0

6,0

6,6

7,7

7,4

25

4,1

4,4

4,7

4,8

5,6

5,6

6,2

6,6

6,8

27

3,8

4,1

4,4

4,4

5,2

5,2

5,7

6,1

6,3

29

3,6

3,7 4 4,1

4,7

4,7

5,3

5,6

5,8

31

3,6

3,6

3,7

3,7

4,3

4,3

4,8

5,1

5,3

33

3,6

3,6

3,6

3,6

3,9

3,9

4,4

4,6

4,8

35

3,6

3,6

3,6

3,6

3,6 - - - -

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

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VOL

2

2-1-63

02-May-2017

NORMAL TAKE-OFF THRUST SETTINGS (ALL EN GI NES OPERATING) %N1 – STATIC TO
65KIAS

ENGINE BLEEDS CLOSED

PACKS ON, ANTI ICE OFF

°C °F -1000 0 2000 4000 6000 8000 10000 12000 14000

-45 -49 83,9 84,2

-40 -40 79,3 79,7 80,5 81,3 82,1 83,1 84,0 84,8 85,0

-35 -31 80,1 80,5 81,3 82,1 82,9 83,9 84,8 85,6 85,9

-30 -22 80,9 81,3 82,2 82,9 83,8 84,7 85,7 86,4 86,7

-25 -13 81,7 82,1 82,9 83,8 84,6 85,5 86,5 87,3 87,5

-20 -4 82,4 82,9 83,8 84,6 85,4 86,3 87,3 88,1 88,3

-15 5 83,2 83,7 84,5 85,3 86,2 87,1 88,1 88,9 89,1

-10 14 84,0 84,5 85,3 86,1 87,0 87,9 88,9 89,7 89,9

-5 23 84,8 85,3 86,1 86,9 87,8 88,7 89,7 90,4 90,7
0 32 85,5 86,0 86,8 87,7 88,6 89,5 90,5 91,2 91,5

5 41 86,3 86,8 87,6 88,4 89,3 90,3 91,2 92,0 92,0

10 50 87,0 87,5 88,4 89,2 90,1 91,0 92,0 91,9 91,8
15 59 87,8 88,2 89,1 89,9 90,8 91,6 91,5 91,4 91,3

20 68 88,5 89,0 89,8 90,7 91,1 91,0 90,9 90,8 90,7

25 77 89,2 89,7 90,6 90,6 90,5 90,4 90,3 90,2 90,1
30 86 89,9 90,4 90,2 89,9 89,7 89,6 89,5 89,4 89,4

35 95 89,5 89,6 89,4 89,1 88,9 88,8 88,7 88,7
40 104 88,3 88,3 88,3 88,2 88,1 88,0

45 113 86,9 86,9 87,0 87,3 87,2
50 122 85,4 85,4 85,5 86,4

OAT

Pressure Altitude

°C °F -1000 0 2000 4000 6000 8000 10000 12000 14000

-45 -49 83,4 83,6

-40 -40 78,8 79,3 80,1 80,8 81,6 82,6 83,5 84,2 84,4

-35 -31 79,6 80,1 80,9 81,7 82,4 83,4 84,3 85,1 85,3

-30 -22 80,4 80,9 81,7 82,5 83,3 84,2 85,1 85,9 86,1

-25 -13 81,2 81,7 82,5 83,3 84,1 85,0 85,9 86,7 86,9

-20 -4 82,0 82,5 83,3 84,1 84,9 85,8 86,7 87,5 87,7

-15 5 82,8 83,2 84,1 84,4 85,7 86,6 87,5 88,3 88,5

-10 14 83,5 84,0 84,8 85,6 86,4 87,4 88,3 89,1 89,3

-5 23 84,3 84,8 85,8 86,4 87,2 88,1 89,1 89,8 90,0
0 32 85,0 85,6 86,3 87,2 88,0 88,9 89,9 90,6 90,8

5 41 85,8 86,3 87,1 87,9 88,7 89,7 90,6 91,4 91,3

10 50 86,5 87,0 87,8 88,7 89,5 90,4 91,4 91,2 91,1
15 59 87,2 87,7 88,6 89,4 90,2 90,9 90,8 90,7 90,5

20 68 87,9 88,4 89,3 90,1 90,5 90,4 90,2 90,1 89,9
25 77 88,7 89,2 90,0 90,0 89,8 89,7 89,6 89,4 89,2

30 86 89,4 89,9 89,6 89,3 89,0 88,9 88,7 88,6 88,5
35 95 88,9 89,0 88,9 88,4 88,2 88,0 87,9 87,8

40 104 87,6 87,7 87,6 87,5 87,3 87,1
45 113 86,2 86,2 86,2 86,6 86,3

50 122 84,7 84,7 84,7 85,6

OAT

Pressure Altitude

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

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VOL

2

2-1-64

02-May-2017

PACKS ON, COWL ANTI ICE ON

PACKS ON, COWL & WING ANTI ICE ON

°C °F -1000 0 2000 4000 6000 8000 10000 12000 14000

-45 -49 83,4 83,6

-40 -40 78,8 79,3 80,1 80,8 81,6 82,6 83,5 84,2 84,4

-35 -31 79,8 80,1 80,9 81,7 82,4 83,4 84,3 85,1 85,3

-30 -22 80,4 80,9 81,7 82,5 83,3 84,2 85,1 85,9 86,1

-25 -13 81,2 81,7 82,5 83,3 84,1 85,0 85,9 86,7 86,9

-20 -4 82,0 82,5 83,3 84,1 84,9 85,8 86,7 87,5 87,7

-15 5 82,8 83,2 84,1 84,8 85,7 86,6 87,5 88,3 88,5

-10 14 83,5 84,0 84,3 85,6 86,4 87,4 88,3 89,1 89,3

-5 23 84,3 84,8 85,6 86,4 87,2 88,1 89,1 89,8 90,0
0 32 85,0 85,5 86,3 87,2 88,0 88,9 89,9 90,6 90,8

5 41 85,8 86,3 87,1 87,9 88,7 89,7 90,6 91,1 91,0

10 50 86,5 87,0 87,8 88,7 89,5 90,4 90,8 90,6 90,4

OAT

Pressure Altitude

°C °F -1000 0 2000 4000 6000 8000 10000 12000 14000

-45 -49 83,4 83,6

-40 -40 78,8 79,3 80,1 80,8 81,8 82,6 83,5 84,2 84,4

-35 -31 79,6 80,1 80,9 81,7 82,4 83,4 84,3 85,1 85,3

-30 -22 80,4 80,9 81,7 82,5 83,3 84,2 85,1 85,9 86,1

-25 -13 81,2 81,7 82,5 83,3 84,1 85,0 85,9 86,7 86,9

-20 -4 82,0 82,5 83,3 84,1 84,9 85,8 86,7 87,5 87,7

-15 5 82,8 83,2 84,1 84,8 85,7 86,6 87,5 88,3 88,4

-10 14 83,5 84,0 84,8 85,6 86,4 87,4 88,3 88,8 88,8

-5 23 84,3 84,8 85,6 86,4 87,2 88,1 88,9 88,4 88,1
0 32 85,0 85,5 86,3 87,2 88,0 88,7 88,3 88,0 86,2

5 41 85,8 86,3 87,1 87,9 88,8 88,2 87,8 87,4 85,1

10 50 86,5 87,0 87,5 88,5 88,0 87,6 87,2 86,6 84,4

OAT

Pressure Altitude

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-65

02-May-2017

GO-AROUND THR UST SETTINGS (ALL ENGINES OPERATING ) %N1

ENGINE BLEEDS CLOSED

PACKS ON, ANTI ICE OFF

°C °F -1000 0 2000 4000 6000 8000 10000 12000 14000

-45 -49 84,1 84,4

-40 -40 79,2 79,5 80,6 81,3 82,2 83,2 84,0 84,9 85,2

-35 -31 80,1 80,5 81,3 82,2 82,9 83,9 84,8 85,8 86,0

-30 -22 80,9 81,2 82,3 83,0 83,8 84,8 85,8 86,6 86,9

-25 -13 81,7 82,0 83,0 83,9 84,6 85,6 86,6 87,5 87,7

-20 -4 82,4 82,8 83,9 84,7 85,4 86,4 87,4 88,3 88,5

-15 5 83,1 83,6 84,6 85,4 86,3 87,2 88,2 89,1 89,3

-10 14 84,0 84,4 85,4 86,2 87,0 88,0 89,0 89,9 90,1

-5 23 84,8 85,1 86,1 87,0 87,8 88,8 89,8 90,6 90,9
0 32 85,5 85,9 86,9 87,8 88,6 89,6 90,5 91,3 91,7

5 41 86,3 86,7 87,7 88,5 89,4 90,3 91,2 92,1 91,8

10 50 86,9 87,4 88,5 89,3 90,1 91,1 92,1 91,6 91,4
15 59 87,8 88,1 89,2 90,0 90,8 91,7 91,3 91,1 91,0

20 68 88,5 88,9 89,9 90,8 91,1 90,9 90,9 90,6 90,3
25 77 89,1 89,7 90,7 90,6 90,5 90,3 90,2 89,9 89,8

30 86 89,9 90,3 90,0 89,7 89,6 89,6 89,4 89,2 89,0
35 95 89,4 89,3 89,2 88,7 88,5 88,5 88,6 88,6

40 104 88,2 88,0 87,8 87,7 87,6 87,5
45 113 86,7 86,5 86,6 86,8 86,7

50 122 85,2 85,0 85,1 86,0

OAT

Pressure Altitude

°C °F -1000 0 2000 4000 6000 8000 10000 12000 14000

-45 -49 83,7 83,9

-40 -40 78,8 79,2 80,2 80,9 81,7 82,7 83,6 84,4 84,7

-35 -31 79,6 80,0 81,0 81,8 82,5 83,5 84,4 85,3 85,6

-30 -22 80,4 80,8 81,8 82,6 83,3 84,3 85,2 86,1 86,4

-25 -13 81,2 81,6 82,6 83,4 84,2 85,1 86,0 86,9 87,2

-20 -4 82,0 82,4 83,4 84,2 85,0 85,9 86,7 87,7 88,0

-15 5 82,8 83,1 84,2 84,5 85,7 86,7 87,6 88,5 88,8

-10 14 83,5 83,9 84,9 85,7 86,5 87,5 88,4 89,4 89,5

-5 23 84,3 84,7 85,9 86,5 87,3 88,3 89,2 90,0 90,3
0 32 85,0 85,5 86,4 87,3 88,1 89,1 90,0 90,9 91,0

5 41 85,8 86,2 87,2 88,1 88,8 89,8 90,7 91,6 91,2

10 50 86,5 86,9 87,9 88,8 89,6 90,6 91,5 90,9 90,8
15 59 87,1 87,6 88,6 89,5 90,8 91,0 90,7 90,5 90,3

20 68 87,9 88,2 89,5 90,2 90,6 90,4 90,2 89,9 89,6
25 77 88,7 89,1 90,1 90,0 89,8 89,7 89,6 89,2 88,9

30 86 89,4 89,8 89,4 89,2 88,9 88,9 88,6 88,5 88,2
35 95 88,8 88,7 88,6 88,1 87,9 87,7 87,8 87,7

