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Boeing 737 > AA 737 Limitations > Flashcards

AA 737 Limitations Flashcards

1
Q

Intentional selection of thrust reversers in flight is _______

A

Prohibited

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2
Q

Do not engage the autopilot for takeoff below _______

A

500 feet AGL

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3
Q

Do not operate Weather Radar near _________, or within _________

A

Fuel Spills

50 ft of people

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4
Q

Max Headwind/Crosswind for HUD CAT II OR CAT III approach

A

Headwind 25 kts

Crosswind 15 kts

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5
Q

Intentional running of center tank fuel pump (low pressure light illuminated) is _________

A

Prohibited

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6
Q

The deadbolt position allowing access with a key is to be used ______ ______ ______ only.

A

On the ground

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7
Q

Transmitting Personal Electronic Devices (T-PED) are not approved for use forward of the flight deck door during _______________.

A

Any phase of flight

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8
Q

Random Fuel Imbalance must not exceed ________ for taxi, takeoff, flight, or landing.

A

1000 lbs

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9
Q

If one HF radio is selected for transmission, _______ the other HF radio on all audio select panels to prevent audio interference.

A

Deselect

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10
Q

Lateral fuel imbalance between main tanks 1 and 2 must be scheduled to be ________

A

Zero

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11
Q

The use of Fuel System icing inhibitor additives ______ ______
change the minimum fuel tank temperature limit

A

Does not

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12
Q

Max Crosswind on Narrow (less than 148ft) Runway

A

20 kts

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13
Q

Avoid rapid and large _________ control inputs, especially in combination with large changes in pitch, roll, or yaw as they may result in structural failure at any speed, including below Va

A

Alternating

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14
Q

27K thrust may not be selected or requested through ACARS if the TPS is ______________________
SNA operations are not part of this limitation.

A

Based on any other Thrust Rating

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15
Q

Max Crosswind with Visibility less than 3/4 (RVR 4000)

A

15 kts

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16
Q

Engine Anti-ice must be on during all ground and flight operations when icing conditions exist or are anticipated, except during climb or cruise when the temperature is below _______

A

-40 C SAT

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17
Q

Max altitude for APU Bleed + Electrical Load

A

10,000 ft

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18
Q

Use of dual channel autopilot for approach is ______

A

Prohibited

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19
Q

When extending or retracting with the ALTERNATE FLAPS position switch, allow ________ after releasing the switch before moving the switch again to avoid damage to the Alternate Flap motor clutch

A

15 Seconds

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20
Q

Autopilot to minimums is required for approaches with an RNP value of ________ unless adequate visual references is established.

A

RNP 0.3

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21
Q

Do not operate Wing Anti-ice on the ground when the OAT is above
_________

A

10 C (50 F)

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22
Q

With Engine Bleed Air Switches ON, do not operate the air conditioning packs in HIGH for ______, ______, or ______

A

Takeoff, Approach, or Landing

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23
Q

APU Bleed Valve may be open during engine start, but avoid

_____________________

A

Engine power above idle

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24
Q

Main fuel tanks 1 and 2 must be full if center tank contains more than _______

A

1000 lbs

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25
Q

Icing Conditions Exist when….

A

OAT on the ground or for takeoff, or TAT in flight is 10C (50F) or below and:

  • Visible moisture in any form is present (such as clouds, fog with visibility of one mile or less, rain, snow, sleet, and ice crystals), or…
  • When operating on ramps, taxiways, or runways where surface snow, ice, standing water, or slush may be ingested by the engines or freeze on the engines or nacelles.
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26
Q

What is the maximum airspeed allowable on the final approach segment of an RNAV/RNP approach?

