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B737 > LIMITATIONS > Flashcards

LIMITATIONS Flashcards

1
Q

The maximum allowable in flight difference between captain and first officer
altitude displays for RVSM operations?

A

200 ft

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2
Q

The maximum allowable on-the-ground difference between captain and first
officer altitude displays for RVSM operations is?

A
  • 50 feet (from sea level to 5000 feet).

* 60 feet (from 5001 feet to 10,000 feet)

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3
Q

The maximum allowable on-the-ground difference between captain or first officer
altitude displays and field elevation for RVSM operations is?

A

75 feet

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4
Q

Should you trim the ailerons with autopilot engaged?

A

No

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5
Q

Lowest altitude to disconnect autopilot?

A

50 ft agl

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6
Q

Max tailwind for cat 2 or 3 approach?

A

10 kts

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7
Q

Max headwind for cat 2 or 3 approach?

A

25 kts

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8
Q

Max crosswind for cat 2 or 3 approach?

A

15 kts

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9
Q

Engine cooldown time?

A

Cooldown period is three minutes. Begin timing after clearing the landing runway.
Otherwise use OOOI ON event with four minutes to allow for transition to ground idle after reverse thrust usage.

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10
Q

Turbulence penetration airspeed?

A

280/M0.76

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11
Q

Takeoff with CSFF on upper wing surfaces is allowed. True or False?

A

True. Provided all conditions are met

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12
Q

Maximum operating altitude with flaps and/or slats

extended

A

20000 ft

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13
Q

Maximum takeoff and landing altitude

A

8400 ft

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14
Q

Maximum operating altitude

A

41000 ft

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15
Q

The maximum allowable in flight difference between captain and first officer
altitude displays for RVSM operations

A

200 ft

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16
Q

The maximum allowable on-the-ground difference between captain and first
officer altitude displays for RVSM operations is

A 
50 feet (from sea level to 5000 feet).
60 feet (from 5001 feet to 10,000 feet)
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17
Q

The maximum allowable on-the-ground difference between captain or first officer
altitude displays and field elevation for RVSM operations is

A

75 ft

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18
Q

Severe turbulence air penetration airspeed

A

280 kts / M0.76

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19
Q

Vlo

A

275 kts

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20
Q

Vle

A

320 kts

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21
Q

Vmo / Mmo

A

340 Kts / 0.82M

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22
Q

Maximum gear retraction speed (VLO)

A

235 kts

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23
Q

Maximum takeoff weight NG

A

174200 lb

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24
Q

Maximum takeoff weight MAX

A

181200 lb

25
Q

Maximum landing weight NG

A

146300 lbs

26
Q

Maximum taxi weight NG

A

174700 lb

27
Q

Maximum taxi weight MAX

A

181700 lbs

28
Q

Maximum landing weight NG

A

146300 lbs

29
Q

Maximum landing weight MAX

A

152800 lbs

30
Q

Live animals will only be carried in the forward cargo compartment. True or False?

A

True

31
Q

With either one or both engine bleed air switches ON, do not operate the air
conditioning packs in HIGH for takeoff, approach or landing. True or False?

A

True

32
Q

Maximum altitude when aircraft is dispatched for unpressurized flight

A

10000 ft

33
Q

Maximum altitude for unpressurized flight, following an inflight depressurization

A

14,000 feet. This altitude may be exceeded when terrain clearance requirements
dictate.

34
Q

Maximum cabin pressure differential

safety relief valve setting

A

9.1 psi

35
Q

Engine ignition must be on when operating in icing conditions. True or False?

A

True

36
Q

Engine anti-ice must be on during all ground and flight operations when icing
conditions exist or are anticipated, except during climb and cruise when the
temperature is below - 40°C SAT. True or False?

A

True

37
Q

Engine anti-ice must be on prior to and during descent in icing conditions, including
temperatures below - 40°C SAT. True or False?

A

True

38
Q

Should you use level change below 1000 ft?

A

No

39
Q

Should you use aileron trim with autopilot on?

A

No

40
Q

Does AA allow auto lands or dual autopilot operations?

A

No

41
Q

APU starter limit?

A

After three consecutive aborted start attempts, a fifteen minute cooling period is required.

42
Q

APU bleed + electrical load: max altitude?

A

10000 ft

43
Q

APU bleed: max altitude?

A

17000 ft

44
Q

APU electrical load: max altitude?

A

41000 ft

45
Q

Do not operate HF radios during refueling operations. True or False?

A

True

46
Q

Operation with assumed temperature reduced takeoff thrust is not permitted with
antiskid inoperative. True or False?

A

True

47
Q

Lowest altitude you can extend speed brakes?

A

1000 ft

48
Q

In flight, do not extend the speed brake lever beyond the FLIGHT detent. True or False?

A

True

49
Q

Conduct an operational check of the fuel crossflow valve prior to each ETOPS flight. True or False?

A

True

50
Q

Maximum tank fuel temperature

A

49 C

51
Q

Minimum fuel temprature

A

Tank fuel temperature prior to takeoff must not be less than -43°C or 3°C above the
fuel freeze point, whichever is higher.

52
Q

Is ballast fuel authorized?

A

No

53
Q

Minimum amount of fuel in wing tanks if center tank has more than 1000 lb of fuel?

A

Wing tanks have to be full

54
Q

Random or transient fuel imbalance must not exceed 1000 lbs for taxi, takeoff, flight or landing. True or False?

A

True

55
Q

The maximum allowable difference between the captain’s and first officer’s PFD AOA
indication is?

A

0.5 degrees

56
Q

Recommend full IRS alignment before each flight. True or False?

A

True

57
Q

Do not operate the entry or service doors with winds at the door of
more than how many knots?

A

40 kts

58
Q

Do not keep the entry or service doors open when wind gusts are more than how many knots?

A

65 kts

B737 (22 decks)

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