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Aloha Air B737 > Limitations > Flashcards

Limitations Flashcards

1
Q

Max operating altitude

A

37,000 feet

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2
Q

N301KH Max taxi weight

A

140,000 pounds

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3
Q

Max takeoff weight

A

139,500 pounds

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4
Q

Maximum landing weight

A

116,000 pounds

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5
Q

Maximum zero fuel weight

A

109,000 pounds

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6
Q

Minimum operating weight

A

78,000 pounds

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7
Q

Maximum cabin differential pressure

A

8.65 psi

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8
Q

Minimum altitude for auto pilot engage

A

1000 feet

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9
Q

Maximum time limit for takeoff trust

A

Five minutes

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10
Q

Maximum N1 RPM

A

106%

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11
Q

Maximum N2 RPM

A

105%

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12
Q

Maximum takeoff EGT

A

940°C

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13
Q

Max continuous EGT

A

895°C

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14
Q

Maximum start EGT

A

725°C

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15
Q

Minimum oil pressure

A

13 psi

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16
Q

Maximum oil temperature

A

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

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17
Q

Engine ignition

A

Continuous ignition must be on during takeoff and landing and during engine anti-ice operations

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18
Q

Do not open MAIN DECK CARGO DOOR in actual or anticipated winds exceeding

A

45 knots

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19
Q

Aircraft is not to be taxied, towed or, jacked unless the MAIN CARGO DOOR is

A

In the fully closed and latched position

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20
Q

How many packs need to be operational for cargo to be in the cabin compartment?

A

At least one pack needs to be operational

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21
Q

Max runway slope

A

+/- 2%

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22
Q

Max tailwind component

A

10 knots

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23
Q

Designed speed for max gust intensity

A

264/.65mach

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24
Q

Operational check of flight deck door

A

Once a day

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25
Q

Don’t not operate HF radio durning?

A

Refueling

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26
Q

Severe turbulence air penetration speed

A

280/.73 Mach

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27
Q

Max allowable difference between CAPT. and FO alt. Display for RVSM

A

200 feet

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28
Q

What direction does the Forward Center the gravity move as weight goes up?

A

Aft

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29
Q

Maximum N1 RPM

A

106%

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30
Q

Maximum N2 RPM

A

105%

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31
Q

Maximum take off EGT

A

940°C

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32
Q

Maximum continuous EGT

A

895°C

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33
Q

Maximum start EGT

A

725°C

34
Q

Minimum oil pressure

A

13 psi

35
Q

Maximum oil temperature

A

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

36
Q

Aircraft is not to be taxi towed or jacked unless the main cargo door is in the

A

Fully closed and latched position

37
Q

 Main deck cargo compartment smoke detector system

A

Pre-flight of the system is required prior to each flight or series of flights by the same crew on the same day

38
Q

Flight with freight in the Main deck cargo compartment without at least what is prohibited

A

One air conditioning pack operating

39
Q

Secondary main Landing gear position indicating system

A

Preflight inspection of the system is required prior to each flight or series of flights by the same crew on the same day

40
Q

Weight and balance control and loading limitations

A

Refer to the weight and balance control and loading manual supplements

41
Q

Main cargo compartment air supply shut off

A

Functionally operate the main cargo compartment air supply shut off valve to ensure proper operation prior to each flight or series of flights by the same crew on the same day

42
Q

Lower cargo compartment activation of BTL 1 accomplishing Cargo fire smoke class C procedure

A

Aircraft must land at the nearest suitable airport within 60 minutes after activation

43
Q

Maximum speeds

A

Observe VMO pointer and gear/flap placard

44
Q

What kind of check does the flight deck door access system go through each day

A

Operational check

45
Q

Do you not operate HF radio’s during when

A

Refueling

46
Q

Altitude display limits for RVSM

A

Standby altimeters do not meet altimeter accuracy requirements of RVSM

47
Q

Maximum allowable inflight difference between captain and first officer altitude display for RVSM. 