A

180 kts

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27
Q

Max Tailwind for Landing

A

10 kts*

*Ops engineering will compute special data for 15 kt TW for select airports

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28
Q

On revenue flights, the escape slide retention bar (girt bar) must be inserted in the brackets on all doors during _____, _____, & _____

A

Taxi, Takeoff, & Landing

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29
Q

After 3 consecutive aborted start attempts a ____________ cooling period is required

A

15 minute

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30
Q

Do not use EGPWS terrain display for __________

A

Navigation

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31
Q

Operation with assumed temperature reduced takeoff thrust is not permitted with _________

A

Anti-skid Inoperative

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32
Q

The following limitations apply with the EEC’s in Alternate Mode

  • _____________________
  • _____________________
  • _____________________
  • _____________________
A
  • Both EEC’s must be in Alternate Mode
  • 26K max (27K If planned) T/O thrust must be used
  • Do not use the FMC takeoff N1or QRH V-speeds
  • Use of Auto-throttle for takeoff is prohibited.
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33
Q

Maximum Takeoff Weight

A

174,200 lbs (NG)

181,200 lbs (MAX)

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34
Q

Maximum altitude for unpressurized flight, following an in-flight depressurization is ______.
This altitude may be exceeded when terrain clearance requirements dictate.

A

14,000 ft

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35
Q

Severe Turbulence Speed

A

280kts/.76M

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36
Q

Exceptions to Maximum Flight Latitudes

A

Between 80W & 130W……..70N

Between 120E & 160E……..60S

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37
Q

Maximum Allowable in-flight difference between CA and FO altimeters for RVSM operations is __________

A

200 ft

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38
Q

Normal operating range of the Engine Limit Display Markings is marked by __________

A

A white arc

39
Q

Any time passengers are on board prior to airplane movement, at least one _____ _____ _____ must be open or armed

A

Floor Level Exit

40
Q

The Maximum on-the-ground difference between the CA and FO altimeters for RVSM operations is
_______ (from sea level to 5000 ft)
_______ (from 5000 ft to 10,000)

A

50 feet

60 feet

41
Q

Max Operating Altitude

A

41,000 ft

42
Q

27K operations will be authorized for use by _______ and may only be selected if it is specified on the Load Agent generated ______

A

Dispatch

TPS

43
Q

Maximum allowable on-the-ground difference between CA or FO altimeters and Field Elevation for RVSM operations is ______

A

75 ft

44
Q

Accomplish a pre-flight check of the Reinforced Flight Deck Door and Flight Deck Access System prior to the _____ _____ of the day.

A

First Flight

45
Q

APU Bleed Valve must be closed when…

  • _________________________
  • _________________________
  • _________________________
A
  • Ground air is connected and Isolation Valve is open
  • Engine #1 Bleed Valve is open
  • Isolation Valve and Engine #2 Bleed Valves are open
46
Q

The EGPWS “TERR INHIBIT” switch should be selected within 15 nm of an airfield under the following conditions

  • _________________________
  • _________________________
A
  • Operations to/from runways not in the EGPWS database

- Specific approach procedures previously identified as potentially producing false terrain alerts

47
Q

Use of aileron trim with the autopilot engaged is ______

A

Prohibited

48
Q

In flight, do not extend the Speed Brake Lever beyond the _________ detent

A

FLIGHT

49
Q

Do not deploy the Speed Brakes in flight at Radio Altitudes less than _____________

A

1000 feet

50
Q

Max altitude for APU bleed air

A

17,000 feet

51
Q

If DC Bus 2 is unpowered, place the ______ ______ switch in ______, and use the deadbolt in the ______ ______ _______ position to lock the door.

A
  • POWER CUTOFF
  • OFF
  • LOCKED KEY INOPERABLE
52
Q

Max Crosswind with Braking Action Medium (Fair)

A

20kts

53
Q

Air Data Inertial Reference Unit (ADIRU) alignment must not be attempted at latitudes greater than
___________

A

78 degrees, 15 minutes

54
Q

Maximum Flight Operating Latitude

A

82N/82S

55
Q

Do not rely on airframe visual icing cues to turn engine anti-ice on. Delaying the use of engine anti-ice until ice buildup is visible from the cockpit may result in
______ ______ ______

A

Severe engine damage

56
Q

Max Demonstrated Crosswind

A

33 kts (NG)

32 kts (MAX)

57
Q

GPS updating must be disabled for approach operation when operating ________________________ , if the FMC database and charts are not referenced to _________ reference datum, unless other appropriate procedures are used.

A

Outside of the United States National Airspace

WGS-84

58
Q

Do not apply brakes until______

A

After Touchdown

59
Q

Runway Slope Limits

A

+/- 2%

60
Q

Maximum Taxi Weight

A

174,700 lbs (NG)

181,700 lbs (MAX)

61
Q

Normal access to the flight deck will be accomplished as specified under Normal Procedures. Use of the access code is considered an ______ ______ request (except prior to departure, when flight deck crew may be required to enter access code to gain entry to the flight deck.)

