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FCOM - Q cards > FCOM random > Flashcards

FCOM random Flashcards

1
Q

Flaps speeds

Flaps up speed = F40 + ?

A

F40 + 70

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2
Q

Flaps speeds

F1 speed = F40 + ?

A

F40 + 50

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3
Q

Flaps speeds

F5 speed = F40 + ?

A

F40 + 30

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4
Q

Flaps speeds

F15 speed = F40 + ?

A

F40 + 20

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5
Q

Flaps speeds

F10 speed = F40 + ?

A

F40 + 30

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6
Q

Flaps speeds

F25 speed = F40 + ?

A

F40 + 10

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7
Q

Flaps speeds

F30 speed = F40 + ?

A

Flaps 30 (no relation to F40)

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8
Q

Structural limits (737-800)

Max taxi weight (800)

A

75 216 kg
(+/- 300)

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9
Q

Structural limits (737-800)

Max take-off weight (800)

A

74 990 kg
(+/- 300)

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10
Q

Structural limits (737-800)

Max landing weight (800)

A

65 317 kg

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11
Q

Structural limits (737-800)

Max ZF weight (800)

A

61 688 kg

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12
Q

SOPs

Inexperienced co-pilot (take-off and landing limitations)

A

> 2/3 of max crosswind
15kts xwind (monitored approved)
Forecast or reported windshear
T/O or LDG RVR < 1000 m
Ceiling < 100 ft above DA or < 200 ft above MDA
Contaminated Rwy
Performance limited Rwy
Visual approach
Abnormal procedures due to system defects

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13
Q

Structural limits (737-8200)

Max taxi weight (8200)

A

76 427 kg

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14
Q

Structural limits (737-8200)

Max take-off weight (8200)

A

76 200 kg

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15
Q

Structural limits (737-8200)

Max landing weight (8200)

A

68 174 kg

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16
Q

Structural limits (737-8200)

Max ZF weight (8200)

A

64 818 kg

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17
Q

Dimensions

Nose tip clearance (800 & 8200)

A

7,4 m

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18
Q

Dimensions

Wing tip clearance (800 & 8200)

A

5,4 m

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19
Q

Dimensions

Wingspan (800 & 8200)

A

35,79 & 35,92 m

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20
Q

Dimensions

Height (800 & 8200)

A

12,57 m

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21
Q

Dimensions

Length (800 & 8200)

A

39,50 m

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22
Q

Dimensions

Wheelbase (800 & 8200)

A

5,70 m

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23
Q

Dimensions

Turn radius (800 & 8200)

A

23 & 23,1 m

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24
Q

Dimensions

180° turn (800 & 8200)

A

24,3 m

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25
Q

SOPs

Use of V/S before Flaps up no light

A

SID speed requires delay in flap retraction
Rate of climb needs to be managed (follow the 1, 2, 3 rule of RYR)
A/C has accelerated to speed limit
AFDS is engaged according to RYR proc
Above MFRA

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26
Q

Flaps speeds

Flaps 1 max speed

A

250 kts

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27
Q

Flaps speeds

Flaps 2 max speed

A

250 kts

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28
Q

Flaps speeds

Flaps 5 max speed

A

250 kts

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29
Q

Flaps speeds

Flaps 10 max speed

A

210 kts

30
Q

Flaps speeds

Flaps 15 max speed

A

200 kts

31
Q

Flaps speeds

Flaps 25 max speed

A

190 kts

32
Q

Flaps speeds

Flaps 30 max speed

A

175 kts

33
Q

Flaps speeds

Flaps 40 max speed

A

162 kts

34
Q

Landing gear speed

Max landing gear extension speed

A

270 kts / M.82

35
Q

Landing gear speed

Max landing gear retraction speed

A

235 kts

36
Q

Landing gear speed

Max landing gear extended speed

A

320 kts / M.82

37
Q

QRH Chapters

General / emergency equipment / doors / windows

A

1

38
Q

QRH Chapters

Air systems

A

2

39
Q

QRH Chapters

Anti ice / rain

A

3

40
Q

QRH Chapters

Automatic flight

A

4

41
Q

QRH Chapters

Communication

A

5

42
Q

QRH Chapters

Electrical

A

6

43
Q

QRH Chapters

Engines / APU

A

7

44
Q

QRH Chapters

Fire protection

A

8

45
Q

QRH Chapters

Flight control

A

9

46
Q

QRH Chapters

Flight instrument display

A

10

47
Q

QRH Chapters

Flight Management

A

11

48
Q

QRH Chapters

Fuel

A

12

49
Q

QRH Chapters

Hydraulics

A

13

50
Q

QRH Chapters

Landing gear

A

14

51
Q

QRH Chapters

Warning systems

A

15

52
Q

SOPs

No assumed temperature

A

Aircraft de-iced (Type II or IV) –> 24K FULL mini
Crosswind > 10 kts
Gear extended flight
Bleeds Off departure
If notified in airfield brief

53
Q

Emergency equipment

Emergency equipment in the flight deck

A

4 - Quick don O2 masks & Life jackets
2 - Flash lights, fire gloves, escape straps
1 - PBE, Crash axe, Halon fire extinguisher, Red first aid kit

54
Q

Systems

Pulling an engine fire switch

A

Arms one discharge squib on each engine fire extinguisher
Closes fuel, hydraulic shutoff and engine bleed air valves
Disables thrust reverser
Trips generator control relay and breaker
Deactivates engine driven hydraulic pump LOW PRESSURE light
Allows engine fire switch to rotate

