FCOM 400 Flashcards
Setting speed bugs 1, R, 2, 🔺🔼 Take off ?
1 = V1
R= VR
2= V2
🔺 = VFR/ V2 ICE 1
🔼 = VBG/VBG ICE 2
Setting speed bugs landing 🔺🔼
🔺= VREF
🔼= VREF ICE
V2 ICE is only to be bugged when ?
Only for takeoff in icing conditions if acceleration is above 1000ft AAL
Min gate speeds
Desce
With Flaps 0 selected = 180 KIAS
With Flaps 5 selected = 165 KIAS
With Flaps 10 selected= 155 KIAS
With Flaps 15 selected for landing= VREF OR VREF ICE
With Flaps 15 selected for Flaps 35 landing = VREF ICE Flaps 35 + 10 KIAS
With Flaps 35 selected= VREF or VREF ICE
The PF is to verify that the [INCR REF SPEED] Message is not displayed on the ED prior to ?
slowing below VREF ICE.
Auto call-outs, above 100ft RA, are treated as all other advisory calls and must be acknowledged by the PF. If an automated call fails to announce as programmed or is not responded to, the PM must ?
make the callout, and the PF must respond with ‘checked”.
The Terminate Checklist may be completed as a ?
read and confirm’ by the Captain.
Whenever the Power Levers are reduced to and remain at Flight Idle, the Pilot Flying shall ?
keep their hand on the Power Levers, unless operationally required for short periods of time.
From the IAF (during an instrument approach) or upon joining the initial leg of the circuit (visual approach), the PF must keep ?
one hand on the Power Levers and one hand on the control wheel irrespective of whether the aircraft is in manual or auto flight.
During a First Officer approach and landing, the Captain must guard the Power Levers from ?
500 ft HAA to touchdown. This is to ensure that the Captain is prepared to take control for an immediate go around if they deem necessary, and there is insufficient time to initiate a standard go around.
Small differences between charted navigation information and displayed navigation data may be noted. Differences of ?
of 3 degrees or less due to the equipment manufacturer’s application of magnetic variation or leg track averaging are operationally acceptable.
Raw data (no flight director) approaches may be considered for crew proficiency or training in ?
VMC only.
The pitch wheel should not be adjusted when ‘ALT *› is annunciated. Pilots should minimise pitch wheel use within ?
1000 ft of the selected level, or the vertical mode will revert to PITCH HOLD and ALT SEL will disarm resulting in a failure to capture the selected altitude.
If a descent clearance is received while still climbing the cleared level is to ?
be recorded. When established in cruise, the assigned altitude will be set in the AAS.
The de Havilland DHC-8 Model 402 is approved in ?
the Transport Category in compliance with the requirements listed for Canada on the Aircraft Type Certificate Data Sheet.
1.2.2
The DHC-8 Model 402 is eligible for the following kinds of operations ?
• Day and night VFR
• IFR
• Icing Conditions
1.2.4
The maximum number. of occupants shall not exceed the following:
Flight Crew: 2
Observer:1
Cabin Crew: 2
Passengers:74
Infants:6
Total: 85
Maximum Structural Weights ?
Max Ramp Weight : 29089 kg
Max Brakes Release Weight: 28998 kg
Max Landing Weight: 28009 kg
Max Zero Fuel Weight: 25855 kg
Compartment Limits ?
Forward Baggage Compartment: 412kg
Aft Baggage 1:1707 kg
Aft Baggage 2: 453 kg
Aft Baggage 1 and 2 (combined): 1707 kg
Locker 11 may be used for the carriage of flight and cabin crew overnight bags when ?
accessed through the internal baggage door only.
Manoeuvring Limit Load Factors ?
Flap retracted +2.5g/-1.0g
Flap extended +2.0g/0.0g
Maximum operating altitude
Maximum operating altitude for takeoff and landing ?
25,000 ft
10,000ft
Ambient Temperature Limits - Flight and Ground ?
