(HPA) B737-800 Limitations Test with CFM56-7 Engines Flashcards by j. Bruce Rickli

The maximum takeoff/landing tailwind component is _______ knots.

10 or 15
Depending on Particular Option
(AOM Vol. 1 L.10.1, 10.2)

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On _________ _________ the escape slide retention bar must be installed during ________, _________, and __________.

Revenue Flights
Taxi, Takeoff, Landing
(AOM Vol. 1 L.10.1, 10.2)

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Runway slope limits: ________%

+/- 2%

AOM Vol. 1, L.10.1, 10.2

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Maximum Operating Altitude: __________ feet

41,000

AOM Vol. 1, L.10.1, 10.2

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Maximum demonstrated takeoff and landing crosswind is ______ kts with winglets and ______ kts without winglets.

33 kts
36 kts

(AOM Vol. 1, L.10.1, 10.2)

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Do not exceed speeds placarded for the ______ and ______.

Gear
Flaps

(AOM Vol. 1, L.10.1, 10.2)

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The Mach/Airspeed warning clackers can be silenced only by ________ __________ below Vmo/Mmo (340 KIAS/ .82M)

Reducing Speed

AOM Vol. 2, 15.20.7

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Va (Turbulent a/s) is _____ KIAS/______ M.

280 KIAS
.76M
(or 250 KIAS if below 15,000 feet and under MLW)

(AOM Vol. 1, SP.16.21)

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Maximum Taxi Weight: ____________

156,000

AOM Vol. 1, L.10.3

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Maximum Takeoff Weight:___________

155,500 lbs

AOM Vol. 1, L.10.3

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Maximum landing weight:____________

144,000 lbs

AOM Vol. 1, L.10.3

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Maximum zero fuel weight:__________lbs

136,000 lbs

AOM Vol. 1, L.10.3

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Maximum Differential Pressure:_________psi

9.1 psi

AOM Vol. 1, L.10.4

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With engines bleed air switches on do not operate the a/c packs in _______ for ________, _________, and __________.

High
Takeoff, Approach, Landing

(AOM Vol. 1, L.10.4)

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__________ _________ must be on when icing conditions exist or are anticipated, except during: ________ and _______ below _______ SAT.

Engine, TAI
Climb, Cruise, -40˚C

(AOM Vol. 1, L.10.4)

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Do not use _________ trim when autopilot is engaged.

Aileron

AOM Vol. 1, L.10.5

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Do not use A/P for takeoff below ________ feet AGL

400

AOM Vol. 1, L.10.5

Do not use the A/P for single channel operation below _____ feet AGL.

AOM Vol. 1, L.10.5

The use of flight deck auxiliary power outlets in the flight deck is ______ _______ without operational regulatory approval.

Not, Allowed

AOM Vol. 1, L.10.8

Maximum and minimum engine (CFM56-7) limits are in ______.

Red

AOM Vol. 1, L.10.8

Engine (CFM56-7) caution limits are in ________.

Amber

AOM Vol. 1, L.10.8

Engine ignition (CFM56-7): Must be “ON” for _______ and _______, operations in _______ _______ and during ________ ______ operations.

Takeoff, Landing
Heavy Rain
Anti Ice

(AOM Vol. 1, L.10.8)

Intentional selection of reverse thrust in flight is __________.

Prohibited

AOM Vol. 1, L.10.8

Maximum altitude for using the APU as a bleed air source and an electrical source simultaneously: __________ feet

10,000 feet

AOM Vol. 1, L.10.8, 10.9

Maximum altitude for using the APU as a bleed air source only: _________ feet.

17,000 feet | AOM Vol. 1, L.10.8, 10.9

Maximum Altitude to use the APU as an electrical source only: ___________ feet.

41,000 feet | AOM Vol. 1, L.10.8, 10.9

APU bleed valve closed when: a) Ground air _________ and the ________ _______ is open b) Eng#1 _______ _______ is open c) Eng#2 _______ _______ is open and the _______ ______ is open

a) connected, Isolation valve b) bleed valve c) bleed balve, Isolation valve (AOM Vol. 1, L.10.8, 10.9)

It is normal to have the APU _______ _______ open during engine ________; However, avoid engine __________ settings above _______.

Bleed Valve, Start Power, Idle (AOM Vol. 1, L.10.8, 10.9)

Maximum flap extension altitude: ___________ feet

20,000 feet | AOM Vol. 1, L.10.9

Holding in _______ _______ with flaps __________ is prohibited.

Icing Conditions, extended | AOM Vol. 1, L.10.8, 10.9

Do not deploy the speedbrakes in flight at radio altitudes below ________ feet AGL

1,000 feet AGL | AOM Vol. 1, L.10.9

In flight do not extend the speedbrake lever beyond the _______ ______ position.

flight detent | AOM Vol. 1, L.10.9

Alternate Flap duty cycle: After releasing "Alternate Flaps" position switch wait __ seconds before reengaging. Complete cycle "flaps 0 to 15 and back to 0" allow ____ minutes off before another extension.

15 Seconds 5 Minutes (AOM Vol. 1, L.10.9)

Weather Radar: Do not operate within ____ feet near ________ or _________

50 ft Personnel, Fuel Spill (AOM Vol. 1, L.10.10)

The restrictions to hanger and personnel do not apply to the ________ _______ mode.

Radar Test | AOM Vol. 1, L.10.10

Maximum fuel temperature: _______

49˚C | AOM Vol. 1, L.10.11

Minimum fuel temperature: _________________ or __________ whichever is higher

3˚C above the freezing point of the specific fuel onboard -43˚C (AOM Vol. 1, L.10.11)

Maximum allowable fuel imbalance between tanks one and two must be scheduled to be ______.

0 | AOM Vol. 1, L.10.11

Random fuel imbalance must not exceed _________ lbs. for ________, __________, __________, or _________.

1,000 lbs Taxi, Takeoff, Flight, Landing (AOM Vol. 1, L.10.11)

Main fuel tanks one and two must be full if _______ _______ contains _______ _______ ________ lbs.

Center Tank More Than 1,000 lbs. (AOM Vol. 1, L.10.11)

Do not apply brakes until ______ ______.

After Touchdown | AOM Vol. 1, L.10.11