40 104 87,5 87,4 87,2 87,1 86,9 86,5
45 113 86,0 85,8 85,8 86,2 85,8

50 122 84,5 84,3 84,3 85,2

OAT

Pressure Altitude

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-66

02-May-2017

PACKS ON, COWL ANTI ICE ON

PACKS ON, COWL & WING ANTI ICE ON

°C °F -1000 0 2000 4000 6000 8000 10000 12000 14000

-45 -49 84,5 85,3

-40 -40 78,8 79,2 80,2 80,9 81,7 82,7 83,6 84,4 84,7

-35 -31 79,8 80,0 81,0 81,8 82,5 83,5 84,4 85,3 85,6

-30 -22 80,4 80,8 81,8 82,6 83,4 84,3 85,2 86,1 86,4

-25 -13 81,2 81,6 82,6 83,4 84,2 85,1 86,0 86,9 87,2

-20 -4 82,0 82,4 83,4 84,2 85,0 85,9 86,8 87,7 88,0

-15 5 82,8 83,1 84,2 84,9 85,8 86,7 87,6 88,5 88,8

-10 14 83,5 83,9 84,4 85,7 86,5 87,5 88,4 89,4 89,5

-5 23 84,3 84,7 85,7 86,5 87,3 88,3 89,2 90,0 90,3
0 32 85,0 85,4 86,4 87,3 88,1 89,1 90,0 90,9 91,0

5 41 85,8 86,2 87,2 88,1 88,8 89,8 90,7 91,2 90,7

10 50 86,5 86,9 87,9 88,8 89,6 90,6 90,8 90,3 90,2

OAT

Pressure Altitude

°C °F -1000 0 2000 4000 6000 8000 10000 12000 14000

-45 -49 83,7 83,9

-40 -40 78,8 79,2 80,2 80,9 81,9 82,7 83,6 84,4 84,7

-35 -31 79,6 80,0 81,0 81,8 82,5 83,5 84,4 85,3 85,6

-30 -22 80,4 80,8 81,8 82,6 83,4 84,3 85,2 86,1 86,4

-25 -13 81,2 81,6 82,6 83,4 84,2 85,1 86,0 86,9 87,2

-20 -4 82,0 82,4 83,4 84,2 85,0 85,9 86,8 87,7 88,0

-15 5 82,8 83,1 84,2 84,9 85,8 86,7 87,6 88,5 88,7

-10 14 83,5 83,9 84,9 85,7 86,5 87,5 88,4 89,2 88,6

-5 23 84,3 84,7 85,7 86,5 87,3 88,3 89,2 88,4 88,0
0 32 85,0 85,4 86,4 87,3 88,1 89,0 88,4 88,1 86,2

5 41 85,8 86,2 87,2 88,1 89,0 88,4 88,1 87,5 86,6

10 50 86,5 86,9 87,6 88,8 88,2 87,7 87,4 86,7 85,9

OAT

Pressure Altitude

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-67

02-May-2017

GO-AROUND THR UST SETTINGS (ONE ENGINE INOPERATIVE) %N1

PACKS OFF, BLEEDS CLOSED

PACKS ON, ANTI ICE OFF

°C °F -1000 0 2000 4000 6000 8000 10000 12000 14000

-45 -49 81,8 82,9

-40 -40 76,6 77,0 77,7 78,7 79,4 80,1 81,2 82,7 83,6

-35 -31 77,4 77,7 78,6 79,4 80,2 81,0 82,0 83,5 84,6

-30 -22 78,2 78,5 79,5 80,2 81,0 81,7 82,9 84,3 85,4

-25 -13 79,0 79,3 80,1 81,1 81,8 82,5 83,7 85,2 86,2

-20 -4 79,6 80,1 81,0 81,9 82,6 83,3 84,5 86,0 87,0

-15 5 80,4 80,9 81,7 82,6 83,4 84,1 85,3 86,8 87,8

-10 14 81,2 81,7 82,5 83,4 84,2 85,0 86,1 87,6 88,6

-5 23 82,0 82,5 83,3 84,2 85,0 85,8 86,9 88,4 89,4
0 32 82,7 83,1 84,0 85,0 85,9 86,6 87,8 89,2 90,3

5 41 83,4 83,9 84,8 85,8 86,5 87,5 88,7 90,3 90,7

10 50 84,2 84,6 85,6 86,5 87,3 88,5 90,2 90,2 90,0
15 59 84,9 85,3 86,3 87,2 88,4 89,6 89,5 89,3 89,0

20 68 85,6 86,1 87,0 88,2 88,9 88,7 88,4 88,4 88,3
25 77 86,3 86,8 87,8 88,1 88,1 88,0 87,9 87,7 87,6

30 86 87,0 87,6 87,5 87,4 87,3 87,2 87,0 87,3 86,9
35 95 86,8 87,0 86,7 86,7 86,5 86,4 86,0 86,0
40 104 85,5 85,6 85,8 85,7 85,7 85,6

45 113 84,1 84,3 84,4 84,8 84,6
50 122 82,7 83,0 83,1 83,9

OAT

Pressure Altitude

°C °F -1000 0 2000 4000 6000 8000 10000 12000 14000

-45 -49 81,3 82,3

-40 -40 76,1 76,7 77,4 78,3 78,9 79,7 80,8 82,1 83,0

-35 -31 76,9 77,4 78,3 79,1 79,7 80,6 81,6 83,0 84,0

-30 -22 77,7 78,2 79,1 79,9 80,6 81,3 82,4 83,8 84,8

-25 -13 78,5 79,0 79,8 80,7 81,4 82,1 83,2 84,6 85,6

-20 -4 79,2 79,8 80,6 81,5 82,2 82,9 84,0 85,4 86,4

-15 5 80,0 80,5 81,4 81,8 83,0 83,7 84,8 86,2 87,2

-10 14 80,7 81,3 82,1 83,0 83,7 84,6 85,6 87,0 88,0

-5 23 81,5 82,1 83,1 83,8 84,5 85,3 86,4 87,8 88,7
0 32 82,2 82,8 83,6 84,6 85,4 86,1 87,3 88,6 89,6

5 41 82,9 83,5 84,4 85,4 86,0 87,0 88,1 89,7 90,0

10 50 83,7 84,2 85,1 86,1 86,8 88,0 89,6 89,5 89,3

15 59 84,3 84,9 85,9 86,8 87,9 88,9 88,8 88,6 88,3
20 68 85,0 85,6 86,6 87,7 88,4 88,2 87,8 87,8 87,6

25 77 85,8 86,4 87,3 87,6 87,5 87,4 87,3 87,0 86,8
30 86 86,5 87,2 87,0 86,8 86,6 86,5 86,2 86,6 86,1

35 95 86,2 86,5 86,3 86,0 85,8 85,6 85,2 85,1
40 104 84,9 85,1 85,2 85,1 84,9 84,7

45 113 83,5 83,7 83,7 84,2 83,8
50 122 82,1 82,3 82,3 83,2

OAT

Pressure Altitude

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-68

02-May-2017

PACKS ON, COWL ANTI ICE ON

PACKS ON, COWL & WING ANTI ICE ON

°C °F -1000 0 2000 4000 6000 8000 10000 12000 14000

-45 -49 81,2 82,1

-40 -40 75,9 76,4 77,2 78,0 78,7 79,6 80,6 82,1 82,9

-35 -31 76,9 77,1 78,1 79,0 79,5 80,4 81,4 83,0 83,7

-30 -22 77,5 77,9 78,8 79,7 80,5 81,2 82,3 83,8 84,5

-25 -13 78,3 78,7 79,6 80,5 81,3 82,0 83,1 84,6 85,3

-20 -4 79,1 79,5 80,4 81,3 82,1 82,8 83,9 85,4 86,1

-15 5 79,9 80,2 81,2 82,1 82,9 83,6 84,7 86,3 86,9

-10 14 80,5 81,0 81,4 82,9 83,5 84,4 85,5 87,0 87,7

-5 23 81,3 81,8 82,6 83,6 84,3 85,1 86,3 87,7 88,3
0 32 82,0 82,5 83,4 84,4 85,2 85,9 87,1 88,5 89,4

5 41 82,8 83,2 84,1 85,1 85,8 86,8 88,3 89,3 89,4

10 50 83,5 84,0 84,9 85,9 86,7 88,0 88,8 88,7 88,1

OAT

Pressure Altitude

°C °F -1000 0 2000 4000 6000 8000 10000 12000 14000

-45 -49 81,2 82,1

-40 -40 75,9 76,4 77,2 78,0 78,9 79,6 80,6 82,1 82,9

-35 -31 76,7 77,1 78,1 79,0 79,5 80,4 81,4 83,0 83,7

-30 -22 77,5 77,9 78,8 79,7 80,5 81,2 82,3 83,8 84,5

-25 -13 78,3 78,7 79,6 80,5 81,3 82,0 83,1 84,6 85,3

-20 -4 79,1 79,5 80,4 81,3 82,1 82,8 83,9 85,4 86,1

-15 5 79,9 80,2 81,2 82,1 82,9 83,6 84,7 86,5 87,1

-10 14 80,5 81,0 81,8 82,9 83,5 84,4 86,2 87,1 87,5

-5 23 81,3 81,8 82,6 83,6 84,3 85,7 87,2 86,5 86,0
0 32 82,0 82,5 83,4 84,4 85,6 86,9 86,3 85,6 83,8

