737 Memory Items Flashcards

1
Q

Max operating altitude

A

41,000 ft

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2
Q

Max crosswind component TO and LND

A

33 knots (including gust)
(May be further limited by other factors)

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3
Q

Max TO/LD tailwind component

A

10 kts. (Or as permitted in company pages)

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4
Q

Max TO/LD altitude

A

8,400 ft

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5
Q

Turbulence penetration speed

A

Severe turb- 280kts.76M. Whatever lower. Only applies in climb and descents

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6
Q

Autopilot aileron trim limit

A

Use of aileron trim prohibited with AP engaged

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7
Q

Autopilot takeoff limit

A

Do not engage below 400 agl on TO.

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8
Q

Single channel approach altitude limit

A

Disengage below 50ft AGL

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9
Q

Max wind for autoland

A

Headwind 25kts
Xwind 20 kts
Tailwind 10kts

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10
Q

APU altitude limits

A

Bleed plus electric-10,000ft
Just apu bleed -17,000 ft

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11
Q

Max altitude with flaps extended

A

20,000 ft

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12
Q

Max wind HUD AIII ops

A

Headwind-25knts
Xwind- 15kts
Tailwind- 10kts

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13
Q

HUD AIII approach to manual landing

A

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

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14
Q

Aborted engine start

A

Engine start lever (affected engine) -CUTOFF

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15
Q

Unreliable airspeed

A

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

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16
Q

APU FIRE

A

1-APU fire switch.. confirm, pull, rotate to stop, hold for 1 second
2-APU Switch… off

17
Q

Cabin altitude warning or rapid decompression

A

1-don oxygen masks and set regulators to 100 percent
2- establish crew communication

18
Q

ENGINE FIRE or engine severe damage or seperation

A

1-AT (if engaged)… disengage
2 thrust lever(affected engine)… confirm, close

19
Q

LANDIN G CONFIGURATION caution

A

1- ensure correct airplane landing configuration

20
Q

Loss of thrust both engines

A

1 engine start switches (both)… FLT
2- engine start levers(both)… cutoff
3- when EGT decreases Engine start levers (both)… Idle detent

21
Q

Stab trim runaway

A

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

22
Q

Engine limit or surge or stall

A

1- AT (if engaged) … disengage
2- thrust lever (affected engine)… confirm, retard until indications are within limits or thrust lever closed

23
Q

Evacuation of can’t read checklist

A

Stop. Configure. Shutdown. Evacuate.

24
Q

Takeoff configuration

A

Assure correct airplane takeoff configuration