Limitations Flashcards

1
Q

Maximum 90° Crosswind for takeoff and landing

A

27 knots

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2
Q

Maximum 90° crosswind for landing from a CATII approach

A

15 knots

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3
Q

Maximum headwind for landing from a Category II approach

A

17 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

A

36,000 feet

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6
Q

Maximum operating altitude

A

41,000 feet

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7
Q

Maximum altitude for single pack operation

A

25000 feet

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8
Q

Maximum altitude for single pack operation

A

31000 feet

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9
Q

Turbulence penetration speed

A

280 knots or .75m whichever is lower

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10
Q

Maximum gear extension speed

A

220 knots

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11
Q

Maximum gear extended speed

A

220 knots

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12
Q

Maximum gear retraction speed

A

200 knots

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13
Q

Maximum speed for windshield wiper operation

A

220 knots

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14
Q

Maximum speed flaps can be flown ( Vfe )

A

Flaps 8: 230 knots
Flaps 20: 220 knots
Flaps 30: 185 knots
Flaps 45: 170 knots

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15
Q

Maximum speed to extend the flaps ( Vfo )

A

Flaps 8: 200 knots
Flaps 20: 200 knots
Flaps 30: 185 knots
Flaps 45: 170 knots

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16
Q

APU start on battery

A

Start 1: 30 seconds ON, 2 minutes OFF
Start 2: 30 seconds ON, 20 minutes OFF
Start 3: 30 seconds ON, 2 minutes OFF
Start 4: 30 seconds ON, 40 minutes OFF

17
Q

APU start on D.C. Ground power

A

Start 1: 15 seconds ON, 2 minutes OFF
Start 2: 15 seconds ON, 20 minutes OFF
Start 3: 15 seconds ON, 2 minutes OFF
Start 4: 15 seconds ON, 40 minutes OFF

18
Q

Maximum APU starting altitude

A

30,000 feet

19
Q

Maximum APU starting altitude

A

37,000 feet

20
Q

Maximum APU operating altitude

A

36,000 feet

21
Q

Maximum APU operating altitude

A

41,000 feet

22
Q

Maximum altitude for APU bleed air extraction

A

15,000 feet

23
Q

Maximum altitude for bleed air extraction

A

25,000 feet

24
Q

Maximum permissible time with D.C. Ground power only

A

5 min

25
Q

During all starts, do not exceed ____ % N1 for ____ minutes after start, or until all operating indications are in the normal range which ever is ______

A

75% N1 for 2 minutes or when all operating indications are in the normal range whichever is longer

26
Q

Maximum ITT during engine start

A

900°C

27
Q

Maximum engine to engine N2 split at ground idle power should not be greater than ___% N2

A

2% N2

28
Q

If N2 is ___% or less with an OAT of -20°C or warmer, do not accelerate above ___

A

If N2 is 57% or less with an OAT OF -20°C or warmer, do not accelerate above idle

29
Q

Before the first flight of the day, when the airplane is cold-soaked at an ambient temperature of -30°C (-22°F) or below for more than 8 hours…

A

the engines must be motored for 60 seconds and fan rotation must be verified before an engine start is initiated.
-AND-
Thrust reversers must be actuated until the deploy and stow cycles as less than 5 seconds

thrust reversers must be actuated until the deploy and stow cycles are less than 2 seconds

30
Q

Continuous ignition must be used during the following:

A
  • Takeoff and landing on contaminated runways
  • Takeoff with high crosswind component (15 knots or greater)
  • Flight through moderate or heavier intensity rain
  • Flight through moderate of heavier intensity turbulence
  • Flight in the vicinity of thunderstorms
31
Q

Starter cranking limits

A

Start 1: 1 minute ON, 10 seconds OFF
Start 2: 1 minute ON, 10 seconds OFF
Start 3: 1 minute ON, 5 minutes OFF

32
Q

ITT must be no greater than ___ to bring thrust levers from SHUTOFF to IDLE for all ground starts

A

120°C

33
Q

During landing, maximum reverse thrust is prohibited below ___ knots, and reverse IDLE should be achieved by ___ knots

A

Start 1: 30 seconds ON, 2 minutes OFF
Start 2: 30 seconds ON, 20 minutes OFF
Start 3: 30 seconds ON, 2 minutes OFF
Start 4: 30 seconds ON, 40 minutes OFF