5 41 82,8 83,2 84,1 85,2 86,9 86,3 85,4 84,9 81,1

10 50 83,5 84,0 84,7 86,3 86,0 85,6 84,8 84,0 80,7

OAT

Pressure Altitude

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-69

02-May-2017

MAXIMUM CONTIN UOUS THRUST (ONE ENGINE IN OPERATIVE), %N1 – 170KIAS

PACKS ON, ANTI ICE OFF

PACKS ON, COWL ANTI ICE ON

°C 0 5000 10000 15000 20000 25000 30000 35000 41000

-70 -94 85,5 85,8 85,5

-65 -85 85,8 86,4 86,7 86,3

-60 -76 85,2 86,7 87,3 87,6 87,2

-55 -67 86,1 87,5 88,2 88,4 88,1

-50 -58 85,0 87,0 88,4 89,1 89,2 88,9

-45 -49 83,7 85,9 87,8 89,2 89,9 90,0 89,3

-40 -40 80,4 82,5 84,6 86,8 88,7 90,1 90,8 90,8 88,8

-35 -31 81,2 83,3 85,4 87,6 89,5 90,9 91,8 90,3 88,2

-30 -22 82,0 84,2 86,3 88,4 90,3 91,8 92,0 89,6 87,4

-25 -13 82,8 85,0 87,1 89,2 91,2 92,6 91,4 89,0 86,6

-20 -4 83,6 85,8 87,9 90,1 92,0 92,3 90,7 88,3 85,6

-15 5 84,4 86,6 88,7 90,9 92,8 91,6 90,1 87,6

-10 14 85,2 87,4 89,5 91,7 92,2 91,0 89,5 86,8

-5 23 86,0 88,2 90,3 92,4 91,7 90,4 88,6
0 32 86,8 89,0 91,1 92,0 91,1 89,8 87,6

5 41 87,5 89,7 91,9 91,4 90,6 89,2

10 50 88,3 90,5 91,4 90,9 89,9 88,6
15 59 89,0 91,3 90,9 90,2 89,3

20 68 89,7 90,7 90,2 89,6 88,7
25 77 90,5 90,0 89,5 88,9

30 86 89,7 89,2 88,7 88,2
35 95 88,7 88,4 87,9 87,4

40 104 87,4 87,8 87,0
45 113 86,0 86,7 86,2

50 122 84,7 85,8

SAT

Pressure Altitude

°C 0 5000 10000 15000 20000 25000 30000

-70 -94

-65 -85 85,8 86,4

-60 -76 85,2 86,7 87,3

-55 -67 86,1 87,5 88,2

-50 -58 85,0 87,0 88,4 89,1

-45 -49 83,7 85,9 87,8 89,2 89,9

-40 -40 80,4 82,5 84,6 86,8 88,7 90,1 90,8

-35 -31 81,2 83,3 85,4 87,8 89,5 90,9 91,1

-30 -22 82,0 84,2 86,3 88,4 90,3 91,8 90,4

-25 -13 82,8 85,0 87,1 89,2 91,2 91,7 89,8

-20 -4 83,6 85,8 87,9 90,1 92,0 91,1 89,2

-15 5 84,4 86,6 88,7 90,9 92,0 90,5 88,7

-10 14 85,2 87,4 89,5 91,7 91,5 89,9 88,2

-5 23 86,0 88,2 90,3 91,9 90,9 89,3 87,6

0 32 86,8 89,0 91,1 91,3 90,3 88,7 86,8
5 41 87,5 89,7 91,4 90,8 89,8 88,2

10 50 88,3 90,5 90,9 90,2 89,2 87,0

SAT

Pressure Altitude

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-70

02-May-2017

PACKS ON, WING AND COWL ANTI ICE ON

MAXIMUM CONTINUOUS THR UST (ON E ENGINE IN OPERATIVE), %N1 – 230 KIAS

ENGINE PACKS ON, ANTI ICE OFF

°C 0 5000 10000 15000 20000 25000 30000

-70 -94

-65 -85 85,3 84,0

-60 -76 84,8 86,2 83,9

-55 -67 85,7 86,2 83,8

-50 -58 85,0 86,5 85,7 83,6

-45 -49 82,7 85,9 87,4 85,3 83,5

-40 -40 80,4 82,5 84,6 86,8 88,2 84,7 83,3

-35 -31 81,2 83,3 85,4 87,6 87,6 84,2 83,0

-30 -22 82,0 84,2 86,3 88,4 87,1 83,9 82,6

-25 -13 82,8 85,0 87,1 89,2 86,6 83,6 82,2

-20 -4 83,8 85,8 87,9 89,5 86,0 83,0 81,8

-15 5 84,4 86,6 88,7 88,8 85,4 82,3 81,3

-10 14 85,2 87,4 89,1 86,6 84,3 81,7 81,0

-5 23 86,0 88,2 88,7 85,1 83,1 81,0 80,6

0 32 86,8 89,0 88,3 84,3 81,9 80,7 80,2
5 41 87,5 88,4 87,8 83,6 81,1 80,3

10 50 88,2 87,8 87,3 82,9 80,7 79,9

SAT

Pressure Altitude

°C 0 5000 10000 15000 20000 25000 30000

-70 -94

-65 -85 85,3 84,0

-60 -76 84,8 86,2 83,9

-55 -67 85,7 86,2 83,8

-50 -58 85,0 86,5 85,7 83,6

-45 -49 82,7 85,9 87,4 85,3 83,5

-40 -40 80,4 82,5 84,6 86,8 88,2 84,7 83,3

-35 -31 81,2 83,3 85,4 87,6 87,6 84,2 83,0

-30 -22 82,0 84,2 86,3 88,4 87,1 83,9 82,6

-25 -13 82,8 85,0 87,1 89,2 86,6 83,6 82,2

-20 -4 83,8 85,8 87,9 89,5 86,0 83,0 81,8

-15 5 84,4 86,6 88,7 88,8 85,4 82,3 81,3

-10 14 85,2 87,4 89,1 86,6 84,3 81,7 81,0

-5 23 86,0 88,2 88,7 85,1 83,1 81,0 80,6

0 32 86,8 89,0 88,3 84,3 81,9 80,7 80,2
5 41 87,5 88,4 87,8 83,6 81,1 80,3

10 50 88,2 87,8 87,3 82,9 80,7 79,9

SAT

Pressure Altitude

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-71

02-May-2017

PACKS ON, COWL ANTI ICE ON

PACKS ON, COWL & WING ANTI ICE ON

°C 0 5000 10000 15000 20000 25000 30000

-70 -94

-65 -85 85,4 86,7

-60 -76 84,8 86,3 87,6

-55 -67 85,7 87,2 88,5

-50 -58 84,8 86,6 88,1 89,4

-45 -49 83,7 85,7 87,5 88,9 90,3

-40 -40 80,2 82,4 84,5 86,6 88,3 89,8 91,1

-35 -31 81,0 83,3 85,4 87,4 89,2 90,7 90,7

-30 -22 81,8 84,1 86,2 88,3 90,0 91,5 90,2

-25 -13 82,6 84,9 87,1 89,1 90,9 91,4 89,7

-20 -4 83,4 85,7 87,9 89,9 91,7 90,9 89,2

-15 5 84,2 86,5 88,7 90,7 91,9 90,4 88,7

-10 14 85,0 87,3 89,5 91,5 91,4 89,9 88,2

-5 23 85,8 88,1 90,3 91,8 90,9 89,4 87,7

0 32 86,5 88,9 91,1 91,3 90,4 88,8 87,2
5 41 87,3 89,7 91,4 90,8 89,8 88,2

10 50 88,0 90,4 90,9 90,2 89,2 87,6

SAT

Pressure Altitude

°C 0 5000 10000 15000 20000 25000 30000

-70 -94

-65 -85 84,9 84,4

-60 -76 84,6 85,8 84,1

-55 -67 85,5 86,7 84,0

-50 -58 84,8 86,4 86,5 83,9

-45 -49 83,7 85,7 87,3 86,1 83,7

-40 -40 80,2 82,4 84,5 86,8 88,1 85,6 83,5

-35 -31 81,0 83,3 85,4 87,4 88,6 85,1 83,3

-30 -22 81,8 84,1 86,2 88,3 87,8 84,6 82,9

-25 -13 82,6 84,9 87,1 89,1 87,2 84,1 82,6

-20 -4 83,4 85,7 87,9 89,5 86,6 83,3 82,2

-15 5 84,2 86,5 88,7 89,2 86,1 82,6 81,8

-10 14 85,0 87,3 89,1 88,9 85,0 82,0 81,4

-5 23 85,8 88,1 88,8 87,8 83,9 81,4 81,1

0 32 86,5 88,9 88,4 85,7 82,7 81,0 80,7
5 41 87,3 88,8 87,9 84,1 81,5 80,6

10 50 88,0 88,0 87,4 83,4 80,9 80,2

SAT

Pressure Altitude

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-72

02-May-2017

V2 GO-AROUND SPEEDS, FLAPS 8

Weight

[lbs]

Weight

[kg]

V

2GA

[KIAS]

50‘000

22‘680

133*

52‘000

23‘000

133*

54‘000

24‘000

133*

57‘000

25‘000

133*

58‘000

26‘000

133*

60‘000

27‘000

136*

62*000

28‘000

138*

64‘000

28‘000

140

66‘000

29‘000

143

68‘000

30‘000

145

70‘000

31‘000

147

72‘000

32‘000

149

74‘000

33‘000

152

76‘000

34‘000

154

78‘000

35‘000

156

*

For weights less than 28‘000kg and altitudes less than 2‘000ft, use

the V

2GA

presented in the table below

Weight

[lbs]

Weight

[kg]

V

2GA

Sea Level

(KIAS)

V

2GA

1‘000ft
(KIAS)

V

2GA

2‘000ft
(KIAS)

OAT

OAT

OAT

Below

35°C

35°C &

above

Below

35°C

35°C &

above

Below

35°C

35°C &

above

50‘000

22‘680

153

133

143

133

133

133

54‘000

24‘500

144

133

133

133

133

133

57‘000

27‘220

136

133

133

133

133

133

60‘000

27‘220

136

133

133

133

133

133

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-73

02-May-2017

LANDING DATA, LANDING GEAR DOWN, FLAPS 45

Weight

[lbs]

Weight

[kg]

VREF
(KIAS)

Pressure Altitude (x 1‘000ft)

0 2 4 6 8

10

Actual Landing Distance (Meters / Feet)

50‘000

22‘680

125

825
2‘706

861
2‘823

899
2‘950

941
3‘088

990
3‘247

1‘048
3‘438

52‘000

23‘000

125

825
2‘710

861
2‘827

899
2‘954

942
3‘092

990
3‘251

1‘048
3‘443

54‘000

24‘000

125

826
2‘713

862
2‘831

901
2‘958

943
3‘096

992
3‘255

1‘050
3‘447

56‘000

25‘000

125

828
2‘716

864
2‘835

902
2‘962

944
3‘100

993
3‘259

1‘051
3‘450

57‘000

25‘800

125

828
2‘718

864
2‘837

903
2‘965

945
3‘105

994
3‘266

1‘054
3‘465

59‘000

26‘000

125

832
2‘786

868
2‘909

907
3‘041

950
3‘186

999
3‘357

1‘061
3‘568

61‘000

27‘000

128

855
2‘854

892
2‘981

933
3‘117

977
3‘266

1‘031
3‘454

1‘096
3‘671

63‘000

28‘000

130

878
2‘921

917
3‘052

959
3‘192

1‘005
3‘352

1‘064
3‘550

1‘130
3‘772

65‘000

29‘000

132

900
2‘987

940
3‘121

983
3‘265

1‘034
3‘439

1‘095
3‘643

1‘164
3‘872

67‘000

30‘000

135

922
3‘052

963
3‘189

1‘009
3‘344

1‘063
3‘527

1‘127
3‘736

1‘197
3‘971

69‘000

31‘000

137

943
3‘116

986
3‘258

1‘035
3‘424

1‘093
3‘615

1‘158
3‘830

1‘231
4‘072

71‘000

32‘000

139

965
3‘181

1‘010
3‘331

1‘063
3‘506

1‘122
3‘702

1‘189
3‘923

1‘266
4‘177

73‘000

33‘000

141

987
3‘245

1‘035
3‘406

1‘091
3‘589

1‘152
3‘790

1‘221
4‘017

1‘302
4‘285

75‘000

34‘000

143

1‘009
3‘313

1‘061
3‘482

1‘118
3‘671

1‘181
3‘877

1‘253
4‘112

1‘339
4‘395

77‘000

35‘000

145

1‘034
3‘386

1‘088
3‘562

1‘147
3‘756

1‘212
3‘969

1‘287
4‘215

1‘378
4‘511

V

REF

= speed at 50 ft screen heigth (KIAS), Flaps 45°

Actual Landing Distance = Dry Landing Field Length x 0,6

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-74

02-May-2017

LANDING DATA, LANDING WITH FLA PS OTHER THAN FLAPS 45

Weight

[lbs]

Weight

[kg]

Flap Setting (degrees)

0 1 8

20

30

V

ref

(KIAS)

50‘000

22‘680

165

149

143

137

133

52‘000

23‘000

165

149

143

137

133

54‘000

24‘000

165

149

143

137

133

56‘000

25‘000

165

149

143

137

133

57‘000

25‘800

165

149

143

137

133

59‘000

26‘000

165

149

143

137

133

61‘000

27‘000

168

152

146

140

136

63‘000

28‘000

170

154

148

142

138

65‘000

29‘000

172

156

150

144

140

67‘000

30‘000

175

159

153

147

143

69‘000

31‘000

177

161

155

149

145

71‘000

32‘000

179

163

157

151

147

73‘000

33‘000

181

165

159

153

149

75‘000

34‘000

183

167

161

155

151

77‘000

35‘000

185

169

163

157

153

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-75

02-May-2017

FLIG HT PLANNING

CLI MB (FL-050 T O FL-190)

