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B737CL Type Rating > Limitations > Flashcards

Limitations Flashcards

1
Q

Runway slope

A

+ / - 2%

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2
Q

Max. T/O and Landing Tailwind component

A

10 knots

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3
Q

Maximum speeds

A

Observe Vmo pointed and gear / flaps placards

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4
Q

Maximum flight operational latitude

A

73 North / 60 South

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5
Q

Maximum operating altitude

A

37000 ft

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6
Q

Maximum T/O and landing altitude

A

8400 ft

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7
Q

Severe turbulent air penetration speed

A

280 KIAS / .73M Applicable to Climb and Descent only

During Cruise, refer to SP.16, Severe Turbulence Supplementary Procedure

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8
Q

Standby altimeters do not meet altimeter accuracy requirements of RVSM airspace.

True or false?

A

True

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9
Q

The maximum allowable in-flight difference between Captain and First Officer altitude displays for RVSM operations

A

200 ft

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10
Q

The maximum allowable on-the-ground altitude display differences for RVSM operations are

A

Memory

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11
Q

Possible conflicts between the AFM and the FCOM may occur due to separate publication release dates. In the event of a conflict between the FCOM and the AFM

A

the AFM shall govern

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12
Q

Maximum Taxi Weight

A

29337 & 29341 :
128,500 lbs (58,286 kgs)

28558 :
140,000 lbs (63,502 kgs)

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13
Q

Maximum Takeoff Weight

A

29337 & 29341:

128,000 lbs (58,059)

28558:

139,500 lbs (63,276 kgs)

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14
Q

Maximum Landing Weight

A

29337 & 29341:

114,000 lbs (51,709 kgs)

28558:

114,000 lbs (51,709 kgs)

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15
Q

Maximum zero fuel weight

A

29337 & 29341:
105,000 lbs (47,627kgs)

28558:

105,000 lbs (47,627 kgs)

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16
Q

The maximum cabin differential pressure (relief valves) is:

Air system

A

8.65 psi

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17
Q

Do not use aileron trim with:

A

autopilot engaged.

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18
Q

Maximum and minimum glideslope angles for autoland

A

3.25 degrees and 2.5 degrees respectively.

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19
Q

Do not use LVL CHG on final approach below

A

1000 ft AFE

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20
Q

Maximum generator drive oil temperature

A

157° C

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21
Q

Maximum and minimum limits are

A

Red

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22
Q

Caution limits are

A

Amber

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23
Q

Maximum time limit for takeoff thrust

A

5 minutes

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24
Q

Maximum N1 RPM

A

106%

25
Q

Maximum N2 RPM

A

105%

26
Q

Maximum Takeoff EGT

A

930

27
Q

Maximum Continuous EGT

A

895

28
Q

Maximum Start EGT

A

725

29
Q

Minimum Oil Pressure

A

13 psi

30
Q

Maximum Oil Temperature

A

165° C maximum
160° C – 165° C allowable for 15 minutes
160° C maximum continuous

31
Q

Continuous ignition must be on (ENGINE START switch in the CONT position) during

A

takeoff and landing and during engine anti–ice operations

32
Q

When flight in moderate or heavy rain, hail, or sleet is encountered or anticipated, engine start switches must be set to

A

FLT and a minimum of 45% N1 must be maintained except on short final when landing is assured

33
Q

Both PMCs must be either

A

OFF or ON for takeoff

34
Q

Intentional selection of reverse thrust in flight is…

A

Prohibited

35
Q

APU Maximum start EGT is

A

760° C

36
Q

APU Maximum continuous EGT is

A

710° C

37
Q

With APU bleed + electrical load, maximum altitude is

A

10,000 ft

38
Q

With APU bleed, maximum altitude is

A

17,000 ft

39
Q

APU can operate up to

A

37,000 ft

40
Q

With APU electrical load, maximum altitude is…

A

35,000 ft

41
Q

Pneumatic pressure (prior to starter engagement)

A

minimum 30 psig at sea level, decreasing 1/2 psig per 1,000 ft. above sea level.

42
Q

APU bleed valve must be closed when:

A
  • ground air connected and isolation valve open •engine no. 1 bleed valve open
  • isolation valve and engine no. 2 bleed valve open.
43
Q

APU bleed valve may be open during engine start, but …

A

avoid engine power above idle

44
Q

APU
If there are multiple aborted start attempts … minutes of cooling is required between the second and third start attempt.

A

5

45
Q

APU

A wait of… is required after the third start attempt.

A

One hour

46
Q

The maximum altitude with flaps extended is

A

20,000 ft

47
Q

In flight, do not extend the SPEED BRAKE lever beyond the…

A

FLIGHT DETEND

48
Q

Do not deploy the speedbrakes in flight at radio altitudes less than…

A

1000 ft

49
Q

When extending or retracting flaps with the ALTERNATE FLAPS position switch, allow … after releasing the ALTERNATE FLAPS position switch before moving the switch again to avoid damage to the alternate flap motor clutch

A

15 minutes

50
Q

After a completed extend/retract cycle, i.e., 0 to 15 and back to 0, allow … cooling before attempting another extension.

A

5 minutes

51
Q

Avoid weather radar operation in …, or within … of fueling operations or a fuel spill.

A

A hangar - 50 feet (15.25 meters)

52
Q

The hangar recommendation does not apply to… .

A

the weather radar test mode.

53
Q

Do not reset a tripped … circuit breaker

A

Fuel pump

54
Q

Maximum fuel temperature is… .

A

49°C.

55
Q

Inflight tank fuel temperature must be maintained at least … or … , whichever is higher.

A

3°C above the freezing point of the fuel being used / –45°C

56
Q

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

A

Zero

57
Q

Random fuel imbalance must not exceed … for taxi, takeoff, flight, or landing.

A

1,000 lbs (453 kgs)

58
Q

Main tanks 1 and 2 must be scheduled to be full if center tank contains more than … of fuel.

A

1,000 lbs (453 kgs)

59
Q

Do not apply brakes until …

A

after touchdown

B737CL Type Rating (6 decks)

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