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Verklegt > Boeing 737 limitations > Flashcards

Boeing 737 limitations Flashcards

1
Q

A typical maximum landing weight of the B737-800 is

A

65,317 Kg

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2
Q

The maximum T/O and landing tailwind component on a dry or wet runway (non contaminated) is ?

A

10 kts (or 15kts as certified) including gusts.

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3
Q

The maximum speed with the MACH TRIM system inoperative is?

A

280/0.82M

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4
Q

The severe air turbulent penetration airspeed for climb and descent is

A

280Kts/0.76M

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5
Q

The maximum time limit for take-off thrust is

A

Usually 5 minutes but can be 10 minutes as a customer option

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6
Q

The maximum speed for landing gear extension is

A

270 kt. or .82M

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7
Q

The maximum speed for landing gear retraction is

A

235 Kts

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8
Q

The maximum speed for landing gear extended is

A

320 kt. or .82M

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9
Q

Engine ignition must be on for:

A

takeoff, landing, operation in heavy rain, anti-ice operation. (EKKI engine-out ops).

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10
Q

The maximum wind speed for airstair operation is

A

40 Kts

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11
Q

The runway slope limits are __ %

A

+/- 2 %

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12
Q
A
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13
Q

Maximum takeoff and landing altitude

A

8400 feet pressure altitude

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14
Q

The maximum differential pressure is __ PSI

A

NG: 9.1 psi

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15
Q

Maximum operating altitude

A

41,000 feet pressure altitude

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16
Q

Maximum takeoff and landing altitude

A

8400 feet pressure altitude

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17
Q

Severe turbulent air speed is __KIAS/__M

A

.76M / 280 kts

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18
Q

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

A

200ft

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19
Q

Hvað máttu nota APU bleed og electrical load lang uppi? En ef þú notar bara bleed? En bara electrical load?

A

Upp að 10,000 ft.
Bara bleed: 17,000 ft.
Bara electrical load: 41,000 ft.

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20
Q

The maximum altitude with flaps extended is ___ feet.

A

20,000 ft

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21
Q

Do not use speed brakes below ___ feet above the surface

A

1000ft

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22
Q

In flight, do not extend the speedbrake lever beyond the setting ______ with
flaps ___selected.

A

ARMED detent, 40 kts

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23
Q

Flaps ___ normal landings are
prohibited

A

15

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24
Q

Maximum tank fuel temperature is __°C

A

49°C

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25
Q

Minimum tank fuel temperature prior to takeoff and inflight is __°C, or 3°C
above the fuel freezing point temperature, whichever is higher.

A

-43°C

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26
Q

Fuel imbalance á milli tanka má mest vera

A

453 kgs

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27
Q

Hvað þarftu að passa ef center tank er með meira en 453 kgs?

A

Main tank 1 og 2 verða að vera fullir.

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28
Q

The maximum cabin differential pressure for take-off and landing is

A

.125 psi

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29
Q

Þú ert að starta vél. Hvernig þarf APU bleed valve að vera?

A

Má vera opinn en ekki vera með meira en idle engine power

30
Q

Þú ert búinn að reyna að starta APU þrisvar sinnum, hvað þarftu núna að gera?

A

Leyfa þessu að kólna í 15 mínútur

31
Q

The maximum aircraft altitude for APU generator use is (Boeing Max)

A

41,000 ft.

32
Q

The battery voltage range is

A

22-30 volts

33
Q

Do not use the HUD System at latitudes greater than:

A

85 degrees latitude

34
Q

When should window heat switched on

A

10 minutes before take-off.

35
Q

The maximum external air pressure (ground cart) is

A

60 PSI (at 232 degrees C).

36
Q

The maximum EGT for take-off is ___ °C

A

930 degrees C

37
Q

The maximum start engine EGT is ___ °C

A

725 degrees C

38
Q

The minimum engine oil pressure is

A

13 psi

39
Q

The maximum continuous engine oil temperature is

A

160 degrees C

40
Q

The minimum operating brake pressure indication is ___ PSI

A

2800 psi

41
Q

The minimum start pressure at 2000 feet above sea level (prior to starter engagement) is ___ PSI

A

29 psi

42
Q

The recommended refuelling nozzle pressure is ___ psi

A

50 psi

43
Q

Do not operate engine or wing anti-ice when the temperature is above ___ OAT/SAT/TAT?

