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PSA > 200/700/900 Limitations > Flashcards

200/700/900 Limitations Flashcards

1
Q

Maximum 90° crosswind for takeoff and landing

A

27 knots

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2
Q

Maximum 90 crosswind for takeoff and landing from a CAT II approach

A

15 knots

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3
Q

Maximum headwind for landing from a CAT II approach

A

16 knots

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4
Q

Maximum direct tailwind for takeoff and landing

A

10 knots

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5
Q

Maximum operating altitude (200)

A

36,000

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6
Q

Maximum operating altitude (700/900)

A

41,000

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7
Q

Minimum runway width for takeoff and landing

A

100 ft

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8
Q

Turbulence penetration speed

A

280 knots/.75 mach whichever is lower

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9
Q

Maximum gear extension speed

A

220 knots

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10
Q

Maximum gear extended speed

A

220 knots

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11
Q

Maximum gear retraction speed

A

200 knots

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12
Q

Maximum airspeed for windshield wiper operation

A

220 knots

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13
Q

Maximum cruise mach in RVSM airspace

A

.82 mach

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14
Q

Bleed air extraction from the APU is not permitted above:

A

(200)
15,000 ft

(700/900)
25,000 ft

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15
Q

If both engines are to be started using APU bleed air, the operating engines thrust must not exceed…

A

(200)

70% N2

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16
Q

With the APU door not closed or the door position is unknown, the airplane must be limited to…

A

(200)
300 knots

(700/900)
220 knots

Or

The APU must remain in operation

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17
Q

Max AC main generator loading

A

(200)
0-35,000 ft: 30 kVa
35,001-36,000 ft: 25 kVa

(700/900)
40 kVa

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18
Q

Max AC APU generator loading

A

(200)
30 kVa

(700/900)
40 kVa

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19
Q

Maximum continuous load on each TRU:

A

(200)
100 amps

(700/900)
120 amps

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20
Q

Maximum permissible time for ground operations with DC power only…

A

5 minutes

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21
Q

Do not exceed 75% N1 until how long after start?

A

2 minutes

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22
Q

Operate engines at or near idle for ____ minutes prior to shutdown.

A

2 minutes

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23
Q

Max ITT for start

A

(200)
900

(700/900)
815

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24
Q

Minimum oil pressure for takeoff

A

45 PSI

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25
Q

Continuous ignition must be used during the following:

A

Takeoff and landing on contaminated runways

Takeoff with crosswind 15 knots or greater

Flight through moderate or heavy rain

Flight through moderate or heavy turbulence

Flight in the vicinity of thunderstorms

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26
Q

At initiation of thrust lever movement from SHUTOFF to IDLE…

A

ITT must be 120°C or less for all ground starts

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27
Q

During landing, maximum reverse thrust is prohibited before ____ knots, and reverse idle should be achieved by ____ knots.

A

75 knots

60 knots

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28
Q

Maximum slats and/or flaps extended altitude

A

15,000 ft

29
Q

To ensure adequate maneuvering margins, flight spoilers must not be extended in flight at airspeeds below the recommended reference speed plus….

A

17 knots

30
Q

Maximum fuel imbalance for takeoff:

A

(200)
800lbs

(700/900)
300

31
Q

Maximum fuel imbalance for all other phases of flight:

A

800 lbs

32
Q

Takeoff with a fuel load in excess of ____ lbs in the center tank is not permitted unless each wing tank is above ____ lbs.

A

500 lbs

4400 lbs

33
Q

Minimum fuel quantity per wing tank for a go-around

A

(200)
450 lbs

(700/900)
600 lbs

34
Q

Ground contamination definition

A

Runway, ramps or taxiways with surface snow, ice, slush or standing water

35
Q

Visible moisture definition

A

Visible moisture or precipitation in any form (such as fog with visibility of one mile or less, mist, rain, snow, sleet and ice crystals or clouds inflight)

36
Q

If visible moisture is present below ____ with OAT ____ or below activate ____ for takeoff.

A

400 ft AGL

10 C

Cowl anti-ice

37
Q

If visible moisture is present below ____ with OAT ____ or below activate ____ for takeoff.