53 55 57 60 62 64 66 68 71 73 75 77

24 25 26 27 28 29 30 31 32 33 34 35
Min. 5,2 5,5 5,8 6,1 6,4 6,6 6,9 7,2 7,5 7,9 8,1 8,5
nm 28,0 29,4 30,9 32,4 33,9 35,4 37,0 38,7 40,3 42,1 43,8 45,8
kg 279 293 308 322 337 352 368 384 400 417 435 452
lbs 615 646 679 710 743 776 811 847 882 919 959 996
Min. 4,9 5,1 5,4 5,7 5,9 6,2 6,4 6,7 7 7,3 7,6 7,9
nm 25,8 27,1 28,5 29,9 31,3 32,7 34,1 35,6 37,1 38,8 40,4 42,1
kg. 263 276 289 303 317 331 346 361 376 392 408 425
lbs 580 608 637 668 699 730 763 796 829 864 899 937
Min. 4,5 4,8 5 5,2 5,5 5,7 6 6,2 6,5 6,8 7 7,4
nm 23,7 24,9 26,1 27,3 28,6 29,9 31,2 32,6 34 35,4 36,9 38,5
kg 246 258 271 283 296 310 323 337 351 366 382 397
lbs 542 569 597 624 653 683 712 743 774 807 842 875
Min. 4,2 4,4 4,6 4,8 5 5,3 5,5 5,7 6 6,2 6,5 6,8
nm 21,5 22,6 23,7 24,8 26 27,2 28,3 29,5 30,8 32,1 33,5 34,8
kg. 230 241 252 264 276 289 301 314 327 341 355 370
lbs 507 531 556 582 608 637 664 692 721 752 783 816
Min. 3,8 4 4,2 4,4 4,6 4,8 5 5,2 5,5 5,7 5,9 6,2
nm 19,3 20,3 21,3 22,3 23,3 24,4 25,4 26,5 27,6 28,8 30 31,2
kg 213 223 234 245 256 268 279 291 303 316 329 342
lbs 470 492 516 540 564 591 615 642 668 697 725 754
Min. 3,4 3,6 3,8 4 4,2 4,4 4,5 4,7 5 5,2 5,3 5,6
nm 17,3 18,2 19,1 20 20,8 21,8 22,7 23,7 24,7 25,8 26,8 27,9
kg. 194,2 203,2 213,2 223,2 233,4 244,2 254,2 265,2 276,2 288 299,8 311,6
lbs 428 448 470 492 515 538 560 585 609 635 661 687
Min. 3,1 3,2 3,4 3,6 3,8 3,9 4,1 4,2 4,5 4,6 4,8 5
nm 15,3 16 16,8 17,6 18,4 19,2 20,1 20,9 21,8 22,7 23,7 24,6
kg 175,4 183,4 192,4 201,4 210,8 220,4 229,4 239,4 249,4 260 270,6 281,2
lbs 387 404 424 444 465 486 506 528 550 573 597 620
Min. 2,7 2,9 3 3,1 3,3 3,5 3,6 3,8 3,9 4,1 4,2 4,5
nm 13,2 13,9 14,6 15,3 15,9 16,7 17,4 18,2 18,9 19,7 20,5 21,4
kg. 156,6 163,6 171,6 179,6 188,2 196,6 204,6 213,6 222,6 232 241,4 250,8
lbs 345 361 378 396 415 433 451 471 491 511 532 553
Min. 2,4 2,5 2,6 2,7 2,9 3 3,2 3,3 3,4 3,5 3,7 3,9
nm 11,2 11,7 12,3 12,9 13,5 14,1 14,8 15,4 16 16,6 17,4 18,1
kg 137,8 143,8 150,8 157,8 165,6 172,8 179,8 187,8 195,8 204 212,2 220,4
lbs 304 317 332 348 365 381 396 414 432 450 468 486
Min. 2 2,1 2,2 2,3 2,5 2,6 2,7 2,8 2,9 3 3,1 3,3
nm 9,2 9,6 10,1 10,6 11 11,5 12,1 12,6 13,1 13,6 14,2 14,8
kg. 119 124 130 136 143 149 155 162 169 176 183 190
lbs 262 273 287 300 315 328 342 357 373 388 403 419
Min. 0,8 0,8 0,9 0,9 1 1 1 1,1 1,1 1,2 1,2 1,3
nm 3,5 3,6 3,8 4 4,2 4,4 4,5 4,7 4,9 5,1 5,3 5,6
kg 49 51 54 56 59 61 64 66 69 72 75 78
lbs 108 112 119 123 130 134 141 146 152 159 165 172

140

150

160

170

Flight Level

Weight [t]

190

180

50

100

110

120

130

Weight [1,000 lbs]

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-76

02-May-2017

CLI MB (FL-200 T O FL-290)

53 55 57 60 62 64 66 68 71 73 75 77

24 25 26 27 28 29 30 31 32 33 34 35
Min. 9,8 10,3 10,9 11,4 12 12,5 13,1 13,8 14,4 15,1 15,8 16,6
nm 59,5 62,6 65,9 69,3 72,8 76,3 80,0 83,3 87,9 92,2 96,7 101,5
kg 468 493 518 544 570 597 625 655 685 717 751 786
lbs 1032 1087 1142 1199 1257 1316 1378 1444 1510 1581 1656 1733
Min. 9,3 9,8 10,3 10,8 11,4 11,9 12,4 13 13,6 14,3 14,9 15,7
nm 55,7 58,7 61,7 64,9 68,1 71,4 74,8 78 82 86 90,1 94,5
kg. 449 472 496 521 546 571 598 626 655 685 717 750
lbs 990 1041 1093 1149 1204 1259 1318 1380 1444 1510 1581 1653
Min. 8,8 9,2 9,7 10,2 10,7 11,2 11,7 12,2 12,8 13,4 14 14,7
nm 51,9 54,7 57,5 60,4 63,3 66,4 69,5 72,7 76,1 79,7 83,5 87,4
kg 429 451 474 497 521 545 571 596 624 652 682 713
lbs 946 994 1045 1096 1149 1202 1259 1314 1376 1437 1504 1572
Min. 8,3 8,7 9,1 9,6 10,1 10,5 11 11,5 12 12,6 13,1 13,8
nm 48,3 50,9 53,4 56,1 58,8 61,6 64,5 67,5 70,6 73,9 77,3 80,9
kg. 409 430 451 473 496 519 543 567 593 619 647 676
lbs 902 948 994 1043 1093 1144 1197 1250 1307 1365 1426 1490
Min. 7,7 8,1 8,5 9 9,4 9,8 10,3 10,7 11,2 11,7 12,2 12,8
nm 44,6 47 49,3 51,8 54,3 56,8 59,5 62,2 65 68 71 74,3
kg 388 408 428 449 470 492 514 537 561 586 612 639
lbs 855 899 944 990 1036 1085 1133 1184 1237 1292 1349 1409
Min. 7,3 7,7 8 8,5 8,9 9,3 9,7 10,1 10,6 11 11,5 12,1
nm 41,7 43,9 46,1 48,4 50,8 53,1 55,6 58,1 60,7 63,5 66,3 69,3
kg. 370 389 408 427 447 468 489 511 534 557 582 607
lbs 816 858 899 941 985 1032 1078 1127 1177 1228 1283 1338
Min. 6,9 7,2 7,6 8 8,4 8,7 9,1 9,5 9,9 10,4 10,8 11,3
nm 38,8 40,9 42,9 45 47,2 49,4 51,7 54 56,4 59 61,5 64,3
kg 351 369 387 406 425 444 464 485 506 528 552 575
lbs 774 814 853 895 937 979 1023 1069 1116 1164 1217 1268
Min. 6,4 6,8 7,1 7,5 7,8 8,2 8,6 8,9 9,3 9,7 10,1 10,6
nm 36 37,8 39,7 41,7 43,7 45,6 47,7 49,9 52,1 54,4 56,8 59,4
kg. 333 350 367 384 402 421 440 459 479 500 521 544
lbs 734 772 809 847 886 928 970 1012 1056 1102 1149 1199
Min. 6 6,3 6,7 7 7,3 7,6 8 8,3 8,6 9,1 9,4 9,8
nm 33,1 34,8 36,5 38,3 40,1 41,9 43,8 45,8 47,8 49,9 52 54,4
kg 314 330 346 363 380 397 415 433 451 471 491 512
lbs 692 728 763 800 838 875 915 955 994 1038 1082 1129
Min. 5,6 5,9 6,2 6,5 6,8 7,1 7,4 7,7 8 8,4 8,7 9,1
nm 30,2 31,7 33,3 34,9 36,6 38,2 39,9 41,7 43,5 45,4 47,3 49,4
kg. 296 311 326 341 357 373 390 407 424 442 461 480
lbs 653 686 719 752 787 822 860 897 935 974 1016 1058

210

200

Flight Level

Weight [t]

290

280

270

260

250

240

230

220

Weight [1,000lbs]

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-77

02-May-2017

CLI MB (FL-300 T O FL-390)

53 55 57 60 62 64 66 68 71 73 75 77

24 25 26 27 28 29 30 31 32 33 34 35

Min. 15,6 16,5 17,5 18,6 19,8 21 22,5 24,1 26 28,4 31,6 36,6
nm 100,6 106,8 113,5 120,6 128,4 136,9 146,4 157,4 170,6 187,0 209,0 244,1
kg 646 683 723 764 809 857 909 967 1035 1116 1219 1371
lbs 1424 1506 1594 1684 1784 1889 2004 2132 2282 2460 2687 3023
Min. 14,8 15,7 16,6 17,6 18,6 19,7 21 22,4 23,9 25,8 28,2 31,6
nm 95 100,7 106,8 112,8 120,1 127,6 135,8 145 155,7 168,5 184,7 208,2
kg 624,5 660 697,5 736,5 778 822 869 920,5 979 1046 1127,5 1236,5
lbs 1377 1455 1538 1624 1715 1812 1916 2029 2158 2306 2486 2726
Min. 14 14,8 15,6 16,5 17,4 18,4 19,4 20,6 21,8 23,2 24,7 26,5
nm 89,3 94,6 100 105 111,8 118,3 125,2 132,6 140,8 150 160,3 172,2
kg 603 637 672 709 747 787 829 874 923 976 1036 1102
lbs 1329 1404 1482 1563 1647 1735 1828 1927 2035 2152 2284 2429
Min. 13,4 14,1 14,9 15,7 16,6 17,5 18,4 19,5 20,6 21,8 23,2 24,7
nm 84,9 89,9 94,9 99,9 105,9 111,8 118,1 124,8 132,2 140,2 149,2 159,2
kg 585 618 651 686 722 760 800 842 887 936 990 1049
lbs 1290 1362 1435 1512 1592 1676 1764 1856 1956 2064 2183 2313
Min. 12,7 13,4 14,2 14,9 15,7 16,6 17,4 18,4 19,4 20,4 21,6 22,8
nm 80,5 85,1 89,8 94,8 100 105,3 111 117 123,5 130,4 138 146,2
kg 567 598 630 663 697 733 770 809 851 896 943 995
lbs 1250 1318 1389 1462 1537 1616 1698 1784 1876 1975 2079 2194
Min. 12,2 12,9 13,6 14,3 15,1 15,9 16,7 17,6 18,5 19,4 20,5 21,6
nm 76,8 81,1 85,5 90,2 95 100 105,3 110,9 116,9 123,2 130,1 137,5
kg 551 580 611 643 675 710 745 782 822 864 908 956
lbs 1215 1279 1347 1418 1488 1565 1642 1724 1812 1905 2002 2108
Min. 11,7 12,3 13 13,7 14,4 15,1 15,9 16,7 17,5 18,4 19,3 20,4
nm 73 77,1 81,2 85,5 90 94,7 99,6 104,8 110,2 116 122,2 128,8
kg 534 562 592 622 653 686 720 755 792 832 873 917
lbs 1177 1239 1305 1371 1440 1512 1587 1664 1746 1834 1925 2022
Min. 11,2 11,8 12,5 13,1 13,8 14,5 15,2 15,9 16,7 17,6 18,4 19,4
nm 69,6 73,4 77,3 81,4 85,6 90 94,5 99,4 104,4 109,8 115,5 121,6
kg 518 545 574 603 633 664 696 730 765 803 842 884
lbs 1142 1202 1265 1329 1396 1464 1534 1609 1687 1770 1856 1949
Min. 10,7 11,3 11,9 12,5 13,1 13,8 14,4 15,1 15,9 16,7 17,5 18,4
nm 66,1 69,7 73,4 77,2 81,1 85,2 89,4 93,9 98,6 103,6 108,8 114,4
kg 501 528 555 583 612 641 672 704 738 773 811 850
lbs 1105 1164 1224 1285 1349 1413 1482 1552 1627 1704 1788 1874
Min. 10,3 10,8 11,4 12 12,6 13,2 13,8 14,5 15,2 15,9 16,7 17,5
nm 62,8 66,2 69,7 73,3 77 80,8 84,7 88,6 93,3 97,9 102,8 108
kg 485 511 537 564 591 619 649 680 712 745 781 818
lbs 1069 1127 1184 1243 1303 1365 1431 1499 1570 1642 1722 1803

