Majestic Q400 User Manual

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PREPAR3D GUIDE
MAJESTIC SOFTWARE’S
BOMBARDIER Q400 “DASH 8”
BY CHUCK LAST UPDATED: 06/03/2018
TABLE OF CONTENT
PART 2 – COCKPIT LAYOUT
PART 3 – FLIGHT PLANNING
PART 4 – START-UP PROCEDURE
PART 5 – TAXI
PART 6 – TAKEOFF, CLIMB & CRUISE
PART 7 – AUTOPILOT
PART 8 – ENGINES & HYDRAULICS
PART 9 – ICE PROTECTION
PART 10 – APPROACH & LANDING
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MAJESTIC Q400 EDITION: PRO PLATFORM: PREPAR3D V 4.1
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The Dash 8 “Q400is a series of twin-engine, medium-range, turboprop regional airliners. The aircraft was introduced by de Havilland Canada (DHC) in 1984. Originally named the DHC-8 (nicknamed “Dash 8”), the aircraft started as the -100 series, then the -200 series, the -300 series and finally the -400 series. They are now produced by Bombardier Aerospace. De Havilland Canada was sold to Boeing in 1986, but then re-sold to Montreal-based Bombardier Aerospace in 1992. This acquisition was done in the midst of Bombardier’s expansion of the late 80’s; it had acquired Canadair in 1986, Short Brothers in 1989 and then Learjet as well in 1990.
The Dash 8 was developed from the de Havilland Canada Dash 7, which featured extreme short
take-off and landing (STOL) performance. With the Dash 8, DHC focused on improving cruise
performance and lowering operational costs. The engine chosen was the Pratt & Whitney Canada PW100. The aircraft has been delivered in four series. The Series 100 has a maximum capacity of 39, the Series 200 has the same capacity but offers more powerful engines, the Series 300 is a stretched, 50-seat version, and the Series 400 is further stretched to 78 passengers. Over 1,000 Dash 8s of all models have been built.
The DHC-8-400 “Q400” is a stretched and improved version of the Dash 8 that entered service in 2000. It is equipped with an ANVS system (Active Noise and Vibration Suppression). Models delivered after 1997 have cabin noise suppression and are designated with the prefix "Q“, as in “Q400”. Its 360 knot (667 km/h) cruise speed is 60–90 knots (111–166 km/h) higher than its competitors and predecessors. Powered by PW150A engines rated at 5,071 shp (3,781 kW) at maximum power (4,850 shp or 3,620 kW maximum continuous rated). The maximum operating altitude is 25,000 ft (7,600 m) for the standard version. Production of the Series 100 ceased in 2005, and the Q200 and Q300 in 2009.
The Q400 has been through two company acquisitions, one of which was near fatal. The engineers who worked on this airframe are very proud of its rich history and know all too well the challenges of stretching the airframe and stretching a shrinking budget. We have to remember that this started as a bush flying aircraft that has been marketed to compete with jets. The aircraft is incredibly diverse being able to serve in high end commuter markets, to military platforms and even as a water bomber. This is an aircraft that has adapted to changing
economic times and kept a great safety rating.
This is an aircraft designed to operate in the harsh canadian winter and difficult weather conditions that you will have to fly into without expensive automation systems: there is no auto-throttle nor auto-land system. The approaches need to be planned very carefully and most of your landings will be quite “firm” because of the landing gear’s configuration. Give it a chance and I am sure that you will enjoy its superbly simulated systems. Great job, Majestic Software!
PART 1
INTRODUCTION
Dash 8-100 Cutaway
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PART 1
INTRODUCTION
DHC-1 Chipmunk (1946) DHC-2 Beaver (1947) DHC-3 Otter (1951)
DHC-4 Caribou (1958)
DHC-5 Buffalo (1964)
DHC-6 Twin Otter (1965)
DHC-7 Dash 7 (1975) DHC-8 Dash 8 “Q-Series” (1983)
De Havilland Canada Aircraft
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Before you even step foot in your virtual cockpit, you need to know where you are, where you are going, how you will get there, what you need to get there. This document is structured like a short tutorial flight.
