Specifications/Limitations Flashcards

1
Q

Maximum Taxi Weight

A

174,700 Ibs

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2
Q

Maximum Takeoff Weight

A

174,200 Ibs

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3
Q

Maximum Landing Weight

A

146,300 Ibs

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4
Q

Maximum Zero Fuel Weight

A

138,300 Ibs

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5
Q

Maximum runway slope

A

+/- 2%

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6
Q

Max. operating pressure altitude

A

41,000 feet

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7
Q

Max. Takeoff and Landing pressure altitude

A

8,400 ft.

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8
Q

Maximum G load limits

A

Flaps up: +2.5 and -1.0

Flaps down: +2.0 and 0.0

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9
Q

Maximum Tailwind Component

A

10 knots

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10
Q

Flap settings used with Autoland

A

30 degrees and 40 degrees

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11
Q

Maximum altitude at which APU can be used as bleed AND electrical sources?

A

In flight: 10,000 ft.

Ground: 15,000 ft.

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12
Q

Maximum altitude APU can be used as a bleed source?

A

17,000 ft.

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13
Q

Maximum Usable Fuel tank quantities:

Tanks 1 and 2

A

9,144 Ibs. each

7.1 Ibs/gal.

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14
Q

Maximum Usable Fuel tank quantities:

Center Tank

A

30,522 Ibs.

7.1 Ibs/gal.

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15
Q

Total Usable Fuel

All tanks combined

A

48,810 Ibs.

7.1 Ibs/gal.

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16
Q

Maximum Crosswind Component

A

34 knots (with winglets)