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AA 737 Study > 737 Limitations > Flashcards

737 Limitations Flashcards

0
Q

What is the max demonstrated crosswind (including gusts)?

A

33 kts

32 kts on the MAX

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1
Q

What is the max peak wind for all operations except emergencies?

A

50 kts

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2
Q

What is the max headwind for CAT II and CAT III approaches?

A

25 kts

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3
Q

What is the max crosswind for landing with braking action medium (including gusts)?

A

25 kts

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4
Q

What is the max crosswind when the runway width is less than standard, 148’ (including gusts)?

A

20 kts

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5
Q

What is the max tailwind for landing (including gusts)?

A

10 kts normal

15 kts if on OPS advisory page (##-7) or an F4 message

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6
Q

What is the max crosswind for landing when the visibility is less than 3/4 mi or RVR 4000 (including gusts)?

A

15 kts

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7
Q

What is the max crosswind component for a CAT II or CAT III approach?

A

15 kts

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8
Q

What is the max crosswind component for a HUD low visibility T/O (including gusts)?

A

10 kts

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9
Q

What is the max crosswind for a landing when braking action is poor (including gusts)

A

15 kts

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10
Q

What is the max tailwind for a CAT II or CAT III approach?

A

10 kts

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11
Q

What is the maximum operating altitude?

A

41,000’

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12
Q

What is the maximum takeoff and landing altitude?

A

8,400’

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13
Q

What is Vmo/Mmo?

A

340 kts / .82 Mach

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14
Q

What is the (severe) turbulent air penetration speed?

A

280 kts / .76 Mach

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15
Q

What is the max taxi speed with or without using the hand wheel?

A

20 kts

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16
Q

What is the maximum ramp weight?

A

174,700 lbs

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17
Q

What is the maximum takeoff weight?

A

174,200 lbs

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18
Q

What is the maximum landing weight?

A

146,300 lbs

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19
Q

What is the maximum zero fuel weight?

A

138,300 lbs

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20
Q

What is the max capacity SOB for the 160 and 172 seat configuration on overwater flights requiring life rafts. (not including lap children)?

A

168 / 193

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21
Q

What must be done on the first flight of the day on aircraft without the CABIN ALTITUDE & T/O CONFIG lights?

A

Conduct the Cabin Altitude Warning T/O Briefing.

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22
Q

With engine bleed air on, what pack setting should not be used during T/O, approach and landing?

A

High

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23
Q

What is the max cabin differential pressure?

A

9.1 psi

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24
Q

What is the max cabin altitude after in-flight depressurization?

A

14,000’

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25
Q

What is the max altitude when dispatched unpressurized?

A

10,000’

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26
Q

Define icing conditions per FM 1.

A

10C/50F and below AND visible moisture in any form, OR surface moisture that could be ingested by or freeze on engines or nacelles.

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27
Q

Engine ignition must be ___ when operating in icing conditions.

A

ON

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28
Q

While in icing conditions (in-flight or ground), when does the engine anti-ice NOT need to be on?

A

Climb or cruise AND -40C SAT or below. Must be on for descent in icing conditions at all temps!

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29
Q

Do not use the wing anti-ice when OAT is above ___.

A

10C / 50F

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30
Q

What is the minimum altitude for engaging the autopilot after takeoff?

A

400’

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31
Q

What is the minimum altitude for single channel autopilot for approach?

A

50’ (must still be off at DA / DDA for a non-ILS approach.

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32
Q

Use of aileron trim with the autopilot engaged is _____.

A

Prohibited.

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33
Q

Use of dual channel autopilot for approach is _____.

A

Prohibited.

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34
Q

If one HF radio is selected for transmission, the other HF radio must be ____ on all other audio panels.

A

Deselected. (to prevent audio interference)

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35
Q

Transmitting PEDs, forward of the flight deck door are _____ during any phase of flight.

A

Not approved for use.

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36
Q

Both EECs must be ____ for takeoff.

A

ON (special limitations for T/O with EECs in ALTN exist)

37
Q

Intentional use of reverse thrust in flight is ____.

A

Prohibited.

38
Q

Use of 27k T/O bump thrust at other than SNA is _____.

A

Prohibited, Unless authorized by dispatch may only be selected if specified on the TPS.

39
Q

What is the minimum oil quantity prior to engine start?

A

12 qts

14 qts on the MAX

40
Q

What is the engine starter duty cycle?

A

2 minutes ON, 10 seconds OFF

3 minutes ON, 10 seconds off on the MAX

41
Q

What is the max altitude to start and operate the APU?

A

41,000’

42
Q

What is the max altitude for the APU to provide both electrical power and bleed air?

A

10,000’ (up to 20,000’ on use of Captain’s emergency authority)

43
Q

What is the recommended maximum altitude for starting the APU?

