B757/767 Limitations & Memory Items Flashcards
Max Peak Wind (except in emergency)
50 kts
Max 90° XW for Takeoff
29 kts
Max 90° XW for Landing
29 kts
Max HW for Autoland
25 kts
Max XW for Autoland
15 kts
may be further limited by runway or visibility limitations
Max TW for Takeoff
10 kts
may be further limited by performance requirements
Max TW for Landing
10 kts
Up to 15 kts only if specified by Special Landing Analysis in PERFORMANCE - LANDING
Do not operate HF radios during ___________.
Refueling operations
Max Turbulent Air Penetration Speed
290 KIAS / .78 Mach (whichever is lower)
Do not operate the weather radar ________ or ________.
- In a hangar
- Within 50 feet of any fuel spill
(Does not apply to test mode)
After takeoff do not engage autopilot below ______.
1000’ AFL
Disconnect the autopilot by not less than _________ for all approaches (except Autoland).
100’ above TDZE
[757] Do not use the autopilot below ________ at airport PA above _______.
100’ RA
8400’
Reverse thrust is for ______ use only.
Ground
[767] Flight crew shall not blank ________ during takeoff.
Engine vibration display
Avoid ___________ control inputs, especially in combination with large changes in ____________ as they may result in structural failure at any speed, including below Va.
- Rapid and large alternating control inputs
- Pitch, roll, or yaw (e.g. large side slip angles)
Do not extend flaps above ______.
20,000’
Cabin Altitude or Rapid Depressurization
- Don the oxygen masks.
- Establish crew communications.
- Check the cabin altitude and rate.
- If the cabin altitude is uncontrollable:
- PASS OXY switch - Push and hold for 1 second
- Without delay, descend to the lowest safe altitude or 10,000 feet, whichever is higher.
- To descend:
- Move the thrust levers to idle
- Extend the speedbrakes
- If structural integrity is in doubt, limit airspeed and avoid high maneuvering loads
- Descend at Vmo/Mmo
Aborted Engine Start
- FUEL CONTROL switch (affected side) - CUTOFF
Dual Engine Failure
- ENG START selectors (both) - FLT
- Thrust levers (both) - Idle
- Do not advance thrust levers during engine recovery until above 50% N3
- FUEL CONTROL switches (both) - CUTOFF, then RUN
- If engine appears stalled or EGT approaches the Standby Engine Indicator placard limit:
- FUEL CONTROL switch (affected engine) - Confirm - CUTOFF, then RUN
- If engine appears stalled again or EGT approaches the Standby Engine Indicator placard limit, repeat as needed.
Engine Limit or Surge or Stall
- A/T ARM switch - OFF
- Thrust lever (affected side) - Confirm - Retard until engine indications stay within limits or the thrust lever is at idle
Engine Fire or Engine Severe Damage or Separation
- A/T ARM switch - OFF
- Thrust lever (affected side) - Confirm - Idle
- FUEL CONTROL switch (affected side) - Confirm - CUTOFF
- Engine fire switch (affected side) - Confirm - Pull
- If the engine fire warning light is illuminated:
- Engine fire switch (affected side) - Rotate to the stop and hold for 1 second
- If after 30 seconds the engine fire warning light stays illuminated:
- Engine fire switch (affected side) - Rotate to the other stop and hold for 1 second
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 75% N1
- Flaps up - 4° and 75% N1