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B737NG Limitations (FCOM) > Limitations > Flashcards

Limitations Flashcards

1
Q

Runway Slope

A

+/- 2%

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2
Q

Maximum Take Off & Landing Tailwind Component (Dry or Wet)

A

15kts

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3
Q

Max Operating Altitude

A

41,000ft

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4
Q

Maximum Take Off & Landing Altitude

A

8,400ft

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5
Q

Severe Turbulent Air Penetration Speed in Climb / Descent

A

280KTS or 0.76M, whichever is lower

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6
Q

HF Operation during refueling

A

Do not operate HF

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7
Q

Max Allowable In Flight Difference between Captain & FO Altitude Displays for RVSM

A

200ft

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8
Q

Max On The Ground Altitude Display Differences for RVSM

A

Field Elevation between Sea Level to 5,000ft
Between Captain & FO : 50ft
Between Captain, FO & Field Elevation : 75ft

Field Elevation between 5,001ft to 10,000ft
Between Captain & FO : 60ft
Between Captain, FO & Field Elevation : 75ft

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9
Q

Max Taxi Weight

A

73,935kg

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10
Q

Max Take Off Weight

A

73,708kg

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11
Q

Max Landing Weight

A

66,360kg

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12
Q

Max Zero Fuel Weight

A

61,688kg

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13
Q

Max Cabin Differential Pressure (Relief Valves)

A

9.1psi

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14
Q

With Either One or Both ENG BLEED Air Switches ON on Take Off, Approach & Landing

A

Do Not Operate Air Conditioning Packs in HIGH

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15
Q

Use Of Aileron Trim with Autopilot Engaged

A

Prohibited

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16
Q

Min Height for Use Of Autopilot

A

400ft AGL

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17
Q

Max Height for Autopilot Engaged in Single Channel Operation during Approach

A

Autopilot shall not be engaged below 50ft AGL

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18
Q

Max Headwind on Autoland Operations

A

25kts

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19
Q

Max Crosswind on Autoland Operations

A

20kts

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20
Q

Max Tailwind in Autoland Operations

A

15kts

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21
Q

Max Glideslope Angle for Autoland

A

3.25°

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22
Q

Min Glideslope Angle for Autoland

A

2.5°

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23
Q

Aircraft Config for Autoland Capability

A

Flaps 30 or 40 with Both Engines Operative

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24
Q

On Final Approach, do not use LVL CHG below

A

1,000ft AFE

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25
Q

Engine Ignition must be ON for

A

TakeOff, Landing, Operation in Heavy Rain & Anti-Ice operation

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26
Q

Operation with Assumed Temp Reduced T/O Thrust is not permitted with

A

Anti-Skid Inop

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27
Q

Intentional selection of Reverse Thrust in Flight is

A

Prohibited

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28
Q

Max Altitude for APU Bleed + Electrical Load in flight

A

10,000ft

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29
Q

Max Altitude for APU Bleed + Electrical Load on Ground

A

15,000ft

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30
Q

Max Altitude For APU Bleed

A

17,000ft

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31
Q

Max Altitude For APU Electrical Load

A

41,000ft

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32
Q

APU Bleed Valve Must Be Closed When :

A
  1. Ground Air Connected & Isolation Valve Open
  2. ENG NO 1 Bleed Valve Open
  3. Isolation Valve & ENG NO 2 Bleed Valve Open
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33
Q

Precautions for APU Bleed Valve Open during Engine Start

A

Avoid Engine Power Above IDLE

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34
Q

Required cooling period duration following 3 consecutive aborted start attempts

A

15 Mins

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35
Q

15 mins cooling period is required after :

A

3 Consecutive Aborted Start Attemps

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36
Q

Max Altitude With Flaps Extended

37
Q

Holding in Icing Condition With Flaps Extended

A

Is Prohibited

38
Q

Use Of Speed Brake lever In Flight

A

Do Not Extend Beyond FLIGHT DETENT

39
Q

Min Altitude for Speed Brake Deployment

A

1,000ft Radio Altitude

40
Q

Alternate Flap Duty Cycle : When Extending or Retracting flaps with ALTERNATE FLAPS position Switch -

A

Allow 15 seconds after releasing the switch before moving the switch again to avoid damage to alternate flap motor clutch