330

320

310

Weight [1,000lbs]

300

Flight Level

390

370

380

360

350

340

Weight [t]

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-78

02-May-2017

CRUISE (FL-100 TO FL-240)

53 55 57 60 62 64 66 68 71 73 75 77

24 25 26 27 28 29 30 31 32 33 34 35

nm/hr 425 425 425 425 425 425 425 425 425 425 425 425

kg/hr/engine 817 823 829 835 842 848 854 861 868 875 883 892

lbs/hr/engine 1801 1814 1828 1841 1856 1870 1883 1898 1914 1929 1947 1967

nm/hr 418 418 418 418 418 418 418 418 418 418 418 418

kg/hr/engine 819 824 831 837 843 850 856 862 869 876 884 893

lbs/hr/engine 1806 1817 1832 1845 1858 1874 1887 1900 1916 1931 1949 1969

nm/hr 412 412 412 412 412 412 412 412 412 412 412 412

kg/hr/engine 820 826 832 838 844 851 857 864 871 878 885 894

lbs/hr/engine 1808 1821 1834 1847 1861 1876 1889 1905 1920 1936 1951 1971

nm/hr 406 406 406 406 406 406 406 406 406 406 406 406

kg/hr/engine 822 828 833 839 846 852 858 865 872 879 887 895

lbs/hr/engine 1812 1825 1836 1850 1865 1878 1892 1907 1922 1938 1956 1973

nm/hr 400 400 400 400 400 400 400 400 400 400 400 400

kg/hr/engine 824 829 835 841 847 853 860 866 873 880 888 895

lbs/hr/engine 1817 1828 1841 1854 1867 1881 1896 1909 1925 1940 1958 1973

nm/hr 394 394 394 394 394 394 394 394 394 394 394 394

kg/hr/engine 826 832 838 844 850 856 862 869 876 883 890 898

lbs/hr/engine 1821 1834 1847 1861 1874 1887 1900 1916 1931 1947 1962 1980

nm/hr 388 388 388 388 388 388 388 388 388 388 388 388

kg/hr/engine 829 834 840 846 852 858 865 871 878 885 892 900

lbs/hr/engine 1828 1839 1852 1865 1878 1892 1907 1920 1936 1951 1967 1984

nm/hr 382 382 382 382 382 382 382 382 382 382 382 382

kg/hr/engine 831 836 842 848 854 861 867 873 880 887 894 902

lbs/hr/engine 1832 1843 1856 1870 1883 1898 1911 1925 1940 1956 1971 1989

nm/hr 377 377 377 377 377 377 377 377 377 377 377 377

kg/hr/engine 833 838 844 850 856 863 869 875 882 889 896 904

lbs/hr/engine 1836 1847 1861 1874 1887 1903 1916 1929 1944 1960 1975 1993

nm/hr 371 371 371 371 371 371 371 371 371 371 371 371

kg/hr/engine 833 839 845 851 858 864 870 877 883 890 897 905

lbs/hr/engine 1836 1850 1863 1876 1892 1905 1918 1933 1947 1962 1978 1995

nm/hr 366 366 366 366 366 366 366 366 366 366 366 366

kg/hr/engine 835 841 847 853 860 866 872 879 885 892 899 907

lbs/hr/engine 1841 1854 1867 1881 1896 1909 1922 1938 1951 1967 1982 2000

nm/hr 360 360 360 360 360 360 360 360 360 360 360 360

kg/hr/engine 837 842 849 855 861 868 874 881 887 894 901 908

lbs/hr/engine 1845 1856 1872 1885 1898 1914 1927 1942 1956 1971 1986 2002

nm/hr 355 355 355 355 355 355 355 355 355 355 355 355

kg/hr/engine 838 843 850 856 862 869 875 882 888 895 902 909

lbs/hr/engine 1847 1858 1874 1887 1900 1916 1929 1944 1958 1973 1989 2004

nm/hr 350 350 350 350 350 350 350 350 350 350 350 350

kg/hr/engine 838 844 850 857 863 870 876 883 889 896 903 910

lbs/hr/engine 1847 1861 1874 1889 1903 1918 1931 1947 1960 1975 1991 2006

nm/hr 345 345 345 345 345 345 345 345 345 345 345 345

kg/hr/engine 839 845 851 857 864 870 877 883 890 896 903 910

lbs/hr/engine 1850 1863 1876 1889 1905 1918 1933 1947 1962 1975 1991 2006

Flight Level

190

200

210

220

230

240

Weight [t]

100

110

120

130

140

150

160

170

180

Weight [1,000lbs]

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-79

02-May-2017

CRUISE (FL-250 TO FL-390)

53 55 57 60 62 64 66 68 71 73 75 77

24 25 26 27 28 29 30 31 32 33 34 35

nm/hr 424 424 424 424 424 424 424 424 424

kg/hr/engine 577 586 597 609 623 639 665 676 697

lbs/hr/engine 1272 1292 1316 1343 1373 1409 1466 1490 1537

nm/hr 424 424 424 424 424 424 424 424 424

kg/hr/engine 593 601 610 621 633 646 665 678 696

lbs/hr/engine 1307 1325 1345 1369 1396 1424 1466 1495 1534

nm/hr 424 424 424 424 424 424 424 424 424 424 424 424

kg/hr/engine 608 615 623 632 642 653 665 679 695 711 730 752

lbs/hr/engine 1340 1356 1373 1393 1415 1440 1466 1497 1532 1567 1609 1658

nm/hr 425 425 425 425 425 425 425 425 425 425 425 425

kg/hr/engine 624 632 639 648 656 666 677 690 703 718 734 753

lbs/hr/engine 1376 1393 1409 1429 1446 1468 1493 1521 1550 1583 1618 1660

nm/hr 426 426 426 426 426 426 426 426 426 426 426 426

kg/hr/engine 640 648 655 663 670 679 689 700 711 724 738 754

lbs/hr/engine 1411 1429 1444 1462 1477 1497 1519 1543 1567 1596 1627 1662

nm/hr 428 428 428 428 428 428 428 428 428 428 428 428

kg/hr/engine 659 666 673 681 689 697 706 716 726 738 750 764

lbs/hr/engine 1453 1468 1484 1501 1519 1537 1556 1579 1601 1627 1653 1684

nm/hr 430 430 430 430 430 430 430 430 430 430 430 430

kg/hr/engine 677 684 691 699 707 715 723 731 740 751 762 774

lbs/hr/engine 1493 1508 1523 1541 1559 1576 1594 1612 1631 1656 1680 1706

nm/hr 432 432 432 432 432 432 432 432 432 432 432 432

kg/hr/engine 698 704 711 718 726 734 742 750 759 769 778 789

lbs/hr/engine 1539 1552 1567 1583 1601 1618 1636 1653 1673 1695 1715 1739

nm/hr 434 434 434 434 434 434 434 434 434 434 434 434

kg/hr/engine 718 724 730 737 744 752 761 769 778 786 794 804

lbs/hr/engine 1583 1596 1609 1625 1640 1658 1678 1695 1715 1733 1750 1773

nm/hr 436 436 436 436 436 436 436 436 436 436 436 436

kg/hr/engine 741 747 753 759 766 773 781 789 798 807 815 824

lbs/hr/engine 1634 1647 1660 1673 1689 1704 1722 1739 1759 1779 1797 1817

nm/hr 438 438 438 438 438 438 438 438 438 438 438 438

kg/hr/engine 763 769 775 781 787 794 801 809 818 827 835 844

lbs/hr/engine 1682 1695 1709 1722 1735 1750 1766 1784 1803 1823 1841 1861

nm/hr 440 440 440 440 440 440 440 440 440 440 440 440

kg/hr/engine 788 794 800 806 812 818 825 832 840 849 857 866

lbs/hr/engine 1737 1750 1764 1777 1790 1803 1819 1834 1852 1872 1889 1909

nm/hr 441 441 441 441 441 441 441 441 441 441 441 441

kg/hr/engine 812 818 824 830 836 842 848 855 862 870 878 887

lbs/hr/engine 1790 1803 1817 1830 1843 1856 1870 1885 1900 1918 1936 1956

nm/hr 438 438 438 438 438 438 438 438 438 438 438 438

kg/hr/engine 819 825 831 837 843 849 855 862 869 876 885 893

lbs/hr/engine 1806 1819 1832 1845 1858 1872 1885 1900 1916 1931 1951 1969

nm/hr 431 431 431 431 431 431 431 431 431 431 431 431

kg/hr/engine 816 822 828 834 840 847 853 859 866 874 882 891

lbs/hr/engine 1799 1812 1825 1839 1852 1867 1881 1894 1909 1927 1944 1964

390

380

370

360

350

Weight [t]

250

Flight Level

340

330

320

310

300

290

280

270

260

Weight [1,000lbs]

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-80

02-May-2017

DESCENT (FL-050 TO FL-190)

