Limitations Flashcards

1
Q

Runway Slope

A

+/- 2%

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2
Q

Maximum Takeoff and Landing Tailwind
Component

A

10 Knots (Basic)
15 Knots (Optional)

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3
Q

Maximum Operating Altitude

A

43,100ft Pressure Altitude

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4
Q

Maximum Takeoff and Landing Altitude

A

8,400ft Pressure Altitude (Basic)
9,800ft Pressure Altitude (Optional)

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5
Q

Door Marked ARMED/DISARMED

A

select handle in the ARMED position prior to taxi, takeoff and landing whenever
passengers are carried.

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6
Q

Door Marked AUTO/MANUAL

A

must be armed with
mode select handle in the AUTOMATIC position prior to taxi, takeoff and landing
whenever passengers are carried

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7
Q

Flight Deck Security Door

A

Verify that an operational check of the Flight Deck Access System has been
accomplished according to approved procedures once each flight day.

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8
Q

Lower Crew Rest Compartment

A

The lower crew rest compartment may not be occupied, and the main entry hatch must
be closed during taxi, takeoff and landing.

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9
Q

The Maximum demonstrated takeoff and landing crosswind

A

38kts

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10
Q

Severe Turbulent Air Penetration Speed

A

270 < 25,000
280/M.82 <25,000

Maintain a minimum speed of 15 knots above the minimum maneuvering speed at all
altitudes when airspeed is below 0.82 Mach.

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11
Q

HF radio limitation

A

DO NOT operate HF radios during refueling operations

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12
Q

wx radar operation limitations

A
  • Avoid weather radar operation in a hangar or within 50ft (15.25 m) of fueling operations
    or a fuel spill
  • Avoid weather radar operation when personnel are within the are normally enclosed by
    the aircraft nose radome
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13
Q

max allowable difference between capt or FO’s altimeters to field elevation

A

75’

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14
Q

777F weights

A
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15
Q

Maximum Zero Fuel Weight

A

547,000lbs

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16
Q

Maximum Taxi Weight

A

768,000lbs

17
Q

Maximum Takeoff Weight

A

766,000lbs

18
Q

Maximum Landing Weight

A

575,000lbs

19
Q

B777-300ER

A
20
Q

Maximum Zero Fuel Weight
-300

A

529,000lbs

21
Q

Maximum Taxi Weight
-300

A

777,000lbs

22
Q

Maximum Takeoff Weight
-300

A

775,000lb

23
Q

Maximum Landing Weight
-300

A

554,000lbs

24
Q

Autoflight Limitations

A
25
Q

AP limitation

A

DO NOT use the autopilot below 100ft radio altitude at airport field elevations above
8,400ft

26
Q

Min alt engagement for AP after takeoff?

A

200’ AGL

27
Q

Without LAND 2 or LAND 3 annunciated, AP limitation?

A

autopilot must be disengaged below 200
feet AGL.

28
Q

Autoland Wind Limits

A
29
Q

Headwind/Crosswind

A

25kts

30
Q

Tailwind

A

10kts (15kts optional)

31
Q

Max/Min glide slope angle

A

2.5-3.25

32
Q

FLCH limitation

A

DO NOT use FLCH on final approach below 1,000ft AFE.

33
Q

Reverse Thrust Limitation

A
  • Intentional selection of reverse thrust in flight is prohibited.
  • Backing the airplane with use of reverse thrust is prohibited.-
34
Q

taxi with tailwind limit

A

for crosswind and tailwinds 30-45 kits limit Engine thrust to 70% N1

35
Q

The APU’s starter motors duty cycle for the electric starter motor and air turbine starter

A

i3 starts attempts in a 60 minute period each.

36
Q

Maneuver limitation

A

Avoid rapid and large alternating control inputs, 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

37
Q

max altitude with flaps extended

A

FL200