Limitations // Good things to know Flashcards

1
Q

Max RWY upslope / downslope

A

+ / - 2%

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2
Q

Max T/O LDG tailwind

A

Classic: 10kts (may be 15kts customer option)
NG: 15kts

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3
Q

Max windspeed for taxi

A

65kts

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4
Q

Turbulent airspeed 3/500

A

280kts/.73M

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5
Q

Turbulent airspeed 6/900

A

280kts/.76M

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6
Q

Max operating altitude 1/500

A

37000ft

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7
Q

Max operating altitude 6/900

A

41000ft

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8
Q

Maximum T/O and LDG altitude

A

8400ft (12000ft high altitude option)

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9
Q

Max dry snow depth for T/O or LDG

A

60mm

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10
Q

Max water / wet snow / slush depth for T/O or LDG

A

13mm

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11
Q

Max demonstrated crosswind 3/500

A

35kts

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12
Q

Max demonstrated crosswind 6/900 (no winglets)

A

36kts

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13
Q

Max demonstrated crosswind 6/900 (winglets)

A

33kts

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14
Q

Do the SBY altimeters meet the requirements for RVSM airspace?

A

No

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15
Q

Max in flight difference between FO and Captain altitude displays in RVSM airpsace?

A

200 feet

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16
Q

At sea level, what is the max difference between the Captain and FOs altimeter display on the ground for RVSM ops? (737 1/500)

A

40ft (75 foot between either altimeter and field elevation)

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17
Q

Between sea level and 5000 feet, what is the max difference between the Captain and FOs altimeter display on the ground for RVSM ops? (737 NG)

A

50 ft (75 ft between either altimeter and field elevation).

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18
Q

With one pack inoperative, what’s the max altitude one can fly at?

A

FL250

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19
Q

Engine anti-ice must be on during all ground and flight operations when icing conditions exist or are anticipated, except during climb and cruise below which temperature?

A

-40C SAT

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20
Q

Do not use wing anti-ice on the ground when the OAT is above which temperature?

A

10C

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21
Q

Window heat inop: max speed below 10,000ft?

A

250kts

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22
Q

Max windspeed for operation of airstairs?

A

40kts

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23
Q

Max windspeed that airstairs may remain extended?

A

60kts

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24
Q

Do not engage the autopilot for takeoff below which height? (737 3/500)

A

1000ft AGL

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25
Q

For single channel operation, on approach; the autopilot shall not be engaged below which height?

A

158ft AGL (EASA)

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26
Q

For 737 3/500, Maximum allowable wind speeds, when conducting a dual channel Cat II or Cat III landing predicated on autoland operations, are?

A

Headwind 25 knots
Crosswind 15 knots
Tailwind: 10knots

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27
Q

Do not engage the autopilot for takeoff below which height? (737 6/900)

A

400ft AGL

28
Q

For 737 6/900; Maximum allowable wind speeds, when conducting a dual channel Cat II or Cat III landing predicated on autoland operations, are: (EASA)

A

. Headwind 25 knots
. Crosswind 20 knots
. Tailwind:
- Flap 30: 12kts
- Flap 40: 15kts

29
Q

What is the TR voltage range?

A

24-30V

30
Q

What is the battery voltage range?

A

22-30V (may rise to 33V during pulse mode charging)

31
Q

What is the max altitude for flap extension?

A

20,000ft

32
Q

What is the lowest height for speedbrake extension?

A

1000ft RA

33
Q

What is the maximum fuel temperature?

A

+49C

34
Q

What is the minimum fuel temperature for 737-1/500?

A

-45C (or freeze point +3C)

35
Q

What is the minimum fuel temperature for 737-6/900?

A

-43C (or freeze point +3C)

36
Q

What is maximum lateral fuel imbalance?

A

453kgs (1000lbs)

37
Q

The main fuel tanks must be full if the centre tank contains more than ___kg

A

453kgs

38
Q

For ground operation, centre tank pumps must be not be positioned to __, unless defuelling or transferring fuel, if quantity is below ___kgs.

A

ON, 453kgs

39
Q

Centre tank pumps must be switched ___ when both LP lights illuminate

A

OFF

40
Q

Regarding hydraulic systems, what is the minimum % required for despatch?

A

88%

41
Q

Max speed for gear extension?

A

270kt / 0.82

42
Q

Max speed for gear retraction?

A

235kt

43
Q

Max speed with gear extended?

A

320kt / 0.82

44
Q

Do not operate main deck cargo door in wind speeds above?

A

45kts

45
Q

Maximum N1 RPM? (Classic)

A

106%

46
Q

Maximum N2 RPM? (Classic)

A

105%

47
Q

Maximum continuous EGT? (Classic)

A

895C

48
Q

When must continuous ignition be on (CONT position)

A

T/O, landing and during engine anti-ice operations

49
Q

Max cabin differential pressure

A

Classic 8.65 psi
NG 9.10 psi

50
Q

Minimum width of pavement for a 180 turn?

A

300: 20m (just under)
400: 23m (just under)
800: 24.3 metres

51
Q

Wingspan of 300, 400 and 800?

A

300: 29m
400: 29m
800: 36m

52
Q

What is Vmo / Mmo?

A

340kts IAS / 0.82M

53
Q

After three consecutive start attempts, a cooling period of how long is required?

A

Fifteen minutes

54
Q

Max altitude for APU supplying bleed air and electrical load?

A

10,000ft (EASA)

55
Q

Max altitude for APU supplying bleed air alone?

A

17,000ft

56
Q

NG: Max altitude that APU can supply electrical load alone?

A

37,000ft Classic
41,000ft NG

57
Q

Minimum quantity in each main fuel tank for electrical hydraulic pump operation?

A

760kgs

58
Q

Minimum engine warm up time?

A

Two minutes from engine start to take off thrust

59
Q

Minimum engine cool down time?

A

Three minutes at idle

60
Q

Max EGT for Takeoff? (Classic)

A

930C (940C permissable if transient, for 20 seconds)

61
Q

Max EGT at start?

A

725C

62
Q

When flying in moderate or heavy rain, hail or sleet, what must we do?

A

Set engine start switches to FLT, maintain N1 to minimum 45%, except on short final when landing is assured

63
Q

Max continuous N1 (NG)

A

104%

64
Q

Max continuous N2 (NG)

A

105%

65
Q

Max takeoff EGT (NG)

A

950C

66
Q

Max continuous EGT (NG)

A

925C