The flight tutorial is structured as follows:
Familiarize yourself with the cockpit layout
Plan your flight
Determine the flight route, fuel & cargo loads
Spawn the aircraft and set it in a Cold & Dark state
Provide aircraft with power
Program the FMC (Flight Management Computer)
Start–up the aircraft and make it ready for flight
Taxi
Takeoff
Climb and cruise
Explore autopilot capabilities
Explain engine and hydraulic system functionalities
Explain the ice protection systems
Descend, approach and land
TUTORIAL STRUCTURE
PART 1
INTRODUCTION
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DISCLAIMER: Do not use this guide for real life flying. I mean it.
Majestic Software Downloads Section
http://majesticsoftware.com/mjc8q400/downloads.html
Smart Cockpit Dash-8-400
http://www.smartcockpit.com/plane/BOMBARDIER/DASH-8-400.html
Froogle Sims Q400 Fully Loaded Playlist (Youtube)
https://www.youtube.com/watch?v=PkOc2gIS_s8&list=PL_xDmvmUFDEjAyzamHQaoM7hXrJudErUX
Airline2Sim (Payware Course)
https://www.airline2sim.com/course/q400-cadet/
Airline2Sim SIDs and STAR (Youtube)
https://www.youtube.com/watch?v=CKhxjVHTJYc
Aircraft Icing:
https://aircrafticing.grc.nasa.gov/1_1_3_3.html
BEST RESOURCES
PART 1
INTRODUCTION
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PART 2
COCKPIT LAYOUT
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PART 2
COCKPIT LAYOUT
Circuit Breaker Panel
Microphone &
Headset Jacks
Oxygen Crew Mask
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PART 2
COCKPIT LAYOUT
Circuit Breaker Panel
Side Window De-Mist Control
AFT = OPEN FWD = CLOSED
Low Level Vents Control
AFT = OPEN
FWD = CLOSED
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PART 2
COCKPIT LAYOUT
Map Light Control
Airspeed Limitations Placard
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PART 2
COCKPIT LAYOUT
GPWS (Ground Proximity Warning System) Flap Override Button
Ground Crew Connection Annunciator
Steering Hand Control (Tiller)
Used to steer aircraft on ground. Left click and drag to steer.
Push-To -Talk (PTT) Switch
Circuit Breaker Panel Lighting Control Toggle Switch
Windshield Wiper Ice Detection Light Pushbutton
Pilot’s Side Panel Dimmer Knob
Propeller Overspeed Governor Test Toggle Switch
Nosewheel Steering Toggle Switch
AFT = OFF FWD = NOSEWHEEL STEERING ON
Takeoff Warning System Test Toggle Switch
ADC (Air Data Computer) Test Toggle Switch
Stall Warning Test Toggle Switch
Alternate Pilot Wiper Pushbutton
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PART 2
COCKPIT LAYOUT
Transmit/Interphone Push-to-Talk Switch
Elevator Trim Switches
Autopilot Disengage Pushbutton
Yoke
TCS (Tactile Control Steering) Pushbutton
ATC (Air Traffic Controller)
Identification Pushbutton
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PART 2
COCKPIT LAYOUT
Barometric Pressure Setting Adjustment Knob
Standby ADI (Attitude Director Indicator)
Caution Press-to­Reset Switchlight
Terrain Warning
Inhibit Switch
Autopilot Disengage Light
PULL UP GPWS (Ground-
Proximity Warning
System) Test Light
BELOW G/S (Glide Slope) Light
Clock
Elevator Trim Push Switchlight
Stick Pusher Shut Off Switchlight
Flight/Taxi Switch
Roll Outboard & Roll Inboard Spoilers Lights
Roll Outboard & Roll Engine Fire
Press-to-Reset Switchlight
Propeller Ground (Beta) Range Lights (1/2)
Speed Bug Select Button
Speed Bug Setting Knob
