Limitations Flashcards

1
Q

A B737 has how many main propulsion engines?

A

Two

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2
Q

The CFM 56-26B engine develops how many pounds of thrust?

A

26000

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3
Q

Maximum gross takeoff weight for B737-700 is

A

153000

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4
Q

without the optional high elevaiton kit from Boeing, the maximum takeoff and landing field elevation is

A

8400

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5
Q

How many fuel tanks are there on a b737-700

A

three

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6
Q

what is the maximum imbalance between the left and right wing tanks on a b737-700?

A

1000 lbs

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7
Q

what is the standard passenger seating available on the B737-700

A

149

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8
Q

What is the maximum altitude that the APU can be used in flight

A

41000

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9
Q

Under 14 CFR 121, how many flight attendants are required on a B737-700?

A

3

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10
Q

If the APU is providing both electrical and Pneumatic service inflight, what is the aircraft’s maximum operating altitude?

A

10,000

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11
Q

Transport category aircraft performance calculations all begin by determining

A

Density Altitude

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12
Q

Transport category aircraft takeoff and landing performance calculations all RESULT in

A

An allowable weight.

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13
Q

which of the weights listed below is not an aircraft structural weight limitation?

A

DOW

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