53 55 57 60 62 64 66 68 71 73 75 77

24 25 26 27 28 29 30 31 32 33 34 35

Min. 7,9 8,1 8,3 8,5 8,7 8,9 9,1 9,3 9,5 9,6 9,8 9,9
nm 40,0 41,2 42,3 43,4 44,5 45,5 46,5 47,4 48,3 49,1 50,0 50,7
kg 60 61 63 65 66 68 69 71 72 73 74 75
lbs 132 134 139 143 146 150 152 157 159 161 163 165
Min. 7,5 7,7 7,9 8,2 8,3 8,5 8,7 8,9 9,1 9,2 9,4 9,5
nm 37,9 39,1 40,1 41,2 42,2 43,1 44,1 44,9 45,8 46,5 47,3 48
kg 58 59 61 63 64 65 67 68 69 70 72 72
lbs 128 130 134 139 141 143 148 150 152 154 159 159
Min. 7,2 7,4 7,6 7,8 8 8,2 8,3 8,5 8,6 8,7 8,9 9
nm 35,9 36,9 38 38,9 39,9 40,8 41,6 42,5 43,2 44 44,7 45,4
kg 56 57 59 60 61 63 64 66 67 68 69 70
lbs 123 126 130 132 134 139 141 146 148 150 152 154
Min. 6,8 7 7,2 7,5 7,6 7,8 7,9 8,1 8,2 8,3 8,5 8,6
nm 33,8 34,8 35,8 36,7 37,6 38,4 39,2 40 40,7 41,4 42 42,7
kg 54 55 57 58 59 60 62 63 64 65 67 67
lbs 119 121 126 128 130 132 137 139 141 143 148 148
Min. 6,5 6,7 6,9 7,1 7,2 7,4 7,5 7,7 7,8 7,9 8,1 8,2
nm 31,8 32,7 33,6 34,5 35,3 36,1 36,8 37,5 38,2 38,8 39,4 40
kg 52 53 55 56 57 58 60 61 62 63 64 64
lbs 115 117 121 123 126 128 132 134 137 139 141 141
Min. 6,1 6,3 6,4 6,6 6,7 6,9 7 7,2 7,3 7,4 7,5 7,6
nm 29,4 30,2 31 31,9 32,6 33,3 33,9 34,6 35,2 35,8 36,3 36,8
kg 49 50 51,8 52,6 53,6 54,6 56,4 57,4 58,2 59,2 60 60,2
lbs 108 110 114 116 118 120 124 127 128 131 132 133
Min. 5,7 5,8 6 6,1 6,2 6,4 6,5 6,7 6,8 6,8 7 7,1
nm 27 27,7 28,5 29,2 29,9 30,5 31,1 31,7 32,2 32,7 33,2 33,7
kg 46 47 48,6 49,2 50,2 51,2 52,8 53,8 54,4 55,4 56 56,4
lbs 101 104 107 108 111 113 116 119 120 122 123 124
Min. 5,2 5,4 5,5 5,7 5,8 5,9 6 6,1 6,2 6,3 6,4 6,5
nm 24,5 25,3 25,9 26,6 27,1 27,7 28,2 28,7 29,3 29,7 30,1 30,5
kg 43 44 45,4 45,8 46,8 47,8 49,2 50,2 50,6 51,6 52 52,6
lbs 95 97 100 101 103 105 108 111 112 114 115 116
Min. 4,8 4,9 5,1 5,2 5,3 5,4 5,5 5,6 5,7 5,7 5,9 6
nm 22,1 22,8 23,4 23,9 24,4 24,9 25,4 25,8 26,3 26,6 27 27,4
kg 40 41 42,2 42,4 43,4 44,4 45,6 46,6 46,8 47,8 48 48,8
lbs 88 90 93 93 96 98 101 103 103 105 106 108
Min. 4,4 4,5 4,6 4,7 4,8 4,9 5 5,1 5,2 5,2 5,3 5,4
nm 19,7 20,3 20,8 21,3 21,7 22,1 22,5 22,9 23,3 23,6 23,9 24,2
kg 37 38 39 39 40 41 42 43 43 44 44 45
lbs 82 84 86 86 88 90 93 95 95 97 97 99
Min. 1,9 1,9 2 2 2,1 2,1 2,1 2,2 2,2 2,2 2,3 2,3
nm 8,1 8,3 8,6 8,7 8,9 9,1 9,3 9,4 9,6 9,7 9,8 10
kg 17 17 18 18 19 19 19 20 20 20 20 21
lbs 37 37 40 40 42 42 42 44 44 44 44 46

140

130

120

110

100

Weight [t]

50

Flight Level

190

180

170

160

150

Weight [1,000lbs]

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-81

02-May-2017

DESCENT (FL-200 TO FL-290)

53 55 57 60 62 64 66 68 71 73 75 77

24 25 26 27 28 29 30 31 32 33 34 35

Min. 11 11,3 11,6 12 12,3 12,5 12,8 13,1 13,3 13,6 13,8 14
nm 61,4 63,3 65,1 66,9 68,6 70,2 71,8 73,4 74,8 76,2 77,5 78,7
kg 77 79 82 84 86 88 90 92 93 95 96 98
lbs 170 174 181 185 190 194 198 203 205 209 212 216
Min. 10,7 11 11,3 11,7 12 12,2 12,5 12,8 13 13,3 13,5 13,7
nm 59,3 61,2 62,9 64,6 66,3 67,9 69,4 70,9 72,3 73,6 74,9 76
kg 76 78 80 82 84 86 88 90 91 93 94 96
lbs 168 172 176 181 185 190 194 198 201 205 207 212
Min. 10,4 10,7 11 11,3 11,6 11,9 12,1 12,4 12,6 12,9 13,1 13,3
nm 57,2 59 60,7 62,3 63,9 65,5 66,9 68,4 69,7 71 72,2 73,3
kg 74 76 78 80 82 84 86 88 89 91 92 94
lbs 163 168 172 176 181 185 190 194 196 201 203 207
Min. 10,1 10,4 10,7 11 11,3 11,5 11,8 12 12,2 12,5 12,7 12,9
nm 55 56,7 58,3 59,9 61,4 62,9 64,3 65,7 67 68,2 69,3 70,4
kg 73 75 77 79 80 82 84 86 87 89 90 92
lbs 161 165 170 174 176 181 185 190 192 196 198 203
Min. 9,8 10,1 10,4 10,6 10,9 11,1 11,4 11,6 11,8 12,1 12,2 12,4
nm 52,8 54,4 55,9 57,4 58,9 60,3 61,6 62,9 64,2 65,3 66,4 67,4
kg 71 73 75 77 78 80 82 84 85 87 88 89
lbs 157 161 165 170 172 176 181 185 187 192 194 196
Min. 9,5 9,8 10 10,3 10,5 10,7 11 11,2 11,4 11,7 11,8 12
nm 50,6 52,2 53,6 55 56,5 57,8 59,1 60,3 61,5 62,6 63,6 64,6
kg 69 71 73 75 76 78 80 82 83 85 86 87
lbs 152 157 161 165 168 172 176 181 183 187 190 192
Min. 9,2 9,4 9,7 9,9 10,2 10,4 10,6 10,8 11 11,3 11,4 11,6
nm 48,5 50 51,3 52,7 54,1 55,3 56,5 57,7 58,8 59,9 60,9 61,8
kg 67 69 71 73 74 76 78 80 81 82 84 85
lbs 148 152 157 161 163 168 172 176 179 181 185 187
Min. 8,8 9,1 9,3 9,6 9,8 10 10,3 10,5 10,7 10,8 11 11,1
nm 46,3 47,7 49,1 50,3 51,6 52,8 54 55,1 56,2 57,1 58,1 59
kg 66 67 69 71 72 74 75 77 78 80 81 82
lbs 146 148 152 157 159 163 165 170 172 176 179 181
Min. 8,5 8,7 9 9,2 9,5 9,7 9,9 10,1 10,3 10,4 10,6 10,7
nm 44,2 45,5 46,8 48 49,2 50,3 51,4 52,5 53,5 54,4 55,4 56,2
kg 64 65 67 69 70 72 73 75 76 77 79 80
lbs 141 143 148 152 154 159 161 165 168 170 174 176
Min. 8,2 8,4 8,6 8,9 9,1 9,3 9,5 9,7 9,9 10 10,2 10,3
nm 42 43,3 44,5 45,6 46,8 47,8 48,9 49,9 50,8 51,7 52,6 53,4
kg 62 63 65 67 68 70 71 73 74 75 77 78
lbs 137 139 143 148 150 154 157 161 163 165 170 172

Flight Level

Weight [t]

240

250

260

270

280

290

200

210

220

230

Weight [1,000lbs]

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2-1-82

02-May-2017

DESCENT (FL-300 TO FL-390)

53 55 57 60 62 64 66 68 71 73 75 77

24 25 26 27 28 29 30 31 32 33 34 35

Min. 17,3 17,3 17,3 17,3 17,3 17,3 17,3 17,3 17,3 17,3 17,4 17,6
nm 106,2 105,7 105,2 104,8 104,4 104,0 103,7 103,3 103,0 102,7 103,4 104,6
kg 164 159 153 148 143 138 133 128 123 118 117 118
lbs 362 351 337 326 315 304 293 282 271 260 258 260
Min. 16,4 16,4 16,4 16,4 16,4 16,4 16,4 16,5 16,6 16,8 17 17,2
nm 99,8 99,3 98,8 98,4 98 97,5 97 97 98 99,4 100,5 101,8
kg 151 145,5 139,5 134,5 129 124 119,5 116 112 113 114,5 116
lbs 333 321 308 297 284 273 263 256 247 249 252 256
Min. 15,5 15,5 15,5 15,5 15,5 15,5 15,6 15,8 16,1 16,3 16,6 16,8
nm 93,3 92,9 92,4 92 91,6 91,2 91,5 92,8 94,5 96,1 97,5 98,9
kg 138 132 126 121 115 110 106 107 108 110 112 114
lbs 304 291 278 267 254 243 234 236 238 243 247 251
Min. 14,5 14,5 14,5 14,5 14,7 14,9 15,1 15,4 15,7 16 16,2 16,5
nm 86,3 85,9 85,4 85 85,8 87 88,6 90,1 91,8 93,4 94,8 96,2
kg 122 116 110 104 100 100 102 104 106 108 110 112
lbs 269 256 243 229 220 220 225 229 234 238 243 247
Min. 13,5 13,5 13,5 13,8 14,1 14,4 14,7 15 15,3 15,6 15,8 16,1
nm 79,2 78,8 78,3 79,8 81,8 83,7 85,6 87,4 89 90,6 92 93,4
kg 105 99 93 94 96 98 100 102 104 106 108 109
lbs 231 218 205 207 212 216 220 225 229 234 238 240
Min. 12,6 12,9 13,2 13,5 13,8 14,1 14,4 14,7 15 15,3 15,5 15,7
nm 74,1 74,5 75,8 77,5 79,5 81,3 83,2 84,9 86,5 88,1 89,5 90,9
kg 94 89 90 92 94 96 98 100 102 104 106 107
lbs 207 196 198 203 207 212 216 220 225 229 234 236
Min. 12 12,4 12,8 13,1 13,4 13,7 14 14,3 14,6 14,9 15,1 15,3
nm 69 71,1 73,2 75,1 77,1 78,9 80,7 82,4 84 85,5 86,9 88,3
kg 83 85 88 90 92 94 96 98 100 102 104 105
lbs 183 187 194 198 203 207 212 216 220 225 229 231
Min. 11,8 12,1 12,5 12,8 13,1 13,4 13,7 14 14,3 14,6 14,8 15
nm 67 69,1 71,1 73 74,9 76,7 78,4 80,1 81,7 83,1 84,5 85,8
kg 82 84 87 89 91 93 95 97 99 100 102 103
lbs 181 185 192 196 201 205 209 214 218 220 225 227
Min. 11,5 11,8 12,2 12,5 12,8 13,1 13,4 13,7 13,9 14,2 14,4 14,6
nm 65 67 69 70,9 72,7 74,4 76,1 77,7 79,3 80,7 82,1 83,3
kg 80 82 85 87 89 91 93 95 97 98 100 101
lbs 176 181 187 192 196 201 205 209 214 216 220 223
Min. 11,3 11,6 11,9 12,3 12,6 12,8 13,1 13,4 13,6 13,9 14,1 14,3
nm 63,2 65,2 67,1 68,9 70,7 72,3 74 75,6 77,1 78,5 79,8 81
kg 79 81 84 86 88 90 92 94 95 97 98 100
lbs 174 179 185 190 194 198 203 207 209 214 216 220