Barometric Pressure Setting Knob
DH/MDA Switch
Selects Designated Height or Minimum Descent Altitude
PFD 1 (Primary Flight Display)
MFD 1 (Multifunction Display)
Barometric Pressure Setting
Cage Reset
Brightness
Control
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PART 2
COCKPIT LAYOUT
PFD 1 (Primary Flight Display)
Airspeed (kts)
Selected Heading
AFCS (Automatic Flight Control System) Lateral Mode
Flight Director Indications
Primary ADI (Attitude Director Indicator)
Aircraft Pitch Ladder (Angle in deg)
HSI (Horizontal Situation Indicator)
Selected Navigation Source Data
FMS: Flight Management System VOR: VHF Omnidirectional Range Beacon
Vertical Speed (x1000 ft per minute)
Barometric Pressure Setting (in Hg or hPa)
Altitude (ft)
AFCS (Automatic Flight Control
System) Vertical Mode
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PART 2
COCKPIT LAYOUT
MFD 1 (Multifunction Display)
Terrain Radar Information
GREEN = LAND BLUE = WATER
Navigation Page Display
(Top Down View)
Navigation Source Data
FMS: Flight Management System 024: Heading to next waypoint
CYYZ: Next Waypoint (Toronto)
856 NM: Distance to next waypoint
Heading
Magenta Line
Leads to next waypoint
PFCS (Primary Flight Control System)
LO: Left Outer Aileron Indication LI: Left Inner Aileron Indication RO: Right Outer Aileron Indication
RI: Right Inner Aileron Indication
RUD: Rudder Indication L ELEV: Left Elevator Indication R ELEV: Right Elevator Indication
True Airspeed (kts)
Ground Speed (kts)
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PART 2
COCKPIT LAYOUT
Pitot Static Isolation Valve Switch
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PART 2
COCKPIT LAYOUT
Rudder & Spoilers PUSH OFF switches
Autopilot Pitch Wheel
Navigation Source Selector
Course Selection Knob
Altitude Selection
Knob
Heading Selection Knob
Autopilot Mode Selectors
IAS: Indicated Airspeed VS: Vertical Speed VNAV: Vertical Navigation
ALT: Altitude Hold
ALT SEL: Selected Altitude
Autopilot Mode Selectors
HDG: Heading NAV: Navigation APPR: Approach BC: Back Course STBY: Standby
HSI (Horizontal Situation Indicator)
Source Selector for Autopilot
Yaw Damper Button
Illuminated = Engaged
Autopilot Master Switch
Illuminated = Engaged
Navigation Source Selector (Copilot)
Course Selection Knob (Copilot)
Heading Selection Knob (Copilot)
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PART 2
COCKPIT LAYOUT
ED: Engine Display
Displays EFIS (Electronic Flight Instrument System) data
Engine Rating Mode
NTOP: Normal Takeoff
MCL: Maximum Climb MCR: Maximum Cruise MTOP: Maximum Takeoff Power
Engine Rating Target Torque (%)
Engine Torque (%)
NH (High-Pressure Turbine Speed) (% RPM)
NP (Propeller Speed) (RPM)
Fuel Flow (lbs per hour)
NL (Low-Pressure Turbine Speed) (% RPM)
Engine Oil Temperature (deg C)
Fuel Quantity – Left & Right Tank (lbs) Fuel Temperature – Left & Right Tank (deg C) SAT: Static Air Temperature (deg C)
ITT (Interstage Turbine Temperature) (deg C)
Engine Bleed Status Annunciation
Engine Oil Pressure (psi)
Landing Gear Lever
DOWN = GEAR DEPLOYED UP = GEAR RETRACTED
Landing Gear Indications
Yellow: Gear Doors Open
Green: Gear Down
Red: Gear Unsafe
Landing Configuration Warning Mute & Test Switch
Gear Handle Lock Release Switch
GPWS (Ground Proximity Warning System) Landing Flap Indication
GPWS (Ground Proximity Warning System) Landing Flap Control
