Max operating altitude
41,000 ft
Max crosswind component TO and LND
33 knots (including gust)
(May be further limited by other factors)
Max TO/LD tailwind component
10 kts. (Or as permitted in company pages)
Max TO/LD altitude
8,400 ft
Turbulence penetration speed
Severe turb- 280kts.76M. Whatever lower. Only applies in climb and descents
Autopilot aileron trim limit
Use of aileron trim prohibited with AP engaged
Autopilot takeoff limit
Do not engage below 400 agl on TO.
Single channel approach altitude limit
Disengage below 50ft AGL
Max wind for autoland
Headwind 25kts
Xwind 20 kts
Tailwind 10kts
APU altitude limits
Bleed plus electric-10,000ft
Just apu bleed -17,000 ft
Max altitude with flaps extended
20,000 ft
Max wind HUD AIII ops
Headwind-25knts
Xwind- 15kts
Tailwind- 10kts
HUD AIII approach to manual landing
AIII must be selected and AP and AT disengaged prior to 500 ft above TDZE
- landing flaps 30 or 40 with both engines
-landing flaps 15 with 1 engine
Aborted engine start
Engine start lever (affected engine) -CUTOFF
Unreliable airspeed
1-autopilot(if engaged) … disengage
2-AT (if engaged) … disengage
3- FD switches (both)… off
4- if necessary to stabilize aircraft, set following gear up pitch and thrust
-flaps extende-10 degrees and 80% N1
-flaps up- 4 degrees and 75% N1
APU FIRE
1-APU fire switch.. confirm, pull, rotate to stop, hold for 1 second
2-APU Switch… off
Cabin altitude warning or rapid decompression
1-don oxygen masks and set regulators to 100 percent
2- establish crew communication
ENGINE FIRE or engine severe damage or seperation
1-AT (if engaged)… disengage
2 thrust lever(affected engine)… confirm, close
LANDIN G CONFIGURATION caution
1- ensure correct airplane landing configuration
Loss of thrust both engines
1 engine start switches (both)… FLT
2- engine start levers(both)… cutoff
3- when EGT decreases Engine start levers (both)… Idle detent
Stab trim runaway
1- control column… hold firmly
2-AP (if engaged)… disengage
3-AT (if engaged)… disengage
4- control column and thrust levers… control airplane pitch and airspeed
5- Main electric stab trim… reduce control column forces
6- if runaway stops after AP Disengage
…do not re engage AP or AT
………………..
7- if runaway continues after AP disengage… STAB TRIM CUTOUT switches (both) … Cutout
If runaway continues, stab trim wheel… grasp and hold
Engine limit or surge or stall
1- AT (if engaged) … disengage
2- thrust lever (affected engine)… confirm, retard until indications are within limits or thrust lever closed
Evacuation of can’t read checklist
Stop. Configure. Shutdown. Evacuate.
Takeoff configuration
Assure correct airplane takeoff configuration