Limitations Flashcards
Runway slope
+/- 2%
Max tailwind for TO and LDG
15kts
Max operating altitude
43,100’ pressure altitude
Max takeoff and landing altitude
11,000’ pressure altitude
(AFM limit for landing is 14,000’ but restricted to 11,000’ due to takeoff pressure altitude limits)
HF radios
Do not operate while refuelling
Turbulence penetration
Below FL250 290KIAS
Above FL250 310KIAS/.84M whichever is lower
Weather Radar
Avoid weather radar operation in the hangar
This does not apply to the WX radar test mode
difference between Capt and Fo alt displays prior to takeoff
75’
Max taxi weight
Max Takeoff weight
Max landing weight
Max zero fuel weight
228,383 Kg
227,930 Kg
172,365 Kg
161,025 Kg
Minimum height to engage AP after TO
200’ AGL
Autoland max field elevation
8400’
Without LAND2 or LAND3 annunciated what height must the AP be disconnected by
100’ AGL
With LAND2 or LAND3 annunciated and GS angles greater than 3.25 degrees what is AP limitation
must be disconnected by 100’ AGL
Max wind components for HUD (Low Vis) takeoff
HW 25kts
XW 20kts
TW 15kts
Max wind components for autoland
HW 25kts
XW 25kts
TW 15kts
Max glideslope angle for autoland
3.25 degrees
Minimum glideslope angle for autoland
2.5 degrees
Use of FLCH
Do not use below 1,000’ AFE
Minimum engine oil temperature for start
-40 degrees C
Reverse thrust
Not to be used in flight
Not to be used to back the aircraft up
Maximum flap/slat altitude
20,000’
Max fuel temp at takeoff
49degrees C
Max inflight fuel temp
65degrees C
Minimum fuel tank temp prior to takeoff
-29 degrees C
Max flap speeds
1 - 250k
5 - 230k
15 - 215k
20 - 210k
25 - 180k
30 - 170k
Max temperature for dual engine start
If OAT is above 40degrees C start one at a time
Max demonstrated crosswind for TO and LDG
TO 40 kts
LDG 37 kts
