FCOM random Flashcards
1
Q
Flaps speeds
Flaps up speed = F40 + ?
A
F40 + 70
2
Q
Flaps speeds
F1 speed = F40 + ?
A
F40 + 50
3
Q
Flaps speeds
F5 speed = F40 + ?
A
F40 + 30
4
Q
Flaps speeds
F15 speed = F40 + ?
A
F40 + 20
5
Q
Flaps speeds
F10 speed = F40 + ?
A
F40 + 30
6
Q
Flaps speeds
F25 speed = F40 + ?
A
F40 + 10
7
Q
Flaps speeds
F30 speed = F40 + ?
A
Flaps 30 (no relation to F40)
8
Q
Structural limits (737-800)
Max taxi weight (800)
A
75 216 kg
(+/- 300)
9
Q
Structural limits (737-800)
Max take-off weight (800)
A
74 990 kg
(+/- 300)
10
Q
Structural limits (737-800)
Max landing weight (800)
A
65 317 kg
11
Q
Structural limits (737-800)
Max ZF weight (800)
A
61 688 kg
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
13
Q
Structural limits (737-8200)
Max taxi weight (8200)
A
76 427 kg
14
Q
Structural limits (737-8200)
Max take-off weight (8200)
A
76 200 kg
15
Q
Structural limits (737-8200)
Max landing weight (8200)
A
68 174 kg
16
Q
Structural limits (737-8200)
Max ZF weight (8200)
A
64 818 kg
17
Q
Dimensions
Nose tip clearance (800 & 8200)
A
7,4 m
18
Q
Dimensions
Wing tip clearance (800 & 8200)
A
5,4 m
19
Q
Dimensions
Wingspan (800 & 8200)
A
35,79 & 35,92 m
20
Q
Dimensions
Height (800 & 8200)
A
12,57 m
21
Q
Dimensions
Length (800 & 8200)
A
39,50 m
22
Q
Dimensions
Wheelbase (800 & 8200)
A
5,70 m
23
Q
Dimensions
Turn radius (800 & 8200)
A
23 & 23,1 m
24
Q
Dimensions
180° turn (800 & 8200)
A
24,3 m
25
# SOPs
Use of V/S before Flaps up no light
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
26
# Flaps speeds
Flaps 1 max speed
250 kts
27
# Flaps speeds
Flaps 2 max speed
250 kts
28
# Flaps speeds
Flaps 5 max speed
250 kts
29
# Flaps speeds
Flaps 10 max speed
210 kts
30
# Flaps speeds
Flaps 15 max speed
200 kts
31
# Flaps speeds
Flaps 25 max speed
190 kts
32
# Flaps speeds
Flaps 30 max speed
175 kts
33
# Flaps speeds
Flaps 40 max speed
162 kts
34
# Landing gear speed
Max landing gear extension speed
270 kts / M.82
35
# Landing gear speed
Max landing gear retraction speed
235 kts
36
# Landing gear speed
Max landing gear extended speed
320 kts / M.82
37
# QRH Chapters
General / emergency equipment / doors / windows
1
38
# QRH Chapters
Air systems
2
39
# QRH Chapters
Anti ice / rain
3
40
# QRH Chapters
Automatic flight
4
41
# QRH Chapters
Communication
5
42
# QRH Chapters
Electrical
6
43
# QRH Chapters
Engines / APU
7
44
# QRH Chapters
Fire protection
8
45
# QRH Chapters
Flight control
9
46
# QRH Chapters
Flight instrument display
10
47
# QRH Chapters
Flight Management
11
48
# QRH Chapters
Fuel
12
49
# QRH Chapters
Hydraulics
13
50
# QRH Chapters
Landing gear
14
51
# QRH Chapters
Warning systems
15
52
# SOPs
No assumed temperature
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
# Emergency equipment
Emergency equipment in the flight deck
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
# Systems
Pulling an engine fire switch
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
# Systems
Pulling the APU fire switch
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
# Systems
Systems relying on the bleed air system for operation
Air conditioning/pressurization
Wing and engine thermal anti-icing
Engine Starting
Hydraulic reservoirs pressurization
Water tank pressurization
Nitrogen generation system (NGS)
57
# SOPs
Aborting engine start
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
# Memory items
Aborted engine start
Engine start lever (affected engine) CUTOFF
59
# Memory items
Airspeed unreliable
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
# Memory items
APU fire
APU fire switch - Confirm - Pull, rotate to the stop, and hold for 1 second
APU switch - OFF
61
# Memory items
Engine fire or engine severe damage or separation
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
# Memory items
Engine Fire on the Ground
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
# Memory items
Engine limit or surge or stall
Autothrottle (if engaged) - Disengage
Thrust lever (affected engine) - Confirm - Retard until engine indications stay within limits or the thrust lever is closed
64
# Memory items
Engine overheat
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
# Memory items
Take-off / Landing configuration
Assure correct airplane take-off / landing configuration
66
# Memory itmes
Loss of thrust on both engines
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
# Memory items
Runaway stabilizer
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
# Memory items
Rapid depressurization (RYR)
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
# Memory items
Emergency descent FO (RYR)
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
# Memory items
Emergency descent CPT (RYR)
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
# RAAS
Criteria for a long landing caution
Aircraft is within 100 ft AGL
Passed 33% of the runway distance
Still airborne