Standby Hydraulic Pressure Pump switch
PTU (Power Transfer Unit) Control switch
No. 3 Hydraulic System Isolation Valve switch
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PART 2
COCKPIT LAYOUT
HGS (Head-Up Guidance System) Advisory Panel
Anti-Skid Switch
DOWN = OFF
MIDDLE = ON
UP = TEST
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PART 2
COCKPIT LAYOUT
MFD 2 (Multifunction Display)
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PART 2
COCKPIT LAYOUT
MFD 2 (Multifunction Display) Pages
Electrical Systems Page
Hydraulic Systems Page
Engine Page
Fuel Systems Page
Doors Page
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PART 2
COCKPIT LAYOUT
Forward Outflow Valve Guard
Circuit Breaker Panel Lighting Control Toggle Switch
Copilot’s Side Panel Dimmer Knob
Windshield Wiper Ice Detection Light Pushbutton
Microphone Interphone/Transmit Toggle Switch
Forward Outflow Valve Control
Oxygen Supply Pressure (psi)
De-Ice Pneumatic Pressure (left and right systems)
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PART 2
COCKPIT LAYOUT
AHRS (Attitude & Heading Reference System) Alignment Switch
FMS (Flight Management System) CDU (Multifunction Control Display Unit)
An FMS is a specialized computer system that automates a wide variety of in-flight
tasks, reducing the workload on the flight crew to the point that modern civilian aircraft no longer carry flight engineers or navigators. A primary function is in-flight management of the flight plan.
The FMS is controlled through the MCDU physical interface.
The FMS sends the flight plan for display to the Electronic Flight Instrument
System (EFIS), NavigationDisplay (ND),or Multifunction Display (MFD).
AHRS Pitch Basic
Mode Switch
AHRS Directional Gyro Slew Buttons
AHRS Directional Gyro Slaved Mode Switch
AHRS Directional Gyro Mode Switch
Pitch Disconnect Handle
Roll Disconnect Handle
Fuel Tank 1 Auxiliary Pump Pushbutton
Fuel Tank 2 Auxiliary Pump Pushbutton
Fuel Transfer Switch
LEFT / TO TANK 1: Transfers fuel to left fuel tank MIDDLE: OFF RIGHT / TO TANK 2: Transfers fuel to right fuel tank
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PART 2
COCKPIT LAYOUT
MTOP (Maximum Takeoff Power) Engine Rating Selector
RDC NP LDG (Reduced Propeller Speed Landing) Engine Rating Selector
Event Marker Pushbutton
Stores a data snapshot in the Engine Management System leading up to the recorded event (i.e. engine malfunction)
RDC TOP (Reduced Takeoff Power) Engine Mode Reset Button
RDC TOP (Reduced Takeoff Power) Engine Mode Selector
MCR (Maximum Cruise) Engine Rating Selector
MCL (Maximum Climb) Engine Rating Selector
No. 2 Propeller Alternate Feathering Button
No. 1 Propeller Alternate Feathering Button
Autofeather Pushbutton
COM 1 Radio Frequency Display
COM 1 Radio Frequency Tuner
COM 1 Power Selector
OFF / ON / TEST
COM 1 Activate Frequency Button
Cockpit Voice Recorder Microphone Monitor Panel
EFCP (Electronic Flight Instrumentation System Control Panel)
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PART 2
COCKPIT LAYOUT
Left Navigation Source Selector 1
AUX1: Auxiliary Equipment (i.e. MLS) FMS1: Flight Management System 1 ADF1: Automatic Direction Finder 1 VOR1: VHF Omnidirectional Range 1 OFF
TCAS (Traffic & Collision Avoidance System) Button
WX/TERR (Weather /Terrain Radar) Button
FMS Data Selection Button
