Limitations Flashcards

1
Q

Runway slope

A

± 2%

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2
Q

Maximum Operating Altitude

A

43,100

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3
Q

Maximum Takeoff and Landing Altitude

A

8,400

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4
Q
# Maximum Takeoff and Landing Tailwind 
Component
A

10 knots

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5
Q

Flight Deck Security Door - operational check

A

once each flight day

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6
Q

Entry door evacuation slide systems must be armed and engaged

A

prior to taxi, takeoff, or landing

whenever passengers are carried

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7
Q

Severe turbulent air penetration speed

A

290 KIAS/.78 Mach (whichever is lower)

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8
Q

Do not operate HF radios

A

during refueling operations

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9
Q

APU starter duty cycle -

A

maximum of three consecutive starts or attempts within a sixty minute period

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10
Q

Do not use FLCH -

A

on final approach below 1000 feet AFE

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11
Q

Standby altimeters __do/do not__ meet altimeter accuracy requirements of RVSM

A

do not

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12
Q

Maximum allowable in-flight difference between Captain and First Officer altitude displays for RVSM operation -

A

200 feet

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13
Q

The maximum allowable on-the-ground differences between Captain and First Officer altitude displays for RVSM operation are:
(Between CA and FO)

A

SEA LEVEL - 40 feet
5,000 feet - 45 feet
10,000 feet - 50 feet

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14
Q

The maximum allowable on-the-ground differences between Captain or First Officer altitude displays and Field Elevation for RVSM operation is:

A

75 feet

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15
Q

Avoid weather radar operation -

A

in a hangar, or within 50 feet (15.25 meters) of fueling operations or a fuel spill

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16
Q

Maximum Taxi Weight

A

413,000 lbs

17
Q

Maximum Takeoff Weight

A

412,000 lbs

18
Q

Maximum Landing Weight

A

320,000 lbs

19
Q

Maximum Zero Fuel Weight

A

295,000 lbs

20
Q

After takeoff, the autopilot must not be engaged below

A

200 feet AGL

21
Q

Use of aileron trim with the autopilot engaged -

A

prohibited

22
Q

Autoland wind limitations -

A
# Headwind 25 kts
# Crosswind 25 kts
# Tailwind 10 kts
23
Q

Flight crew shall not blank _____ during takeoff

A

engine vibration

24
Q

The minimum inflight fuel tank temperature is ____ above the freeze point of the fuel being used

A

3°C

25
Q

The maximum fuel temperature is ___

A

49°C

26
Q

Reverse Thrust AFM Limitations (2)

A

ground use only

backing the airplane with use of reverse thrust is prohibited

27
Q

The maximum altitude with flaps extended

A

20,000 ft.

28
Q

Avoid ________, especially in combination with large changes in pitch, roll, or yaw (e.g. large side slip angles) as they may result in structural failure at any speed, including below VA

A

rapid and large alternating control inputs