Limitations Flashcards
Runway slope
+/- 2%
Max operating altitude
41,000’ pressure altitude
Maximum TOLD altitude
8,400’ pressure altitude
ViaSat inflight connectivity system fitted: FMC derived EO CRZ Max Altitude is required?
To be reduced by 400’
Operations on narrow runways
(<45m but not less than 30m)
Vis: RCL shall be clearly visible in the prevailing conditions
Systems: not allowed nose gear steering inop or 1 thrust reverser inop.
If an alternate airport is available with a runway at least 45m wide, diversion to that alternate shall be performed in case of jammed or restricted flight controls, trailing edge flap asymmetry, leading edge flap/slat asymmetry, or loss of system A or B hydraulics
Ground wind limits for all doors
-40KT while opening or losing
-65KT while open
Altitude display limits for RVSM operations
-standby altimeters do not meet altimeter accuracy requirements for RVSM
-Max allowable in-flight difference between the C and FO is 200’
-Max allowable on-the-ground (SL-5000’) difference between C and FO is 50’. Between the C or FO and field elevation is 75’.
VXA-VXU max weights
MTW 79242kg
MTOW 79015kg
MLW 66360kg
MZFW 61688kg
VYA-VZE max weights
MTW 75296kg
MTOW 75069kg
MLW 66360kg
MZFW 61688kg
VYZ, VZF-XZP max weights
MTW 79242kg
MTOW 79015kg
MLW 66360kg
MZFW 62731kg
Max cabin differential pressure
9.1psi
Aileron trim with the autopilot engaged?
Prohibited
Autopilot engagement for TO
Not below 400’ AGL
Single channel operation during approach, the autopilot shall not remain engaged below?
50’AGL
Max and min GS angles for autoland
3.25 and 2.5
Autoland capability may only be used:
F30 or F40 and both engines operative
LVL CHG restriction on final approach?
Do not use below 1000’ AFE
Engine ignition must be on:
-TO
-LDG
-operation in +RN
-AI operation
Reverse thrust
Intentional selection in flight is prohibited
Thrust for TO with anti-skid inoperative
ATM is not permitted
APU INFLIGHT: bleed + electrical load max alt
10000’
APU bleed max alt
17000’
APU electrical load max alt
41000’
APU bleed air valve must be closed when:
-ground air connected and isolation valve open
-engine 1 bleed valve open
-Isolation and engine 2 bleed valves open
Can be open during engine start, but avoid engine power above idle.
After 3 consecutive aborted APU start attempts, what cooling period is required?
15 minutes
How long should the APU be run before using it as a bleed air source?
2 full minutes
Max altitude with flaps extended?
20000’
Holding in icing conditions with flaps extended?
PROHIBITED
Sbeedbrakes
Do not deploy in flight at <1000’RA
Alternate flap duty cycle
-when extending or retracting flaps with ALTERNATE FLAPS position switch, allow 15 secs after releasing before moving switch again to avoid damage to the alternate flap motor clutch
-after a complete extend/retract cycle, allow 5 mins cooling before attempting another extension.
Maximum fuel tank temperature
49C