A

Emergency Access

62
Q

Maximum Takeoff and Landing Altitude

A

8,400 ft

63
Q

Maximum Cabin Differential Pressure (system relief)

A

9.1 psi

64
Q

What is the minimum RNP value authorized for RNAV/RNP approaches.

A

RNP 0.11

65
Q

Maximum Fuel Tank Temperature

A

49 C

66
Q

Maximum Speeds

A

Observe all placards and instrument red lines.

.82/340 kts. (Mmo/Vmo)

67
Q

Use of the Head Up Display (HUD) with an inoperative ________ is prohibited

A

Number 1 Radio Altimeter

68
Q

Maximum altitude when an aircraft is DISPATCHED for unpressurized flight is _____

A

10,000 ft

69
Q

Max Altitude for APU Electrical Loading

A

41,000 feet

70
Q

Cautionary range of Engine Limit Display Markings is marked by ____________

A

An amber arc

71
Q

Engine Ignition must be ____ when operating in icing conditions.

A

On

72
Q

Max Tailwind for Takeoff

A

15 kts

73
Q

Maximum Landing Weight

A

146,300 lbs (NG)

152,800 lbs (MAX)

74
Q 
Engine ignition must be used for
\_\_\_\_\_\_\_\_\_
\_\_\_\_\_\_\_\_\_
\_\_\_\_\_\_\_\_\_
\_\_\_\_\_\_\_\_\_
A
  • Takeoff (AUTO or CONT)
  • Landing (AUTO or CONT)
  • Anti-ice (AUTO or CONT)
  • Operation in heavy rain (CONT)
75
Q

After a complete extend/retract cycle (0-15/15-0) using the ALTERNATE FLAPS position switch, allow ______ cooling before attempting another extension

A

5 minutes

76
Q

Ballast Fulel is _____________

A

Not Authorized

77
Q

Engine Anti-ice must be on prior to and during ______ in all icing conditions, including temperatures below -40 C SAT

A

Descent

78
Q

Maximum Altitude with Flaps Extended

A

20,000 feet

79
Q

The Integrated Standby Flight Display (ISFD) must be initialized in accordance with ______ ______

A

Approved Procedures

80
Q

Minimum tank fuel temperature prior to takeoff and in-flight

A

-43 C, or 3 C above the fuel freezing point temperature limit, whichever is higher

81
Q

The _______ _______ does not meet the accuracy requirements of RVSM airspace

A

Standby Altimeter

82
Q

On B737 aircraft with 160 passenger seat configuration, the maximum aircraft capacity is limited to _____ seated occupants for all overwater flights requiring life rafts. This includes all required flight crew, passengers, observers and non-working crew members. Infants and other children not occupying a seat are not counted towards this limitation.

A

168

83
Q

Max Crosswind with Braking Action Poor

A

10 kts

84
Q

Pilots are authorized to deviate from __________ to the extent necessary to comply with an EGPWS warning

A

An ATC Clearance

85
Q

Crews will be notified of runways/airports not contained in the EGPWS database via ____ Pilot Alert Messages, and/or Dispatch Release __________

A

F4

Remarks

86
Q

Verify that an ______ ______ of the flight deck door access system has been accomplished according to approved procedures once each ______ ______

A

Operational Check

Flight Day

87
Q

Do not operate HF radios during _______ _______

A

Refueling operations

88
Q

Maximum Zero Fuel Weight

A

138,300 lbs (NG)

145,400 lbs (MAX)

89
Q

Holding in icing conditions with flaps extended is __________

A

Prohibited

90
Q

Maximum and minimum Engine Limit Display Markings are marked by __________

A

A red line

91
Q

For single channel operation during approach, the autopilot shall not be remain engaged below _______

A

50 ft AGL

92
Q

Minimum oil quantity for Engine Start?

NG________
Max_______

A

NG(3AA-3PX) 12 qts

Max (3RA-3VM) 17 qts

93
Q

Backing the aircraft using reverse thrust is________

A

Prohibited

Boeing 737 (2 decks)

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