55
Q

Systems

Pulling the APU fire switch

A

Arms APU extinguisher circuit
Closes fuel shutoff valve, APU bleed air valve and APU inlet door
Trips generator control relay and breaker
Allows APU fire switch to rotate

56
Q

Systems

Systems relying on the bleed air system for operation

A

Air conditioning/pressurization
Wing and engine thermal anti-icing
Engine Starting
Hydraulic reservoirs pressurization
Water tank pressurization
Nitrogen generation system (NGS)

57
Q

SOPs

Aborting engine start

A

No N1 rotation before the engine start lever is raised to idle detent
No increase in EGT within 15s of raising the engine start lever to idle detent
EGT rapidly approaching or exceeding the start limit
No increase in, or a very slow increase in N1/N2 after EGT indication
No oil pressure indication by the time the engine is stabilized at idle

58
Q

Memory items

Aborted engine start

A

Engine start lever (affected engine) CUTOFF

59
Q

Memory items

Airspeed unreliable

A

Autopilot (if engaged) - Disengage
Autothrottle (if engaged) - Disengage
F/D switches (both) - OFF
Set the following gear up pitch attitude and thrust:
- flaps extended: 10° and 80% N1
- flaps up: 4° and 75% N1

60
Q

Memory items

APU fire

A

APU fire switch - Confirm - Pull, rotate to the stop, and hold for 1 second
APU switch - OFF

61
Q

Memory items

Engine fire or engine severe damage or separation

A

Autothrottle (if engaged) - Disengage
Thrust lever (affected engine) - Confirm - Close
Engine start lever (affected engine) - Confirm - Cutoff
Engine fire switch (affected engine) - Confirm - Pull

If the engine fire switch of ENG OVERHEAT light is illuminated:
Engine fire switch (affected engine) - Rotate to the stop and hold for 1s

62
Q

Memory items

Engine Fire on the Ground

A

Thrust lever (both) - Close
Parking brake - Set
Advise the cabin
Engine start lever (affected engine) - Cutoff
Engine fire switch (affected engine) - Pull
Engine fire switch (affected engine) - Rotate to the stop and hold for 1s

63
Q

Memory items

Engine limit or surge or stall

A

Autothrottle (if engaged) - Disengage
Thrust lever (affected engine) - Confirm - Retard until engine indications stay within limits or the thrust lever is closed

64
Q

Memory items

Engine overheat

A

Autothrottle (if engaged) - Disengage
Thrust lever (affected engine) - Confirm - Close

If the ENG OVERHEAT light stays illuminated: go to the engine fire of engine severe damage or separation checklist

65
Q

Memory items

Take-off / Landing configuration

A

Assure correct airplane take-off / landing configuration

66
Q

Memory itmes

Loss of thrust on both engines

A

Engine start switches (both) - FLT
Engine start levers (both) - Cutoff
When EGT decreases: Engine start levers (both) IDLE detent
If EGT reaches a redline or there is no increase in EGT within 30 seconds:
Engine start lever (affected engine) - Confirm - Cutoff, then idle detent

If EGT again reaches a redline or there is no increase in EGT within 30s, repeat as needed

67
Q

Memory items

Runaway stabilizer

A

Control column - Hold firmly
Autopilot (if engaged) - Disengage
Autothrottle (if engaged) - Disengage
Control column and thrust levers - Control the airplane pitch attitude and airspeed
Main electric stabilizer trim - Reduce control column forces

If the runaway stops after the autopilot is disengaged: Do not re-engage the autopilot or autothrottle

If the runaway continues after the autopilot is disengaged: Stab trim cutout switches (both) - cutout

If the runaway continues: Stabilizer trim wheel - Grasp and hold

68
Q

Memory items

Rapid depressurization (RYR)

A

Don Oxygen mask
Establish crew communication
FO (PM): Pressurization mode selector - MAN
Outflow valve switch - Close

If pressurization is restored continue manual operation.
If uncontrollable:
Passengers sign - ON
PAX oxygen switch - ON

Initiate emergency descent

69
Q

Memory items

Emergency descent FO (RYR)

A

Engine start switches - ON
Transponder - TA 7700
May day call - request QNH and MSA
Turnoff + Ldg lights - ON
Set QNH
Monitor TCAS + descent
Depressurization + Emergency descent C/L
Anticipate turbulence + icing
Call every 10 000ft
Call 2 to go
Call 1 to go

When level:
Verify Cabin alt < 10 000 ft
Remove O2 mask and establish crew communication
Complete NNC
Take over controls

70
Q

Memory items

Emergency descent CPT (RYR)

A

Announce emergency descent on PA
Select lower altitude on MCP
Select level change
Close thrust levers
Speedbrake to flight detent
Set VMO/MMO or speed limit (if structural integrity is in doubt, keep current speed and extend landing gear. Check speed)
Tidy up MCP

Reduce rate of descent at 2 to go
Stow speedbrake at 1 to go

When level:
Set appropriate speed (LRC or 300 kts)
When FO takes over control: remove O2 mask and re-establish crew communication
N1 to flightdeck for NITS

71
Q

RAAS

Criteria for a long landing caution

A

Aircraft is within 100 ft AGL
Passed 33% of the runway distance
Still airborne

FCOM - Q cards (7 decks)

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