B757/767 Limitations & Memory Items

Question 1

Max Peak Wind (except in emergency)

Answer 1

50 kts

Question 2

Max 90° XW for Takeoff

Answer 2

29 kts

Question 3

Max 90° XW for Landing

Answer 3

29 kts

Question 4

Max HW for Autoland

Answer 4

25 kts

Question 5

Max XW for Autoland

Answer 5

15 kts

may be further limited by runway or visibility limitations

Question 6

Max TW for Takeoff

Answer 6

10 kts

may be further limited by performance requirements

Question 7

Max TW for Landing

Answer 7

10 kts

Up to 15 kts only if specified by Special Landing Analysis in PERFORMANCE - LANDING

Question 8

Do not operate HF radios during ___________.

Answer 8

Refueling operations

Question 9

Max Turbulent Air Penetration Speed

Answer 9

290 KIAS / .78 Mach (whichever is lower)

Question 10

Do not operate the weather radar ________ or ________.

Answer 10

• In a hangar
• Within 50 feet of any fuel spill

(Does not apply to test mode)

Question 11

After takeoff do not engage autopilot below ______.

Answer 11

1000’ AFL

Question 12

Disconnect the autopilot by not less than _________ for all approaches (except Autoland).

Answer 12

100’ above TDZE

Question 13

[757] Do not use the autopilot below ________ at airport PA above _______.

Answer 13

100’ RA

8400’

Question 14

Reverse thrust is for ______ use only.

Answer 14

Ground

Question 15

[767] Flight crew shall not blank ________ during takeoff.

Answer 15

Engine vibration display

Question 16

Avoid ___________ control inputs, especially in combination with large changes in ____________ as they may result in structural failure at any speed, including below Va.

Answer 16

• Rapid and large alternating control inputs

- Pitch, roll, or yaw (e.g. large side slip angles)

Question 17

Do not extend flaps above ______.

Answer 17

20,000’

Question 18

Cabin Altitude or Rapid Depressurization

Answer 18

1. Don the oxygen masks.
2. Establish crew communications.
3. Check the cabin altitude and rate.
4. 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

Question 19

Aborted Engine Start

Answer 19

1. FUEL CONTROL switch (affected side) - CUTOFF

Question 20

Dual Engine Failure

Answer 20

1. ENG START selectors (both) - FLT
2. Thrust levers (both) - Idle
   
   • Do not advance thrust levers during engine recovery until above 50% N3
3. FUEL CONTROL switches (both) - CUTOFF, then RUN
4. 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.

Question 21

Engine Limit or Surge or Stall

Answer 21

1. A/T ARM switch - OFF
2. Thrust lever (affected side) - Confirm - Retard until engine indications stay within limits or the thrust lever is at idle

Question 22

Engine Fire or Engine Severe Damage or Separation

Answer 22

1. A/T ARM switch - OFF
2. Thrust lever (affected side) - Confirm - Idle
3. FUEL CONTROL switch (affected side) - Confirm - CUTOFF
4. Engine fire switch (affected side) - Confirm - Pull
5. 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

Question 23

Airspeed Unreliable

Answer 23

1. Autopilot (if engaged) - Disengage
2. Autothrottle (if engaged) - Disengage
3. F/D switches (both) - OFF
4. Set the following gear up pitch attitude and thrust:
   
   • Flaps extended - 10° and 75% N1
   • Flaps up - 4° and 75% N1