370

380

390

Flight Level

Weight [t]

300

310

320

330

340

350

360

Weight [1,000lbs]

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CRJ-700 CRJ-900

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2-1-83

02-May-2017

CRJ 900

LOA D SHEET

CRJ 900 TAKEOFF AND LANDING DATA CARD

WEIGHT AND BALANCE

PAYLOAD

Maximum CRJ700ER: 8‘190kg / 18‘055lbs Maximum CRJ900ER: 9‘907kg / 21‘840lbs

Description

Passenger count

Arm

Weight

Moment

[kg]

[lbs]

Max

Actual

[in]

[ft]

[kg or lbs]

Dry Operation
Weight

22.131

48.790

878,4

73,20

Pilots

95ea

209ea 2

255

21,25

Forward Flight
Attendant

75ea

165ea 1

312

26,00

Aft Flight
Attendant

75ea

165ea 1

1.114

92,83

Passengers Rows
1-3

84ea

185ea

10

431

35,92

Passengers Rows
4-7

84ea

185ea

16

658

54,83

Passengers Rows
8-11

84ea

185ea

16

784

65,33

Passengers Rows
12-16

84ea

185ea

16

926

77,17

Passengers Rows
17-20

84ea

185ea

16

1.050

87,50

Passengers Rows
21-24

84ea

185ea

16

1.051

87,58

Forward Cargo
compartment

771

1.700

597

49,75

Aft Cargo
compartment

1.697

3.740

1.188

99,00

Zero Fuel Weight
(ZFW)

31.751

69.998

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02-May-2017

FUEL

Fuel Wing tanks
(left + right)

6.832

15.062

865

72,08

Fuel Center tank

2.115

4.663

836

69,67

TAKEOFF

Description

Passenger count

Arm

Weight

Moment

[kg]

[lbs]

Max

Actual

[in]

[ft]

[kg or lbs]

Takeoff Weight
= Zero Fuel
Weight + Est.
Fuel at Takeoff

37.422

82.500

Center of
Gravity [% MAC]

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TAKEOFF

Airport

Field Elev.

QNH

RWY.

C.G. & Trim

Temp.

V1

VR

V2

Flaps 20 → Flaps 8

Flaps 8 → Flaps 1

Flaps 1 → Flaps 0

LANDING

Est. Rem. Fuel

0.00%

5.00%

10.00%

15.00%

20.00%

25.00%

30.00%

35.00%

762 767 772 777 782 787

CoG [% MAC]

Arm [in]

CoG (CRJ700)

0.00%

5.00%

10.00%

15.00%

20.00%

25.00%

30.00%

35.00%

861 866 871 876

CoG [% MAC]

Arm [in]

CoG (CRJ900)

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Landing Weight = Zero Fuel Weight + Est. Rem. Fuel

Max. Landing Weight

CRJ700ER: 30.391kg / 67.000lbs CRJ900ER: 33.340kg / 73.500lbs

Airport

Field Elev.

QNH

RWY.

C.G. & Trim

Temp.

V

Ref

V

2GA

Flaps 20 → Flaps 8

Flaps 8 → Flaps 1

Flaps 1 → Flaps 0

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2-1-87

02-May-2017

PERFORMANCE

V-SPEED-TABLE S

55’000LBS / 24‘948 KGS

55’000lbs / 24‘948 kgs

Landing

Flaps

0°

1°

8°

20°

30°

45°

Min Maneuvering

171

155

149

143

139

131

V

REF

161

145

139

133

129

121

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

114

115

116

116

117

119

118

118

118

117

20°C

114

115

115

116

118

119

118

118

117

117

30°C

114

115

116

117

120

118

118

117

117

117

40°C

116

117

118

38° /
120

34° /
120

118

117

117

38° /
116

34° /
117

MAX TEMP

50° / 118

46° / 120

42° / 118

50° / 117

46° / 117

42° / 117

VR

≤ 10°C

119

119

119

119

119

119

118

118

118

117

20°C

119

119

119

119

119

119

118

118

117

117

30°C

119

119

119

119

120

118

118

117

117

117

40°C

119

119

119

38° /
121

34° /
120

118

117

117

38° /
116

34° /
117

MAX TEMP

50° / 119

46° / 120

42° / 119

50° / 117

46° / 117

42° / 117

V2 / V

2GA

135 / 128

136

Flap

Retraction

147

(Flaps 1)

155

(Flaps 0)

148

(Flaps 8)

156

(Flaps 1)

156

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL310

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

170

174

177

180

182

184

186

189

192

195

198

VMD/Min Hold

199

199

199

200

200

201

200

201

204

207

212

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56’000LBS / 25‘401 KGS

56’000lbs / 25‘401 kgs

Landing

Flaps

0°

1°

8°

20°

30°

45°

Min Maneuvering

172

156

150

142

140

132

V

REF

162

146

140

132

130

122

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

115

116

117

117

119

119

118

118

118

117

20°C

115

115

116

117

120

119

118

118

117

117

30°C

115

116

117

119

122

118

118

117

117

117

40°C

117

118

120

38°
/122

34° /
122

118

117

117

38° /
116

34° /
117

MAX TEMP

50° /120

46° / 122

42° / 120

50° / 117

46° / 117

42° / 117

VR

≤ 10°C

119

119

119

120

120

119

118

118

118

117

20°C

119

119

119

120

121

119

118

118

117

117

30°C

119

119

119

120

121

122

118

118

117

117

40°C

119

120

121

38° /
122

34° /
122

118

117

117

38° /
116

34° /
117

MAX TEMP

50° / 120

46° / 122

42° / 121

50° / 117

46° / 117

42° / 117 V2

/ V

2GA

135 / 129

136

Flap

Retraction

147

(Flaps 1)

157

(Flaps 0)

148

(Flaps 8)

156

(Flaps 1)

157

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL310

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

172

175

178

182

184

186

188

191

194

197

200

VMD/Min Hold

201

201

201

201

202

202

202

203

206

210

214

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2-1-89

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57’000LBS / 25‘855 KGS

57’000lbs / 25‘855 kgs

Landing

Flaps

0°

1°

8°

20°

30°

45°

Min Maneuvering

173

157

151

145

141

133

V

REF

163

147

141

135

131

123

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

115

116

117

118

120

119

118

118

117

117

20°C

115

115

117

118

121

118

118

118

117

117

30°C

115

116

118

121

123

118

118

117

117

116

40°C

117

119

122

38° /
123

34° /
123

118

117

117

38° /
116

34° /
116

MAX TEMP

50° /121

46° / 123

42° / 122

50° / 117

46° / 117

42° / 117

VR

≤ 10°C

119

119

119

120

121

119

118

118

117

117

20°C

119

119

119

120

122

118

118

118

117

117

30°C

119

119

120

122

123

118

118

117

117

116

40°C

119

120

122

38° /
123

34° /
123

118

117

117

38° /
116

34° /
116

MAX TEMP

50° / 121

46° / 123

42° / 122

50° / 117

46° / 117

42° / 117

V2 / V

2GA

134 / 130

135

Flap

Retraction

146

(Flaps 1)

158

(Flaps 0)

147

(Flaps 8)

155

(Flaps 1)

158

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL310

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

173

177

180

183

185

188

190

193

195

198

202

VMD/Min Hold

203

203

203

203

204

204

204

205

208

212

217

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2-1-90

02-May-2017

58’000LBS / 26‘308 KGS

58’000lbs / 26‘308 kgs

Landing

Flaps

0°

1°

8°

20°

30°

45°

Min Maneuvering

174

158

152

146

142

134

V

REF

164

148

142

136

132

124

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

116

117

119

120

122

119

118

118

117

117

20°C

116

117

118

120

123

118

118

118

117

117

30°C

116

118

120

123

125

118

118

117

117

117

40°C

119

121

124

38° /
125

34° /
125

118

117

117

38° /
117

34° /
117

MAX TEMP

50° / 123

46° / 124

42° / 124

50° / 117

46° / 117

42° / 117

VR

≤ 10°C

120

120

121

121

123

119

118

118

117

117

20°C

120

120

121

122

124

118

118

118

117

117

30°C

120

120

122

123

125

118

118

117

117

117

40°C

121

122

124

38° /
125

34° /
125

118

117

117

38° /
117

34° /
117

MAX TEMP

50° / 123

46° / 124

42° / 124

50° / 117

46° / 117

42° / 117

V2 / V

2GA

135 / 132

135

Flap

Retraction

147

(Flaps 1)

160

(Flaps 0)

147

(Flaps 8)

155

(Flaps 1)

160

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL300

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

175

178

182

185

187

189

192

194

197

200

204

VMD/Min Hold

205

204

205

205

206

206

206

208

211

215

220

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2-1-91

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59’000LBS / 26‘762 KGS

59’000lbs / 26‘762 kgs

Landing

Flaps

0°

1°

8°

20°

30°

45°

Min Maneuvering

175

159

153

147

143

135

V

REF

165

149

143

137

133

125

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

117

118

120

121

123

118

118

118

117

117

20°C

117

118

119

121

124

118

118

117

117

117

30°C

117

119

121

124

126

118

118

117

117

117

40°C

120

122

125

38° /
126

34° /
126

118

117

117

38° /
118

34° /
117

MAX TEMP

50° / 124

46° / 125

42° / 125

50° / 117

46° / 117

42° / 117

VR

≤ 10°C

120

121

122

122

124

118

118

118

117

117

20°C

120

121

122

123

125

118

118

117

117

117

30°C

120

121

123

124

126

118

118

117

117

118

40°C

122

123

125

38° /
126

34° /
126

118

117

117

38° /
118

34° /
118

MAX TEMP

50° / 124

46° / 125

42° / 125

50° / 117

46° / 117

42° / 117

V2 / V

2GA

135 / 133

134

Flap

Retraction

147

(Flaps 1)

161

(Flaps 0)

146

(Flaps 8)

154

(Flaps 1)

161

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL300

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

176

180

183

187

189

191

193

196

199

202

206

VMD/Min Hold

206

206

207

207

208

207

207

210

213

218

223

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2-1-92

02-May-2017

60’000LBS / 27‘216 KGS

60’000lbs / 27‘216 kgs

Landing

Flaps

0°

1°

8°

20°

30°

45°

Min Maneuvering

176

160

154

148

144

136

V

REF

166

150

144

138

134

126

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

119

120

121

123

125

118

118

118

117

117

20°C

119

120

121

123

126

118

118

117

117

118

30°C

119

121

123

126

127

118

118

117

118

119

40°C

122

124

126

38° /
128

34° /
127

118

117

118

38° /
119

34° /
119

MAX TEMP

50° / 126

46° / 127

42° / 126

50° / 118

46° / 119

42° / 118

VR

≤ 10°C

121

122

123

124

125

118

118

118

117

118

20°C

122

122

123

125

126

118

118

117

117

118

30°C

122

123

125

126

127

118

118

117

118

119

40°C

123

125

126

38° /
128

34° /
127

118

19

118

38° /
119

34° /
119

MAX TEMP

50° / 126

46° / 127

42° / 126

50° / 118

46° / 119

42° / 118

V2 / V

2GA

136 / 134

134

Flap

Retraction

148

(Flaps 1)

163

(Flaps 0)

145

(Flaps 8)

154

(Flaps 1)