A

400 ft AGL

5 C

Cowl and Wing anti-ice

38
Q

Wing anti-ice must be selected ____ during the final ____ prior to takeoff during all ground operations at temperatures of ____ or below unless Type IV anti-icing fluid has been applied.

A

ON

2 minutes

5 C

39
Q

A tactile check is required when…

A

The OAT is 10 C or less, or

The bulk fuel temperature is 0 C or less, or

The atmospheric conditions have been conducive to frost formation, or

Ice and frost may continue to adhere to wing surfaces for some time even at outside temperatures above 10 C

40
Q

Taxi lights must be switched ____ whenever the airplane is stationary in excess of ____.

A

OFF

10 minutes

41
Q

Minimum brake cooling time is ____, and all BTMS indicators must be green and ____.

A

15 minutes

not increasing

42
Q

CAT II approaches are ____ when the braking action is reported as less than ____.

A

PROHIBITED

Medium

43
Q

Use of SPEED MODE, flight director or autopilot coupled, during an approach is ____.

A

Not permitted.

44
Q

Use of VNAV, flight director or autopilot coupled, during the climb and approach phases of flight is ____.

A

Not permitted

45
Q

The minimum height for autopilot use is ____, except for visual and non precision approaches which is ____, precision approaches is ____, and precision approaches with one engine is ____.

A

600 ft AGL

400 ft AGL

80 ft AGL

110 ft AGL

46
Q

Maximum taxi and ramp weight (200)

A

53,250 lbs

47
Q

Maximum takeoff weight (200)

A

53,000 lbs

48
Q

Maximum landing weight (200)

A

47,000 lbs

49
Q

Maximum zero fuel weight (200)

A

44,000 lbs

50
Q

Maximum taxi and ramp weight (700)

A

75,250 lbs

51
Q

Maximum takeoff weight (700)

A

75,000 lbs

52
Q

Maximum landing weight (700)

A

67,000 lbs

53
Q

Maximum zero fuel weight (700)

A

62,300 lbs

54
Q

Maximum landing weight (900)

A

85,000 lbs

55
Q

Maximum takeoff weight (900)

A

84,500 lbs

56
Q

Maximum landing weight (900)

A

75,100 lbs

57
Q

Maximum zero fuel weight (900)

A

70,750 lbs

58
Q

If ground contamination or visible moisture is present and the temperature is 10 C or below, the ____ anti-ice must be on. (For taxi)

A

Cowl

59
Q

If ground contamination or visible moisture is present and the temperature is 10 C or below, the ____ anti-ice must be on. (For takeoff)

A

Cowl

60
Q

If ground contamination or visible moisture is present and the temperature is 5 C or below, the ____ anti-ice must be on. (For takeoff)

A

Wing and cowl

61
Q

If visible moisture is present and the temperature is from ____ to ____, and if the airspeed is greater or equal to ____, the ____ anti-ice must be on. If the airspeed is less than ____, the ____ anti-ice must be on. (In flight)

A

10 C TAT

-39 C SAT

230 knots

Cowl

230 knots

Wing and cowl

62
Q

____ thrust may be applied before brake released when the wind is within 30° of the airplane nose with no windspeed limit or if the windspeed is <5 knots it can be >30° of the airplane nose

A

TOGA

63
Q

Apply max of ____ before brake release, then ____ thrust, when the wind is >30° off the nose and the windspeed is between 5 and 30 knots.

A

75% N1

TOGA

64
Q

Apply max of ____ thrust before brake release, then ____ thrust when the wind is >30° off the nose and the windspeed is >30 knots.

A

Idle/taxi

TOGA

65
Q

Starter cranking limits (200)

A

60 sec on, 10 sec off
60 sec on, 10 sec off
60 sec on, 5 min off

66
Q

Starter cranking limits (700/900)

A

90 sec on, 10 sec off
90 sec on, 10 sec off
90 sec on, 5 min off

67
Q

APU starter cranking limits (200)(on battery)

A

30 sec on, 2 min off
30 sec on, 20 min off
30 sec on, 2 min off
30 sec on, 40 min off

68
Q

APU starter cranking limits (200)(on ground power)

A

15 sec on, 2 min off
15 sec on, 20 min off
15 sec on, 2 min off
15 sec on, 40 min off

PSA (2 decks)

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