A

10°C TAT

44
Q

The manoeuvre speed with flap 5 (gross weight of 52,000 kgs) is __ kts

A

170 kts

45
Q

Starter assist (inflight engine start) should be used when N2 is below __ %

A

15%

46
Q

The flight operating latitude limits of the B737NG are MOSTLY __ degrees North and __ degrees South

A

82°

47
Q

When engine bleeds are ON, both air conditioning packs must be set to

A

AUTO or OFF for take-off, approach or landing.

48
Q

When engine bleeds are ON, both air conditioning packs must be set to

A

AUTO or OFF for take-off, approach or landing.

49
Q

Except for ER operation, one air-conditioning pack may be inoperative provided altitude is limited to FL ___

A

FL 250

50
Q

For single channel operation, the autopilot shall not be engaged below ___ feet AGL

A

140 ft

51
Q

The maximum lateral fuel imbalance between wing tanks 1 and 2 must be scheduled to be zero and, for all phases of flight, must not exceed ___ kgs.

A

453 kgs

52
Q

The engine Thermal Anti Ice must be on when icing conditions exist or are anticipated, except during climb or cruise when the temperature is below -40°C OAT/SAT eða TAT?

A

SAT

53
Q

Á hvaða stigum þarftu að vera með engine ignition on?

A

Take off og landing (ekki approach)

54
Q

The maximum continuous engine EGT is ___ °C

A

895

55
Q

The maximum allowable engine oil temperature is ___ °C

A

165 °C

56
Q

The engine start duty cycle (normal start) is First attempt: 2 minutes on, 20 seconds off
Second and subsequent attempts: 2 minutes on, __ minutes off

A

3 minutes

57
Q

Both PMCs must be ON/OFF for take-off

A

rétt er on or of, bara ekki t.d. servicable for take off

58
Q

What are the max differential restrictions when ANY window in the cockpit has a cracked outer pane?

A

No restrictions

59
Q

What is the minimum engine oil quantity (per engine) for despatch for an aircraft with EIS?

A

75% full

60
Q

For a 737NG automatic landing the head and crosswind limits are Headwind limit is __ kts and the crosswind limit is __ kts.

A

í landing er max headwind 25 kts og crosswind 20 kts

61
Q

The maximum tailwind for T/O and landing on a contaminated runway is __ kts

A

0 kts

62
Q

The maximum windspeed for taxying is ___ kts

A

65 kts

63
Q

The maximum depth of Dry Snow (runway contaminant) for take-off based on maximum figures available for calculation of performance is ___ mm

A

60mm

64
Q

The maximum depth of Wet Snow (runway contaminant) for take-off based on maximum figures available for calculation of performance is __ mm

A

15 mm

65
Q

The maximum depth of Compacted Snow/Slush (runway contaminant) for take-off based on maximum figures available for calculation of performance is ___

A

13 mm

66
Q

The maximum depth of Standing Water (runway contaminant) for take-off based on maximum figures available for calculation of performance is ___ mm

A

13 mm

67
Q

The 737NG maximum demonstrated crosswind component for taking-off and landing is ___ kts (with winglets)

A

33 kts með winglets. (þolir meiri crosswind ef það er ekki winglet).

68
Q

The maximum crosswind component (including gusts) for taking-off and landing on a runway where braking action is reported as MEDIUM is ___ kts

A

25 kts.

69
Q

The maximum crosswind component (including gusts) for taking-off and landing on a runway where braking action is reported as MEDIUM/POOR is ___ kts

A

20 kts

70
Q

What is the category of the B737 brakes ?

A

Category A brakes

71
Q

Hvaða category er Boeing 737?

A

CAT C

Verklegt (42 decks)

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