200/700/900 Limitations Flashcards by Jacob Reiter

Maximum 90° crosswind for takeoff and landing

27 knots

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

15 knots

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Maximum headwind for landing from a CAT II approach

16 knots

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Maximum direct tailwind for takeoff and landing

10 knots

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Maximum operating altitude (200)

36,000

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Maximum operating altitude (700/900)

41,000

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Minimum runway width for takeoff and landing

100 ft

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Turbulence penetration speed

280 knots/.75 mach whichever is lower

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Maximum gear extension speed

220 knots

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Maximum gear extended speed

220 knots

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Maximum gear retraction speed

200 knots

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Maximum airspeed for windshield wiper operation

220 knots

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Maximum cruise mach in RVSM airspace

.82 mach

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Bleed air extraction from the APU is not permitted above:

(200)
15,000 ft

(700/900)
25,000 ft

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

(200)

70% N2

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

(200)
300 knots

(700/900)
220 knots

The APU must remain in operation

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Max AC main generator loading

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

(700/900)
40 kVa

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Max AC APU generator loading

(200)
30 kVa

(700/900)
40 kVa

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Maximum continuous load on each TRU:

(200)
100 amps

(700/900)
120 amps

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Maximum permissible time for ground operations with DC power only…

5 minutes

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

2 minutes

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

2 minutes

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Max ITT for start

(200)
900

(700/900)
815

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Minimum oil pressure for takeoff

45 PSI

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Continuous ignition must be used during the following:

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

At initiation of thrust lever movement from SHUTOFF to IDLE...

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

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

75 knots 60 knots

Maximum slats and/or flaps extended altitude

15,000 ft

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

17 knots

Maximum fuel imbalance for takeoff:

(200) 800lbs (700/900) 300

Maximum fuel imbalance for all other phases of flight:

800 lbs

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

500 lbs 4400 lbs

Minimum fuel quantity per wing tank for a go-around

(200) 450 lbs (700/900) 600 lbs

Ground contamination definition

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

Visible moisture definition

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)

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

400 ft AGL 10 C Cowl anti-ice

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

400 ft AGL 5 C Cowl and Wing anti-ice

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.

ON 2 minutes 5 C

A tactile check is required when...

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

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

OFF 10 minutes

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

15 minutes not increasing

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

PROHIBITED Medium

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

Not permitted.

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

Not permitted

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 ____.

600 ft AGL 400 ft AGL 80 ft AGL 110 ft AGL

Maximum taxi and ramp weight (200)

53,250 lbs

Maximum takeoff weight (200)

53,000 lbs

Maximum landing weight (200)

47,000 lbs

Maximum zero fuel weight (200)

44,000 lbs

Maximum taxi and ramp weight (700)

75,250 lbs

Maximum takeoff weight (700)

75,000 lbs

Maximum landing weight (700)

67,000 lbs

Maximum zero fuel weight (700)

62,300 lbs

Maximum landing weight (900)

85,000 lbs

Maximum takeoff weight (900)

84,500 lbs

Maximum landing weight (900)

75,100 lbs

Maximum zero fuel weight (900)

70,750 lbs

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

Cowl

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

Cowl

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

Wing and cowl

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)

10 C TAT -39 C SAT 230 knots Cowl 230 knots Wing and cowl

____ 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

TOGA

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.

75% N1 TOGA

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

Idle/taxi TOGA

Starter cranking limits (200)

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

Starter cranking limits (700/900)

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

APU starter cranking limits (200)(on battery)

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

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

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