Phase Ones Flashcards

1
Q

Normal Taxi Speed Limit

A

20 knots

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2
Q

Maximum dry surface taxi speed for turn angles greater than a high speed turnoff

A

Approximately 10 knots

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3
Q

Maximum taxi speed on a long straight taxi route

A

Up to 30 knots

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4
Q

Reverse thrust backing up

A

Is not authorized

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5
Q

Maximum takeoff and landing crosswind

A

38 knots

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6
Q

Maximum crosswind for side slip only (zero crab) landings

A

Crosswind component over 31 knots

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7
Q

Cat II and III approaches do not allow

A

Flaps 25 for landing

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8
Q

Maximum allowable headwind for autoland

A

25 knots

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9
Q

Maximum allowable tailwind for autoland

A

10 knots

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10
Q

Maximum allowable crosswind for autoland

A

25 knots

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11
Q

Maximum allowable tailwind component for takeoff and landing

A

10 knots

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12
Q

Maximum operating altitude

A

43,100 feet pressure altitude

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13
Q

Maximum ramp/taxi weight

A

768,000 pounds

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14
Q

Maximum landing weight

A

575,000 pounds

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15
Q

Minimum fuel tank temperature prior to takeoff

A

-40 degrees C or 3 degrees C above the fuel freezing point, whichever is higher

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16
Q

The inflight tanke fuell temperature should be

A

Maintained at least 3 degrees C above the freezing point of the fuel being used

17
Q

Usable fuel quantity of left or right main tank

A

73,130 lbs.

18
Q

Usable fuel quantity of the center tank

A

193,759 lbs.

19
Q

Minimum pave width to make a 180 degree turn

A

155.8 feet

20
Q

If in cruise flight and FUEL IN CENTER EICAS advisory displayed

A

Use center tank fuel feed

21
Q

Maximum allowable crosswind for Autoland

A

15 knots

22
Q

Maximum crosswind limit for landing with good to medium braking action

A

35 knots

23
Q

Maximum crosswind limit for landing with medium to poor braking action

A

20 knots

24
Q

Maximum crosswind limit for landing with poor braking action

A

17 knots

25
Q

Maximum runway altitude limit for takeoff and landing

A

9,800 feet

26
Q

Icing conditions exist when

A

OAT on the ground and for takeoff or TAT in-flight is 10 degrees Celsius or below and visible moisture in any form is present

27
Q

When total main tank fuel is greater than 123,000 lbs., the maximum fuel imbalance between main tanks for taxi, takeoff and landing must not exceed

A

3,000 pounds or 4,500 if less than 90,000 lbs.