A

200 feet

48
Q

Maximum allowable on the ground altitude display differences for RVSM

A

Max difference between Captain and FO
Sea level 40 feet
5000’… 45 feet
10,000 … 50 feet

Max difference between Captain FO and Field elevation
75 feet for sea level 5000 feet and 10,000 feet

49
Q

What do CG limits use

A

Approved weight and balance systems

50
Q

What happens to the Forward Center of gravity limit as weight is added

A

Center of gravity moves aft

51
Q

Functionally operate the main cargo compartment ….. to ensure proper operation prior to each flight… Or series of flights

A

Air supply shut off valve

52
Q

With either one or both engine bleed air switched on Do not operate the air conditioning packs in …… for takeoff approach or Lanning

A

High

53
Q

What kind of trim is prohibited one auto pilot is engaged

A

Aileron trim

54
Q

Do you not engage the auto pilot for takeoff below what altitude

A

1000 feet

55
Q

For a single channel operation during approach the auto pilot shall not remain engaged below

A

50 feet AGL

56
Q

Do not use Flight level change on final approach below 

A

Thousand feet

57
Q

Maximum generator drive oil temperature

A

157°C

58
Q

Engines and APU engine limit display markings

A

Maximum and minimum limits are red caution limits are Amber

59
Q

Continuous ignition must be on during 

A

Takeoff landing and during engine anti ice operations

60
Q

Power management control (PMC) Must be ….. during takeoff

A

On or off

61
Q

Are we allowed to use reverse thrust in flight

A

No

62
Q

Minimum psig for start

A

Minimum 30 psig At sea level decreasing 1/2 psig Per thousand feet above sea level

63
Q

APU limitation altitudes

A

10,000 feet for APU bleed and electrical load
17,000 with APU bleed
37,000 is the max altitude for the APU and an electrical load

64
Q

APU bleed valve Must be closed

A

Ground air connected and isolation valve open
Engine number one bleed valve open
Isolation valve an engine two bleed valve open

65
Q

Bleed valve may be open during engine start but avoid engine power above

A

Idle

66
Q

How many starts may the APU have

A

Three consecutive aborted start attempts 30 minute cooling period

67
Q

Maximum altitude With flaps extended

A

20,000 feet

68
Q

Inflight do not extend speed brake lever beyond

A

The Flight detent

69
Q

Do not deploy speedbrakes in-flight at radio altitudes less than

A

1000 feet

70
Q

When extending or attracting flaps with the alternate flap position switch

A

Allow 15 seconds after releasing alternate flat position switch before moving to switch again to avoid damaging the alternate Flap motor clutch

71
Q

After a complete extend/retract cycle 0 to 15 and back to zero allow how much time

A

Five minutes cooling before attempt another extension

72
Q

Do not use the terrain display for what

A

Navigation

73
Q

Do not use the look ahead terrain alerting and terrain display functions

A

Within 15 nautical miles of takeoff approach and landing at an airport not contained in GPWS terrain database

The lookahead terrain alerting and terrain display functions must be inhibited by selecting the terrain inhibit switch to inhibit

74
Q

Avoid Weather radar operation in a hanger or 

A

Within 50 feet of fueling operations or a fuel spill

75
Q

Avoid weather radar operations when

A

Personnel are within the area normally enclosed by the aircraft nose radome 

76
Q

Can we reset fuel pump circuit breakers

A

No

77
Q

What fuels are prohibited for revenue flights

A

JP-4 and Jet B

78
Q

Random fuel imbalance must not exceed

A

1000 lbs for taxi, takeoff, or landing

79
Q

Main tanks 1 and 2 must be scheduled to full

A

If center tank contains more than a 1000 lbs

80
Q

Second main landing gear position indicating system

A

Requires a preflight inspection prior to each flight or series of flight by the same crew on the same day.

81
Q

Don’t apply brakes till

A

After touch down

Aloha Air B737 (10 decks)

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