FCOM Limitations Flashcards
Flight Maneouvering Load Acceleration Limits - Clean Configuration
-1 to +2.5 g
Flight Maneouvering Load Acceleration Limits - Other Configurations
0 g to +2 g
Maximum Runway Slope
+/- 2%
Maximum runway altitude
12 500’
Nominal runway width
45 m
Maximum crosswind (takeoff and landing)
40 kt (gust included)
Maximum tailwind for takeoff
15 kt
Maximum tailwind for landing
At or below 11 000’ - 15 kt
Above 11 000’ - 10 kt
Wind limitations for passenger door operation
40 kt (50 kt if aircraft nose into wind).
Doors must be closed before wind exceeeds 60 kt.
Wind limitations for cargo door operation
FWD and AFT cargo doors - 40 kt (50 kt if nose into wind OR doors are on downwind side.
Doors must be closed before wind exceeeds 60 kt.
What is the maximum recommended crosswind on a wet and contaminated runway - ESF=GOOD
Takeoff - 32 kt
Landing - 32 kt
What is the maximum recommended crosswind on a wet and contaminated runway - ESF=GOOD to MEDIUM
Takeoff - 27 kt
Landing - 27 kt
What is the maximum recommended crosswind on a wet and contaminated runway - ESF=MEDIUM
Takeoff - 20 kt
Landing - 20 kt
What is the maximum recommended crosswind on a wet and contaminated runway - ESF=MEDIUM to POOR
Takeoff - 20 kt
Landing - 20 kt
What is the maximum recommended crosswind on a wet and contaminated runway - ESF=POOR
Takeoff - 15 kt
Landing - 15 kt
In what runway conditions is takeoff not recommended?
- Wet ice
- Water on top of compacted snow
- Dry snow or Wet Snow over ice
Maximum cockpit window opening speed?
230 kt
Maximum flaps/slats speeds?
Flap 0 - VMO / MMO Flap 1 - 240 kt Flap 1 + F - 215 kt Flap 2 (Conf 1) - 205 kt Flap 2 - 196 kt Flap 3 - 186 kt Full - 180 kt
Landing gear limit - extended?
250 kt / M0.55
Landing gear limit - operating?
250kt / M0.55
Landing gear limit - landing gear gravity extension?
200 kt
Maximum operating altitude with flaps/slats extended.
20 000 ft
Maximum ground speed.
204 kt
Minimum control speed for landing (VMCL).
118 kt
Maximum taxy weight.
233 900 kg
Maximum takeoff weight.
233 000 kg
Maximum landing weight.
VH-EBA to EBD - 180 000 KG
Remainder - 182 000 kg
Maximum Zero Fuel Weight.
VH-EBA to EBD - 168 000 KG
Remainder - 170 000 kg
Minimum weight.
116 000 lbs
Recommended maximum time without air conditioning with passengers on board.
20 min
Maximum positive differential pressure.
9.25 PSI
Maximum Negative differential pressure.
VH-EBA to : -1.0 PSI
Remainder: - 0.73 PSI
Safety relief valve setting.
8.85 PSI
APU start limits.
3 attempts then 60 mins wait.
APU max rotor speed.
107 %
Maximum EGT for APU start.
1 250 C
Maximum EGT for APU operation.
650 C
APU - Maximum altitude to assist engine start.
20 000’
APU - Maximum altitude for air conditioning and pressurisation (1 pack).
22 500’
APU - Maximum altitude for air conditioning and pressurisation (2 packs).
17 500’
Can APU bleed air be used for wing anti-ice?
No
Time limit for takeoff/go-around (all engines operating).
5 minutes
Temperature limit for takeoff/go-around (all engines operating).
975 C
Time limit for takeoff/go-around (one engine inoperative).
10 mins
Temperature limit for takeoff/go-around one engine inoperative).
975 C
Maximum Continuous Thrust time limit.
Unlimited
Maximum Continuous Thrust EGT limit.
940 C
Engine start (on ground) EGT limit.
750 C
Engine start (in flight) EGT limit.
975 C
Engine maximum N1.
115.5 %
Engine maximum N2.
113 %
Engine oil maximum continuous temperature.
160 C
Engine oil maximum transient temperature (15 min).
175 C
Engine oil minimum starting temperature.
- 40 C
Engine starter maximum continuous operation.
5 min