41
Q

Alternate Flap Duty Cycle : Cooling Period after extending Flaps 0 to Flaps 15, then back to Flaps 0

A

Allow 5 min cooling before attempting another extension

42
Q

ADIRU Alignment must not be attempted at latitudes greater than

A

78°15mins

43
Q

Max Tank Fuel Temp

44
Q

Min Tank Fuel Temp prior to T/O & Inflight

A
  • 43°C or 3°C above fuel freezing point temp, whichever is higher
45
Q

Random Fuel Imbalance between Main Tank 1 & 2 for Taxi, T/O, flight or landing

46
Q

Main Tanks 1&2 must be full if centre tank contains more than

47
Q

Max EGT & Time Limit For Starting

A

725°C & No Limit

48
Q

Max EGT & Time Limit for Max Continuous

A

925°C & No Limit

49
Q

Max EGT & Time Limit For T/O

A

950°C & 5 Mins

50
Q

Minimum Oil Pressure

51
Q

Max Oil Temp for Continuous Operation

52
Q

Max Oil Temp

53
Q

Max Oil Temp and Time Limit

A

Between 140°C to 155°C for 45 mins

54
Q

Max Demonstrated T/O & Landing Crosswind on Dry Runway (SOP)

55
Q

Tolerance acceptable when determining T/O Trim

A

0.75 Trim Units (3.4% MAC)

56
Q

Compartment Weight Limits

A

Compartment 1 : 888kgs
Compartment 2 : 2,670kgs
Compartment 3 : 4,086kgs
Compartment 4 : 736kgs

57
Q

Weight Limit Compartment 1

58
Q

Weight Limit Compartment 2

59
Q

Weight Limit Compartment 3

60
Q

Weight Limit Compartment 4

61
Q

Max Operating Limit Speed for Flaps 1-5

62
Q

Max Operating Limit For Flaps 10

63
Q

Max Operating Limit for Flaps 15

64
Q

Max Operating Limit For Flaps 25

65
Q

Max Operating Limit For Flaps 30

66
Q

Max Operating Limit For Flaps 40

67
Q

Max Speed when flaps are extended using STBY System

68
Q

LDG Gear Retraction Speed

69
Q

LDG Gear Extend Speed

A

270kts / 0.82M

70
Q

LDG Gear Extended Speed

A

320kts / 0.82M

71
Q

Max Tailwind Component when RWY Length less than 2500m

72
Q

Max Crosswind On WET RWY

73
Q

Max Crosswind For Contaminated RWY (Water, Slush, Snow)

74
Q

Max Crosswind For RWY COND CODE 5 (Good)

75
Q

Max Crosswind For RWY COND CODE 4 (Good To Medium)

76
Q

Max Crosswind For RWY COND CODE 3 (Medium)

77
Q

Max Crosswind For RWY COND CODE 2 (Medium To Poor)

78
Q

Max Crosswind For RWY COND CODE 1 (Poor)

79
Q

Co-Pilot Limitations for T/O & Landing

A

Straight In Approach
Visibility 1600M
Ceiling 500ft
Crosswind Less than 15kts
Cat II Approaches (As PM Only)

80
Q

Max Crosswind For Contaminated RWY (Ice)

81
Q

Max Allowable Cabin Pressure Differential for T/O & Landing

82
Q

Differential Pressure Limit at or below 28,000ft

83
Q

Differential Pressure Limit at 28,000ft to 37,000ft

84
Q

Differential Pressure Limit for Above 37,000ft

85
Q

Both Centre Tank Fuel Pump Switches must be 1.______ for T/O if Centre Tank Fuel is less than 2.______

A
  1. OFF
  2. 460kgs (SOP)
86
Q

Max Deviation between FMC Data Base & Raw Data

A

3°. If more than 3° use raw data as primary navigation

87
Q

Window heat must be 1._____ at least 2._______ before T/O

A
  1. ON
  2. 10 Mins
88
Q

Max Thrust Limit Engine

89
Q

When is NOT RECOMMENDED to exercise One Engine Taxi In

A
  1. Visibility Less than 5KM
  2. Wind Speed more than 25kts and/or gusts of more 10kts
  3. Significant Slope Exists

B737NG Limitations (FCOM) (1 decks)

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