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Kalitta Air B777F > Limitations > Flashcards

Limitations Flashcards

1
Q

Runway Slope

A

+/- 2%

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2
Q

Maximum Takeoff and Landing Tailwind Component

A

Boeing - 15 kts
Kalitta - 10 kts

– The capability of the airplane has been satisfactorily demonstrated for takeoff and landings with tailwinds up to 15 knots. This does not constitute operational approval to conduct takeoffs and landings with tailwind components in excess of 10 knots.

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3
Q

Maximum Operating Altitude

A

43,100 feet pressure altitude

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4
Q

Maximum Takeoff and Landing Altitude

A

8,400 feet pressure altitude (Basic)
9,800 feet pressure altitude (Optional)

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5
Q

Door Mounted Power Assists and Escape Slides
Door Marked ARMED/DISARMED

A

Main door emergency power assist and evacuation slide systems must be armed with mode select handle in the ARMED position prior to taxi, takeoff and landing whenever passengers are carried.

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6
Q

Door Mounted Power Assists and Escape Slides
Door Marked AUTO/MANUAL

A

Main door emergency power assist and evacuation slide systems 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

Maximum demonstrated takeoff and landing crosswind

A

38 kts

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8
Q

Severe turbulent air penetration speed

A
  • 270 kts < 25,000 ft
  • 280 kts <> 0.82M =< 25,000 ft
  • if <0.82M, MMS+15kts
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9
Q

DO NOT operate HF radios…

A

during refueling operations

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10
Q

Do not operate the weather radar…

A
  • in a hangar
  • within 50ft of fueling operations or spills
  • when personnel are within the area normally enclosed by the aircraft nose radome
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11
Q

Max difference between CA or FO altitude display and field elevation

A

75 ft

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12
Q

Max Taxi Weight

A

768,000 lbs

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13
Q

Max Takeoff Weight

A

766,000 lbs

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14
Q

Max Landing Weight

A

575,000 lbs

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15
Q

Max Zero Fuel Weight

A

547,000 lbs

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16
Q

DO NOT use the autopilot below 100ft radio altitude at…

A

airport field elevations above 8,400ft

17
Q

After T/O, A/P must not be engaged…

A

Below 200 ft AGL

18
Q

Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged below…

A

200 ft AGL

19
Q

Max wind when ldg wx min are predicated on autoland

  • Headwind
  • Crosswind (Cat II/III and other)
  • Tailwind
A

25 kts - Headwind
10 kts/15 kts - Tailwind
25 kts - Other

20
Q

Max/Min glideslope when ldg wx min are predicated on autoland

A

Max - 3.25 deg
Min - 2.5 deg

21
Q

Do not use FLCH below…

A

1000 ft AFE

22
Q

Max fuel tank temp

A

49oC

23
Q

Reverse thrust prohibited (2)

A
  • Intentional in flight selection
  • Backing the airplane
24
Q

For ground operation (exclusive of takeoff) in tailwinds and crosswinds between 30 and 45 knots…

A

engine power should be limited to a maximum of 70% N1. Avoid thrust levels above that required for normal taxi operation in all tailwinds and crosswinds greater than 45 knots.

25
Q

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

A

3 starts attempts in a 60 minute period each

26
Q

Flight control rapid & large alternating control inputs…

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.

27
Q

Max flap extension altitude

A

20,000 ft

28
Q

The ground maneuver cameras should not be used during…

A

takeoff, approach, and landing.

29
Q

ADIRU alignment must not be attempted at latitudes greater than…

A

78 degrees, 14.75 minutes.

30
Q

Minimum Oxygen pressure CREW

A

1,100 psi for dispatch

  • 4 crew
  • 180 min diversion time
31
Q

Minimum Oxygen pressure SUPERNUMERARY

A

1,300 psi for dispatch

  • 5 supernumeraries
  • 180 min diversion time
32
Q

Minimum Oxygen pressure for Portable bottles

A

1,200 psi for dispatch

33
Q

Flap Limits

  • 1
  • 5
  • 15
  • 20
  • 25
  • 30
A 
Flaps:
265 - 1
245 - 5
230 - 15
225 - 20
200 - 25
180 - 30

Kalitta Air B777F (20 decks)

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