50°C or ISA +35°C
-54°C
Maximum Runway Slopes
+/- 2% uphill and downhill
The maximum crosswind and tailwind components (measured at a height of 10 metres) approved for takeoff and landing are as follows ?
Hard Dry or Wet Runway(1) X-wind 32kts Tailwind 10kts
Contaminated Runway(2) X- wind 14kts Tailwind Nil
Standing Water, Slush, Loose Snow X- Wind 14kts Tailwind: NIL
Compacted Snow: X -wind: 20kts Tailwind: NIL
Tailwind component between 10 to 20 knots is permitted, only when ?
in compliance with approved Aircraft Flight Manual Supplement
1.4.5
Setting takeoff power prior to brake release, with the nose of the airplane more than ?
45° out of wind, is prohibited for wind speeds greater than 8 knots (measured at a height of 10 metres).
1.5.1
Taxi speed limitations are referenced to ground speed.
Taxi speed must not exceed ?
25 knots in a straight line taxi and 15 knots during turns.
On narrow taxiways (between 15 metres and 18 metres taxi speed must not exceed 15 knots in a straight line taxi and 10 knots during turns. Caution should be exercised when turning on narrow taxiways.
Maximum Operating Speed (Vmo)
Altitude (ft)
0 - 8000 :245
10,000: 282
18,000: 286
20,000: 275
25,000: 248
Manoeuvring Speed (VA) ?
204
Turbulence Penetration Speed (Vs)
210
Maximum Flap Extended Speed (VFE)
5: 200
10:181
15: 172
35: 158
Maximum Landing Gear Operation Speed (VLo)
200
Maximum Landing Gear Extended Speed (VLE)
215
Alternate Gear Extension Speed ?
185 kts
Maximum Tyre Speed (Groundspeed)
182 kts
Maximum air start Altitude?
20,000ft
Max Takeoff power
(МТОР) (1) ?
106%
Max takeoff power MTOP
TORQUE
MAX ITT
MAX NL
MAX NH
MAX NP
OIL PRESSURE
OIL TEMP ?
TORQUE: 106%
MAX ITT: 880 degrees Celsius
MAX NL: 100%
MAX NH:100%
MAX NP: 1020
OIL PRESSURE: 61 to 72 PSI
OIL TEMP: 0 to 107 degrees Celsius
Normal
Takeoff (NTOP)
TORQUE
MAX ITT
MAX NL
MAX NH
MAX NP
OIL PRESSURE
OIL TEMP ?
TORQUE: 90.3
MAX ITT: 822
MAX NL: 95.3%
MAX NH: 97.6%
MAX NP: 1020
OIL PRESSURE: 61 to 72
OIL TEMP:0 to 107
Max continuous MCP
TORQUE
MAX ITT
MAX NL
MAX NH
MAX NP
OIL PRESSURE
OIL TEMP ?
TORQUE: 100%
MAX ITT: 880
MAX NL: 100%
MAX NH: 100%
MAX NP: 1020
OIL PRESSURE: 61 to 72
OIL TEMP: 0 to 107
Max ITT starting ?
Max oil pressure starting?
Minimum oil temperature starting ?
920 degrees (20s)
100 max 165 if discing with OAT below 0 degrees Celsius
-40 degrees Celsius
Transient max 20s
TORQUE
MAX ITT
MAX NL
MAX NH
MAX NP
OIL PRESSURE
OIL TEMP ?
TORQUE:135 %
MAX ITT: 920
MAX NL: 102.3%
MAX NH:101.2%
MAX NP: 1173
OIL PRESSURE: 44 to 61 72 to 100
OIL TEMP: 125 max for 5s
Max Reverse
TORQUE
MAX ITT
MAX NL
MAX NH
MAX NP
OIL PRESSURE
OIL TEMP
TORQUE: 35%
MAX ITT: 880
MAX NL: 100
MAX NH: 100
MAX NP: 1020
OIL PRESSURE: 61 to 72
OIL TEMP: 0 to 107