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

25
Q

V1 cut

A

400 -roll mode, auto throttle off, talk to tower
1000-, bug flaps 1 speed, start apu, 5 units rudder trim
Flaps 1 speed-, LVL change, select and set MCT, after to checklist, engine failure checklist
Level off- reduce thrust /rudder, trim, AP after fully trimmed

26
Q

Single engine approach, 1 dot below GS

A

“Gear down, flaps 15, command bug, landing checklist

27
Q

Go around

A

Go around
PF go around flaps 15 toga button
PM confirm pitch power then flaps 15
PM positive rate
PF gear up
Pm verify pitch power FMA and TOGA Verified
Pm lnav active
PF flaps 5 remain in toga
PF after to check

28
Q

PRM breakout

A

PF disconnect AP- leave AT on
PM- turn of FDs sets heading then Alt, then tells atc, then FD back on, heading mode VS 1000ft.
When stabilized- set 180, do go around

29
Q

Upset recovery

A

Disconnect AP AT
Push roll power stabilize

30
Q

Required documents

A

ANQ ERA
aircraft logbook
Normal checklists x2
Qrh x2 (only 1 required for dispatch)
Engine perf log
Registration cert
Airworthiness cert