A

25,000’

44
Q

What is the max altitude for APU bleed air only?

A

17,000’

45
Q

What is the max altitude for the APU to provide electrical power only?

A

41,000’

46
Q

When ground power is connected and the isolation valve is open, the APU bleed air must be ____.

A

CLOSED

47
Q

What is the max flap extension altitude?

A

20,000’

48
Q

Holding in icing conditions with the flaps extended is ____.

A

Prohibited.

49
Q

What is the minimum altitude for the use of speed brakes?

A

1,000’ RA

50
Q

Extending the speed brakes in flight beyond the flight detent is ____.

A

Prohibited.

51
Q

Use of the HUD with the #1 RA inoperative is _____.

A

Prohibited.

52
Q

What is the max difference between the CA and FO altimeters in flight? (For RVSM operations)

A

200’

53
Q

What is the max difference between the CA and FO altimeters on the ground?

A

50’ (sea level to 5,000’)

60’ (5,000’ to 10,000’)

54
Q

What is the max difference between the field elevation and the altimeters?

A

75’

55
Q

Does the standby altimeter meet the accuracy requirements for RVSM?

A

No.

56
Q

ADIRU alignment must not be attempted at latitudes greater than ___.

A

78 degrees, 15 minutes.

57
Q

GPS updating must be disabled for approach operations outside of the US National Airspace unless the FMC and chart database is referenced to ______.

A

WGS-84 reference datum, unless other appropriate procedures are used.

Limitation applies to China and Russia.

All 737 operations are ref to WGS-84

58
Q

What is the max tank fuel temperature?

A

49C

59
Q

What is the minimum inflight fuel temperature for Jet A and Jet A1?

A
  • 37C Jet A

- 43C Jet A1

60
Q

What is the max fuel imbalance?

A

1,000 lbs

61
Q

Main tanks must be ___ if the center tank contains more than ____.

A

full, 1,000 lbs

62
Q

Ballast fuel is ___.

A

Not authorized.

63
Q

Center tank fuel pump switches must be ____ for all ground ops unless there is more than 1,000 lbs of fuel in the center tank.

A

OFF (except for defueling or transferring fuel)

64
Q

Center tank fuel pump switches must be turned off at the first indication of ____.

A

LOW PRESSURE

65
Q

May the center tank fuel pump switches be left on unattended?

A

NO. Personnel must be in the cockpit to monitor the LOW PRESSURE lights.

66
Q

May the brakes be applied before touchdown?

A

NO.

67
Q

Is assumed temp reduced T/O thrust allowed with the anti-skid inop?

A

NO

68
Q

When is an info to maintenance required with regard to min oxygen pressure?

A

Less than 850 psi

69
Q

What is the minimum oxygen gauge pressure at 30C?

A

2 crew 500 psi

3 crew 700 psi

70
Q

May terrain mode be used for navigation?

A

NO

71
Q

Within 15 nm of takeoff, approach or landing to an airport that is not in the GPWS database, ______ use the look-ahead functions of terrain alerting and terrain display.

A

DO NOT…

72
Q

Use of weather radar within 15 feet of personnel or fuel spills is ____.

A

Unsafe/prohibited

73
Q

Severe wind-shear is that which produces airspeed changes greater than ___.

A

15 kts

74
Q

Delay takeoff or approach if ____ wind-shear is detected.

A

severe

75
Q

What thrust and flap settings should be used if conditions are conducive for wind-shear?

A

26k thrust and 5-15 flaps unless limited by obstacle clearance and/or climb gradient.

76
Q

When conditions are conducive to wind-shear, establish a stabilized approach no later than ____ and flaps ___, consistent with field length.

A

1,000’ AGL, 30 degrees

77
Q

How much dry-ice can be carried in each cargo bay? (Fwd and Aft)

A

440 lbs each, 880 lbs total.

78
Q

What is the per pax dry-ice limit?

A

4.4 lbs

79
Q

What is the total dry-ice limit in the pax cabin?

A

20 lbs

80
Q

Flap limit speed - Flaps 1-5

A

240 knots

81
Q

Flap limit speed - Flaps 10

A

210 knots

82
Q

Flap limit speed - Flaps 15

A

200 knots

83
Q

Flap limit speed - Flaps 25

A

190 knots

84
Q

Flap limit speed - Flaps 30

A

175 knots

85
Q

Flap limit speed - Flaps 40

A

162 knots

86
Q

How much fuel can each main tank hold?

A

8600 lbs.

87
Q

How much fuel can the Center tank hold?

A

28,800 lbs.

88
Q

Max total fuel?

A

46000

89
Q

How long does the Flight data recorder record for

A

Most recent 25 hours of operation

AA 737 Study (5 decks)

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