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Southwest B737 > Limitations > Flashcards

Limitations Flashcards

0
Q

APU maximum operating altitude (NG)

A

FL410

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1
Q

Aircraft must land within ___ (300,500, & 700) or ___ (800) of initial
discharge of the fire suppression system.

A

60 minutes/195 minutes

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2
Q

APU maximum operating altitude (CL)

A

FL350

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3
Q

APU electric only maximum altitude (NG)

A

FL410

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4
Q

APU electric only maximum altitude (CL)

A

FL350

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5
Q

APU bleed only maximum altitude

A

17,000’

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6
Q

APU bleed and electric maximum altitude

A

10,000’

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7
Q

With engine bleed air switches ON, do not operate the air conditioning
packs in ___ for ___.

A

HIGH/for takeoff, approach, or landing.

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8
Q

Maximum operating pressure altitude, NG

A

FL410

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9
Q

Maximum operating pressure altitude, CL

A

FL370

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10
Q

Pilots are authorized to ___ to the extent

necessary to ___.

A

Deviate from an ATC clearance/comply with a TCAS II resolution advisory (RA)

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11
Q

A tripped circuit breaker may ___. Allow approximately ___ for cooling before resetting. An in-flight reset should only be accomplished if, ___.

A

Only be reset once/two minutes/in the judgment of the Captain, regaining use of that system is critical to the safe conduct of flight.

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12
Q

Max fuel tank temperature

A

+49C

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13
Q

Minimum fuel tank temperature

A

-37C

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14
Q

Main tanks must be full if the center tank
quantity is greater than ___.
Use ___ to depletion followed by ___.

A

1,000 lb.

Center tank/wing tank fuel.

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15
Q

Circle to land minimums

A

1) 1000/3

2) Use 1000’ above airport elevation for MDA unless higher published minimums

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16
Q

On ground with one generator operating (NG) do not exceed ____ amps.

A

215

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17
Q

Do not remove AC power from aircraft until _____ after IRS shutdown.p

A

30 seconds

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18
Q

Do not use speedbrakes below ____

A

1,000 AGL

19
Q

In flight, do not use speedbrakes unless:

A

Flaps are fully retracted

20
Q

In flight, do not extend speedbrake lever beyond:

A

Flight detent

21
Q

Alternate flap duty cycle in flight is ___ complete cycle then ___ off.

A complete cycle consists of ___ to ___ and then back to ___.

Switch must be off for ___ before reversal.

A

1/5 minutes

0/15/0

15 seconds

22
Q

Do not use flaps above ___.

A

20,000’

23
Q

Maximum engine start EGT:

A

725C

24
Q

** NG **

Holding in icing conditions with ___ is prohibited

A

Flaps extended

25
Q

Operate engines at or near idle, after rollback, for a minimum of ___ prior to applying takeoff thrust.

A

2 minutes

26
Q

** CL **

Min duct pressure for engine start is___ decreasing ___ per ___.

A

30 psi/0.5 psi/1,000’

27
Q

Operate engines at or near idle for a minimum of ___ prior to
shutdown.

A

One minute

28
Q

On the first flight of the day, operate engines at or near idle, after rollback, for a minimum of ___ prior to applying takeoff thrust.

A

Five minutes

29
Q

When operational conditions permit, engines should be operated ___ for ___ prior to shutdown.

A

At or near idle/three minutes

30
Q

Reverse thrust is limited to:

A

Ground use only

31
Q

Center tank fuel pump switches must be positioned to ___ when ___.

A

OFF/both center tank fuel pump low pressure lights illuminate.

32
Q

For ground operation, center tank fuel pump switches must not be
positioned to ___ unless ___ except ___.

A

ON/the center tank fuel quantity exceeds 1,000 lb/when defueling or transferring fuel.

33
Q

Center tank fuel pumps must not be ON unless:

A

Personnel are available on the flight deck to monitor low pressure lights.

34
Q

Flight Deck Crews must not reset tripped ___, ___, or ___ circuit breakers.

A

Fuel quantity indicator/fuel pump/fuel pump control

35
Q

The fuel pump switches must be positioned OFF at the first indication of ___.

A

Fuel pump low pressure.

36
Q

Both center tank fuel pump switches must be positioned OFF for takeoff if ___.

A

Center tank fuel quantity is less than 5,000 lb

37
Q

Flight Crews must immediately respond to ___ by using the ___ located in the ___.

A

TCAS information (both TAs and RAs)/TCAS (traffic avoidance) guidelines/QRH Section P Non-Normal Maneuvers/Profiles.

38
Q

When center tank fuel quantity is greater than ___, turn on both center tank fuel pump switches ___ or after ___.

A

2,000 lb

39
Q

Turn one center fuel pump switch OFF at the beginning of the descent if less than ___ of fuel remain in the center tank. Open the ___ to ___.

A

3,000 lb/crossfeed valve/minimize fuel imbalance.

40
Q

Turn one center fuel pump switch OFF during climb or cruise when the
center tank fuel quantity reaches approximately ___. Open the ___ to ___.

A

2,000 lb/crossfeed valve/minimize fuel imbalance.

41
Q

Do not operate the weather radar during ___, near ___, or near ___.

A

Fueling/fuel spills/people.

42
Q

When center tank fuel quantity is greater than 2,000 lb, turn on both center tank fuel pump switches above ___ or after ___.

A

10,000 ft/reducing the pitch attitude

to accelerate to 250 kt or greater.

43
Q

Climb and Cruise:
Turn one center fuel pump switch OFF during climb or cruise when the center tank fuel quantity reaches approximately ___. Open the crossfeed valve to minimize fuel imbalance.

A

2,000 lb

44
Q

Climb and Cruise:
If more than 2,000 lb of fuel remain in the center tank, both center tank fuel
pump switches should be repositioned ON.
Turn one center fuel pump switch OFF during climb or cruise when the
center tank fuel quantity reaches approximately 2,000 lb. Open the
crossfeed valve to minimize fuel imbalance.

A

test

45
Q

Climb and Cruise:
If more than 2,000 lb of fuel remain in the center tank, both center tank fuel
pump switches should be repositioned ON.
Turn one center fuel pump switch OFF during climb or cruise when the
center tank fuel quantity reaches approximately 2,000 lb. Open the
crossfeed valve to minimize fuel imbalance.

A

test

Southwest B737 (3 decks)

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