Aerosoft CRJ-700 Quick Reference Guide

4.8 (21)

 

Aerosoft – Digital Aviation

 

QUICK REFERENCE GUIDE

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CRJ-700 CRJ-900

 

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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 CONTENTS

 

 

 

 

 

 

 

 

 

 

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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INTRODUCTION

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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CHECKLISTS

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

PRIOR TO START

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

SAFETY 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 WALKAROUND

 

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

 

 

 

 

 

 

 

 

 

 

 

 

 

 

CLEARED 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

TAXI 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

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

CLIMB 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 LANDING

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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VOL

2-1-18

CRJ-700 CRJ-900

2

02-May-2017

 

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

 

 

 

 

V2GA+10 OR HIGHER AS FLAPS ARE RETRACTED TO 8°

 

 

When positive rate of climb is achieved:

 

 

6

Landing gear.........................................

RETRACT / UP

 

 

7

Airspeed...............................................

MAINTAIN V2GA+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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VOL

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CRJ-700 CRJ-900

 

2

02-May-2017

 

 

 

 

 

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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VOL

2-1-20

CRJ-700 CRJ-900

2

02-May-2017

 

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

28‘259kg

 

62‘300lbs

 

31‘751kg

 

70‘000lbs

 

 

(MZFW)

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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

34‘019kg

 

75‘000lbs

 

37‘421kg

 

82‘500lbs

 

 

(MTOW)

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Maximum landing weight (MLW)

30‘391kg

 

67‘000lbs

 

33‘340kg

 

73‘500lbs

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

OPERATING LIMITATIONS (ALTITUDE AND 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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2-1-21

CRJ-700 CRJ-900

2

02-May-2017

 

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 CONDITIONS

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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2-1-22

CRJ-700 CRJ-900

2

02-May-2017

 

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 DATA

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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VOL

2-1-23

CRJ-700 CRJ-900

2

02-May-2017

 

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

Assisted Air

Windmill

Idle

Max.

Normal

APR (Max

 

Start

Start

Start

 

Continuous

Take-off

Power)

 

 

 

 

 

 

(TOGA)

 

N1

-

-

-

20 - 25%

99,50%

99,50%

99,50%

ITT

815°C

815°C

927°C

-

960°C

923°C (2

1‘006°C (2

 

 

 

 

 

 

min)

min)

N2

0-45%

0-45%

 

55-65%

98,00%

99,40%

99,40%

Oil Temp

-40°C

 

 

 

155°C

163°C (15

163°C (15

 

(minimum)

 

 

 

 

min)

 

 

 

 

 

min)

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Oil Press

182 psi

182 psi

182 psi

25-60 psi

45-95 psi

45-95 psi

45-95 psi

 

95 psi (after

95 psi (after

95 psi (after

25--95 psi

 

 

 

 

10 min)

10 min)

10 min)

(oil temp <

 

 

 

 

 

 

 

60 °C)

 

 

 

Minimum Oil

40%

-

-

-

-

-

-

Level for

minimum

 

 

 

 

 

 

Flight

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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VOL

2-1-24

CRJ-700 CRJ-900

2

02-May-2017

 

CONTINUOUS ENGINE IGNITION

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 CRANKING LIMITS

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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VOL

2-1-25

 

 

 

 

CRJ-700 CRJ-900

 

 

2

 

02-May-2017

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

ENGINE RELIGHT

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

RELIGHT TYPE

 

ENVELOPE

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

CRJ700

 

CRJ900

 

 

 

 

 

 

 

 

 

Wind milling

 

Altitude from 21’000 feet to 10’000 feet:

 

Altitude from 25’000

 

 

 

 

Speed 290 KIAS to VMO and 7.2% N2 minimum.

 

feet to sea level:

 

 

 

 

 

 

 

Speed 250 KIAS to VMO

 

 

Wind milling

 

Altitude from 10’000 feet to sea level:

 

 

 

 

 

and 7.2% N2 minimum.

 

 

 

 

Speed 250 KIAS to VMO and 7.2% N2 minimum.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Starter-assisted

 

Altitude from 21’000 feet to sea level:

 

 

 

 

 

 

 

 

 

Speed from VREF 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

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

FUEL

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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VOL

2-1-26

CRJ-700 CRJ-900

2

02-May-2017

 

FUEL 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

BULK FUEL FREEZING POINT

 

MINIMUM TEMPERATURE

 

 

 

 

ASTM D 1‘655 Jet A

-30°C

-40°C

 

 

 

ASTM D 1‘655 JET A1

-37°C

-47°C

 

 

 

FUEL CROSSFLOW

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

AUXILLIARY POWER UNIT, APU

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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VOL

 

2-1-27

 

 

 

 

CRJ-700 CRJ-900

 

2

 

02-May-2017

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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2-1-28

CRJ-700 CRJ-900

2

02-May-2017

 

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

No limitation – TOGA thrust may be

 

airplane nose; no wind speed limit OR

applied before brakes released.

 

>30° in either direction of the airplane

 

 

nose; <5 knots wind speed.

 

 

 

 

NOTE 2

>30° in either direction of the airplane

Apply maximum of 75% N1 before brakes

 

nose, between 5 and 30 knots wind speed

released, then TOGA thrust.

 

 

 

NOTE 3

>30° in either direction of the airplane

Apply maximum of idle / taxi thrust before

 

nose; >30 knots wind speed

brakes released, then TOGA thrust.

 

 

 

OPERATING SPEEDS

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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2-1-29

CRJ-700 CRJ-900

2

02-May-2017

 

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 LANDING 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.

WINDSHIELD 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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2-1-30

CRJ-700 CRJ-900

2

02-May-2017

 

SIDE SLIP MANUEVERS

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

SYSTEM LIMITATIONS

AIR-CONDITIONING & PRESSURIZATION

• 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°

Approved

 

Approved

120 feet AGL

 

≤ 4.0°

 

 

 

 

 

 

 

 

 

 

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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