163

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL290

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

178

181

185

189

191

193

195

198

201

204

208

VMD/Min Hold

208

208

208

209

209

209

210

212

216

220

226

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-93

02-May-2017

61’000LBS / 27‘669 KGS

61’000lbs / 27‘669 kgs

Landing

Flaps

0°

1°

8°

20°

30°

45°

Min Maneuvering

177

161

155

149

145

137

V

REF

167

151

145

139

135

127

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

120

121

122

124

126

118

118

118

117

117

20°C

120

121

122

125

127

118

118

117

117

118

30°C

120

122

124

127

128

118

117

117

118

120

40°C

123

125

127

38° /
129

34° /
128

117

117

119

38° /
120

34° /
120

MAX TEMP

50° /127

46° / 128

42° / 127

50° / 118

46° / 120

42° / 119

VR

≤ 10°C

122

123

124

125

126

118

118

118

117

118

20°C

123

123

124

126

127

118

118

117

117

119

30°C

123

124

126

127

128

118

117

117

119

120

40°C

124

126

127

38° /
129

34° /
128

117

118

119

38° /
120

34° /
120

MAX TEMP

50° / 127

46° / 128

42° / 127

50° / 118

46° / 120

42° / 119

V2 / V

2GA

137 / 135

133

Flap

Retraction

149

(Flaps 1)

164

(Flaps 0)

145

(Flaps 8)

153

(Flaps 1)

164

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL290

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

179

183

186

190

192

195

197

200

203

206

210

VMD/Min Hold

210

210

210

211

211

211

212

214

218

223

228

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-94

02-May-2017

62’000LBS / 28‘123 KGS

62’000lbs / 28‘123 kgs

Landing

Flaps

0°

1°

8°

20°

30°

45°

Min Maneuvering

178

162

156

150

146

138

V

REF

168

152

146

140

136

128

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

121

123

124

126

128

118

118

118

118

119

20°C

121

123

124

127

129

118

118

118

118

120

30°C

122

124

126

129

130

118

118

118

120

121

40°C

125

127

129

38° /
130

34° /
130

118

119

120

38° /
122

34° /
121

MAX TEMP

50° /128

46° / 129

42° / 129

50° / 120

46° / 121

42° / 120

VR

≤ 10°C

124

125

126

127

128

118

118

118

118

120

20°C

124

125

126

127

129

118

118

118

119

120

30°C

124

126

127

129

130

118

118

119

120

121

40°C

126

128

129

38° /
130

34° /
130

118

119

121

38° /
122

34° /
121

MAX TEMP

50° / 128

46° / 129

42° / 129

50° / 120

46° / 121

42° / 121

V2 / V

2GA

138 / 136

133

Flap

Retraction

150

(Flaps 1)

166

(Flaps 0)

145

(Flaps 8)

153

(Flaps 1)

166

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL290

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

181

184

188

190

194

196

199

202

205

208

211

VMD/Min Hold

211

212

212

212

212

212

214

217

221

226

229

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-95

02-May-2017

63’000LBS / 28‘576 KGS

63’000lbs / 28‘576 kgs

Landing

Flaps

0°

1°

8°

20°

30°

45°

Min Maneuvering

179

163

157

151

147

139

V

REF

169

153

147

141

137

129

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

122

124

125

127

129

118

118

118

119

120

20°C

122

124

125

128

130

118

118

118

119

121

30°C

123

125

127

130

131

118

118

119

121

122

40°C

126

128

130

38°
/131

34°
/131

118

120

121

38° /
123

34° /
122

MAX TEMP

50° / 129

46° / 130

42° / 130

50° / 121

46° / 122

42° / 121

VR

≤ 10°C

125

126

127

128

129

118

118

118

119

121

20°C

125

126

127

128

130

118

118

119

120

121

30°C

125

127

128

130

131

118

118

120

121

122

40°C

127

129

130

38°
/131

34°
/131

119

120

122

38° /
123

34° /
122

MAX TEMP

50° / 129

46° / 130

42° / 130

50° / 121

46° / 122

42° / 122

V2 / V

2GA

139 / 137

132

Flap

Retraction

151

(Flaps 1)

167

(Flaps 0)

144

(Flaps 8)

152

(Flaps 1)

167

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL310

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

182

186

189

193

195

198

200

203

206

209

213

VMD/Min Hold

213

213

213

214

214

214

216

219

223

228

230

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-96

02-May-2017

64’000LBS / 29‘030 KGS

64’000lbs / 29‘030 kgs

Landing

Flaps

0°

1°

8°

20°

30°

45°

Min Maneuvering

180

164

158

152

148

140

V

REF

170

154

148

142

138

130

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

124

126

127

129

131

119

119

119

120

121

20°C

124

126

127

129

131

119

119

119

121

122

30°C

124

127

129

131

132

119

119

121

122

124

40°C

128

130

132

38° /
133

34° /
132

120

121

123

38° /
124

34° /
124

MAX TEMP

50° /131

46° / 132

42° / 132

50° / 122

46° / 123

42° / 123

VR

≤ 10°C

126

127

128

129

131

119

119

120

121

122

20°C

127

128

129

130

131

119

119

120

121

123

30°C

127

128

130

131

132

119

120

121

123

124

40°C

129

130

132

38° /
133

34° /
132

120

122

123

38° /
124

34° /
124

MAX TEMP

50° / 131

46° / 132

42° / 132

50° / 122

46° / 123

42° / 123 V2

/ V

2GA

140 / 138

132

Flap

Retraction

152

(Flaps 1)

169

(Flaps 0)

144

(Flaps 8)

152

(Flaps 1)

169

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL280

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

184

187

191

195

197

199

202

205

208

211

215

VMD/Min Hold

214

215

215

216

216

216

218

221

226

231

231

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-97

02-May-2017

65’000LBS / 29‘484 KGS

65’000lbs / 29‘484 kgs

Landing

Flaps

0°

1°

8°

20°

30°

45°

Min Maneuvering

181

165

159

153

149

141

V

REF

171

155

149

143

139

131

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

125

127

128

130

132

119

119

120

121

122

20°C

125

127

128

130

132

119

119

120

122

123

30°C

125

128

130

132

133

119

120

122

123

125

40°C

129

131

133

38° /
134

34° /
133

121

122

124

38° /
125

34° /
125

MAX TEMP

50° / 132

46° / 133

42° / 133

50° / 123

46° / 124

42° / 124

VR

≤ 10°C

127

128

129

130

132

119

120

121

122

123

20°C

128

129

130

131

132

119

120

121

122

124

30°C

128

129

131

132

133

119

121

122

124

125

40°C

130

131

133

38° /
134

34° /
133

121

123

124

38° /
125

34° /
125

MAX TEMP

50° / 132

46° / 133

42° / 133

50° / 123

46° / 124

42° / 124

V2 / V

2GA

141 / 139

132

Flap

Retraction

153

(Flaps 1)

170

(Flaps 0)

144

(Flaps 8)

152

(Flaps 1)

170

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL270

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

185

189

192

196

198

201

204

207

210

213

217

VMD/Min Hold

216

217

217

218

217

218

220

224

228

234

232

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-98

02-May-2017

66’000LBS / 29‘937 KGS

66’000lbs / 29‘937 kgs

Landing

Flaps

0°

1°

8°

20°

30°

45°

Min Maneuvering

182

166

160

154

150

142

V

REF

172

156

150

144

140

132

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

127

129

130

132

133

120

121

122

128

124

20°C

127

129

130

132

134

120

121

122

123

125

30°C

127

130

132

134

135

120

122

123

125

126

40°C

131

133

134

38° /
135

34° /
135

120

124

125

38° /
126

34° /
126

MAX TEMP

50° / 133

46° / 134

42° / 134

50° / 125

46° / 126

42° / 125

VR

≤ 10°C

129

130

131

132

133

120

121

122

123

124

20°C

129

130

131

132

134

120

122

128

129

130

30°C

129

131

132

134

135

121

122

124

125

126

40°C

131

133

134

38° /
135

34° /
135

123

124

125

38° /
126

34° /
126

MAX TEMP

50° / 133

46° / 134

42° / 134

50° / 125

46° / 126

42° / 125

V2 / V

2GA

142 / 140

133

Flap

Retraction

154

(Flaps 1)

172

(Flaps 0)

145

(Flaps 8)

153

(Flaps 1)

172

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL270

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

187

190

194

198

200

203

206

209

212

215

219

VMD/Min Hold

218

218

219

219

219

220

222

226

231

237

233

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-99

02-May-2017

67’000LBS / 30‘391 KGS

67’000lbs / 30‘391 kgs

Landing

Flaps

0°

1°

8°

20°

30°

45°

Min Maneuvering

183

167

161

155

151

143

V

REF

173

157

151

145

141

133

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

128

130

131

133

134

121

122

123

134

125

20°C

128

130

131

133

135

121

122

123

124

126

30°C

128

131

133

135

136

121

123

124

126

127

40°C

132

134

135

38° /
136

34° /
136

123

125

126

38° /
127

34° /
127

MAX TEMP

50° / 134

46° / 135

42° / 135

50° / 126

46° / 127

42° / 126

VR

≤ 10°C

130

131

132

133

134

121

122

123

124

125

20°C

130

131

132

133

135

121

123

134

135

136

30°C

130

132

133

135

136

122

123

125

126

127

40°C

132

134

135

38° /
136

34° /
136

124

125

126

38° /
127

34° /
127

MAX TEMP

50° / 134

46° / 135

42° / 135

50° / 126

46° / 127

42° / 126

V2 / V

2GA

143 / 141

134

Flap

Retraction

155

(Flaps 1)

174

(Flaps 0)

146

(Flaps 8)

154

(Flaps 1)

174

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL270

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

188

192

195

199

202

205

207

210

213

217

220

VMD/Min Hold

219

220

220

221

221

222

225

228

233

239

234

Aerosoft – Digital Aviation

CRJ-700 CRJ-900

QUICK REFERENCE GUIDE

VOL

2

2-1-100

02-May-2017

68’000LBS / 30‘844 KGS

68’000lbs / 30‘844 kgs

Landing

Flaps

0°

1°

8°

20°

30°

45°

Min Maneuvering

184

168

162

156

152

144

V

REF

174

158

152

146

142

134

Takeoff

Add 1 kt to V1 & VR for Wing & Cowl A/I ON

Flaps

8°

20°

Press. Alt.

0

2‘000

4‘000

6‘000

8‘000

0

2‘000

4‘000

6‘000

8‘000

V1

≤ 10°C

130

132

133

134

135

122

123

124

130

126

20°C

130

132

133

135

136

122

123

124

126

127

30°C

130

133

135

136

137

122

124

126

127

128

40°C

134

135

136

38° /
138

34° /
137

125

126

128

38° /
139

34° /
128

MAX TEMP

50° / 136

46° / 137

42° / 136

50° / 127

46° / 128

42° / 128

VR

≤ 10°C

131

132

133

134

135

123

124

125

126

127

20°C

132

133

134

135

136

123

124

130

131

132

30°C

132

134

135

136

137

123

125

126

127

128

40°C

134

135

136

38° /
138

34° /
137

125

126

128

38° /
129

34° /
128

MAX TEMP

50° / 136

46° / 137

42° / 136

50° / 127

46° / 128

42° / 128

V2 / V

2GA

144 / 143

125

Flap

Retraction

156

(Flaps 1)

175

(Flaps 0)

147

(Flaps 8)

155

(Flaps 1)

175

(Flaps 0)

Additional speeds

Approximate Single Engine Drift down Altitude - FL260

Altitude (FL)

<10’000

210

230

250

270

290

310

330

350

370

390

V

FTO

/ V

ENR

190

193

197

201

203

206

209

212

215

218

222

VMD/Min Hold

221

221

222

222

222

224

227

231

236

240

235