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Boeing 737NG COPY > (HPA) B737-800 Limitations Test with CFM56-7 Engines > Flashcards

(HPA) B737-800 Limitations Test with CFM56-7 Engines Flashcards

1
Q

The maximum takeoff/landing tailwind component is _______ knots.

A

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

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2
Q

Runway slope limits: ________%

A

+/- 2%

AOM Vol. 1, L.10.1, 10.2

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3
Q

Maximum Operating Altitude: __________ feet

A

41,000

AOM Vol. 1, L.10.1, 10.2

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4
Q

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

A

33 kts
36 kts

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

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5
Q

Do not exceed speeds placarded for the ______ and ______.

A

Gear
Flaps

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

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6
Q

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

A

Reducing Speed

AOM Vol. 2, 15.20.7

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7
Q

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

A

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

(AOM Vol. 1, SP.16.21)

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8
Q

Maximum Taxi Weight: ____________

A

156,000

AOM Vol. 1, L.10.3

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9
Q

Maximum Takeoff Weight:___________

A

155,500 lbs

AOM Vol. 1, L.10.3

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10
Q

Maximum landing weight:____________

A

144,000 lbs

AOM Vol. 1, L.10.3

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11
Q

Maximum zero fuel weight:__________lbs

A

136,000 lbs

AOM Vol. 1, L.10.3

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12
Q

Maximum Differential Pressure:_________psi

A

9.1 psi

AOM Vol. 1, L.10.4

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13
Q

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

A

High
Takeoff, Approach, Landing

(AOM Vol. 1, L.10.4)

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14
Q

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

A

Engine, TAI
Climb, Cruise, -40˚C

(AOM Vol. 1, L.10.4)

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15
Q

Do not use _________ trim when autopilot is engaged.

A

Aileron

AOM Vol. 1, L.10.5

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16
Q

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

A

400

AOM Vol. 1, L.10.5

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17
Q

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

A

50

AOM Vol. 1, L.10.5

18
Q

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

A

Not, Allowed

AOM Vol. 1, L.10.8

19
Q

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

A

Red

AOM Vol. 1, L.10.8

20
Q

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

A

Amber

AOM Vol. 1, L.10.8

21
Q

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

A

Takeoff, Landing
Heavy Rain
Anti Ice

(AOM Vol. 1, L.10.8)

22
Q

Intentional selection of reverse thrust in flight is __________.

A

Prohibited

AOM Vol. 1, L.10.8

23
Q

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

A

10,000 feet

AOM Vol. 1, L.10.8, 10.9

24
Q

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

A

17,000 feet

AOM Vol. 1, L.10.8, 10.9

25
Q

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

A

41,000 feet

AOM Vol. 1, L.10.8, 10.9

26
Q

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

a) connected, Isolation valve
b) bleed valve
c) bleed balve, Isolation valve

(AOM Vol. 1, L.10.8, 10.9)

27
Q

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

A

Bleed Valve, Start
Power, Idle

(AOM Vol. 1, L.10.8, 10.9)

28
Q

Maximum flap extension altitude: ___________ feet

A

20,000 feet

AOM Vol. 1, L.10.9

29
Q

Holding in _______ _______ with flaps __________ is prohibited.

A

Icing Conditions, extended

AOM Vol. 1, L.10.8, 10.9

30
Q

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

A

1,000 feet AGL

AOM Vol. 1, L.10.9

31
Q

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

A

flight detent

AOM Vol. 1, L.10.9

32
Q

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.

A

15 Seconds

5 Minutes

(AOM Vol. 1, L.10.9)

33
Q

Weather Radar:

Do not operate within ____ feet near ________ or _________

A

50 ft

Personnel, Fuel Spill

(AOM Vol. 1, L.10.10)

34
Q

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

A

Radar Test

AOM Vol. 1, L.10.10

35
Q

Maximum fuel temperature: _______

A

49˚C

AOM Vol. 1, L.10.11

36
Q

Minimum fuel temperature: _________________ or __________ whichever is higher

A

3˚C above the freezing point of the specific fuel onboard
-43˚C

(AOM Vol. 1, L.10.11)

37
Q

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

A

0

AOM Vol. 1, L.10.11

38
Q

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

A

1,000 lbs
Taxi, Takeoff, Flight, Landing

(AOM Vol. 1, L.10.11)

39
Q

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

A

Center Tank
More Than 1,000 lbs.

(AOM Vol. 1, L.10.11)

40
Q

Do not apply brakes until ______ ______.

A

After Touchdown

AOM Vol. 1, L.10.11

41
Q

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

A

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

Boeing 737NG COPY (5 decks)

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