Limitations Flashcards

1
Q
  • What is the Maximum Operating Pressure Altitude?
A

41,000 Feet

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2
Q
  • What is the maximum takeoff/landing tailwind component?
A

15 Knots

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3
Q
  • What is the recommended severe turbulence penetration speed at Cruise?
A

TURB N1 setting from cruise page.

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4
Q
  • What is the recommended severe turbulence penetration speed during climb/descent?
A

280 Knots / .76 Mach.

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5
Q

If severe turbulence is encountered at below 15,000’ and the airplanes gross weight is < max landing, what turbulent penetration speed can the aircraft be slowed to?

A

250 Knots in a clean configuration.

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6
Q
  • Recommended crosswind component:
    Takeoff - RCC 6?
A

33 Knots.

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7
Q
  • Recommended crosswind component:
    Takeoff - RCC 5?
A

25 Knots.

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8
Q
  • Recommended crosswind component:
    Landing - RCC 6?
A

37 Knots

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9
Q
  • Recommended crosswind component:
    Landing - RCC 5?
A

37 Knots.

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10
Q
  • When do icing conditions exist on the ground and for takeoff?
A

When OAT (outside our temp) is 10 degrees or below.

+ visible moisture - or -
+while operating on ramps, taxiways, or runways where snow, standing water, or slush may cause moisture on aircraft. *1 mile or less visibility

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11
Q
  • When do icing conditions exist in flight?
A

When TAT (total air temp) <10 degrees C

+ visible moisture (1 mile or less vis)

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12
Q
  • What is the minimum autopilot engagement height?
A

400 feet AGL

(Per OpSpec C071)

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13
Q
  • What is the minimum altitude for use of autopilot on: an ILS/GLS coupled approach (no auto land)?
A

50 feet AGL

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14
Q
  • What is the minimum altitude for use of autopilot on: Non-precision approaches?
A

50 feet below MDA/DA.

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15
Q

What is the minimum altitude for use of autopilot on: Autoland

A

Touchdown.

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16
Q
  • When is LVL CHG not* authorized?
A

*Do not use LVL CHG on final below 1000’ AFE (above field elevation).

17
Q
  • What is the maximum Flap Extension Altitude?
A

20,000 Feet.

18
Q

Max allowable EGT for engine start? (NG/Max)

A

725 degrees C / 753 degrees C

19
Q

Max altitude the APU can supply electrical and bleed air?

A

10,000 feet

20
Q

Max altitude the APU can supply only electrical power?

A

41,000 feet

21
Q

Max altitude the APU can supply only bleed air?

A

17,000 feet

22
Q

Maximum runway slope?

A

+/- 2 degrees

23
Q

Minimum runway width?

A

100 feet

24
Q

Window heat must be on __ minutes before takeoff?

A

10 minutes.

25
Q

Probe heat must be on _______ to takeoff.

A

Prior

26
Q

Autoland maximum winds?
(Headwind, Crosswind, Tailwind)

A

Headwind = 25 knots
Crosswind = 15 knots
Tailwind = 10 knots