Push 1 shows 10 nearest navigation aids on MFD NAV page
Push 2 shows the 10 nearest airports on MFD NAV page
Push 3 shows navigation aids + airports on MFD NAV page
Push 4 removes all options
Push & HOLD removes all nav aids + airports
Left Navigation Source Selector 2
AUX2: Auxiliary Equipment (i.e. MLS) FMS2: Flight Management System 2 ADF2: Automatic Direction Finder 2 VOR2: VHF Omnidirectional Range 2 OFF
WX/TERR (Weather /Terrain Radar)
Brightness Control
Navigation Display Range Selector (nm)
MFD Navigation Display Format Switch
PFD (Primary Flight Display) Brightness Control
MFD (Multifunction Display) Brightness Control
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PART 2
COCKPIT LAYOUT
Throttle Power Levers
Positions: MAX / FLIGHT IDLE / DISC / MAX REV
Condition Levers
MAX: 1020 RPM (Normal Takeoff Rating)
MCL: 900 RPM (Maximum Climb Rating)
MIN: 850 RPM (Maximum Cruise Rating)
START & FEATHER: Propeller Blade Angle is Feathered
during engine start
FUEL OFF: Fuel shutoff
Condition Lever Friction Control
Throttle Power Lever Friction Control
Elevator Trim Indicator
Parking Brake
FWD: OFF (DISENGAGED) AFT: ON (ENGAGED)
Control Lock Lever
Physically blocks throttle power levers
Flaps Control Lever
0 / 5 / 10 / 15 / 35 deg
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PART 2
COCKPIT LAYOUT
The Thrust Reverser lever can be moved by pressing and holding the “Throttle (decrease quickly)” control mapped to your joystick. Make sure that the “Repeat” slider is set fully to the right. The default key binding is “F2”.
Take note that the Reverse Thrust lever can only be engaged if your throttle is at IDLE. The reason for that is a mechanical stopper that prevents you from engaging thrust reversers at high throttle settings.
No Reverse Thrust Generated
Reverse Thrust Generated
Throttle at IDLE
Thrust Reversers Disarmed
Throttle at MAX REV
Thrust Reversers Armed
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PART 2
COCKPIT LAYOUT
ARCDU 1 (Audio & Radio Control Display Unit)
Frequencies: UHF1 / UHF2 / VOR1 / VOR2/ ADF1 / ADF2 / INT / ATC1
IRS (Inertial Reference System) 1 Mode Switch
OFF: OFF NAV: Navigation Mode ATT: Attitude Information Only
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PART 2
COCKPIT LAYOUT
Rudder Trim Indicator
Aileron Trim Indicator
Rudder Trim Control
Aileron Trim Control
LWD: Left Wing Down RWD: Right Wing Down
MFD (Multifunction Display) 1 Mode
PFD: Primary Flight Display NAV: Navigation Page SYS: System Page ENG: Engine Page
EFIS (Electronic Flight Instrument System) Attitude/Heading Source Selector
MFD (Multifunction Display) Page Selector
Electrical Systems Page Engine Systems Page Fuel Systems Page Doors Systems Page Test Button (not simulated)
EFIS (Electronic Flight Instrument System) ADC (Air Data Computer) Source Selector
ED (Engine Display) Brightness Control
WX (Weather Radar) Power Switch
OFF / STANDBY / TEST / ON
WX (Weather Radar) Gain Control
WX (Weather Radar) Mode Buttons
WX: Weather Radar Mode WXA: Weather Radar Alert Mode GND MAP: Ground Map Mode
WX (Weather Radar) Tilt Control
HGS (Head-Up Guidance System) Control Panel
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PART 2
COCKPIT LAYOUT
ARCDU 2 (Audio & Radio Control Display Unit)
Frequencies: UHF1 / UHF2 / VOR1 / VOR2/ ADF1 / ADF2 / INT / ATC1
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