EIA B747-400 Limitations Flashcards

2
Q

Aircraft Length

A

232’

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3
Q

Aircraft Wingspan

A

213’

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4
Q

N492EV, N493EV, N779BA Maximum Zero Fuel Weight (MZFW)

A

610.0

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5
Q

Maximum Landing Weight

A

N491EV–666.0

N492EV, N493EV, N779BA–652.0

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6
Q

Maximum Demonstrated T/O & Landing X-Wind

A

30 Knots (not limiting)

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7
Q

Maximum Operating Altitude

A

45,100’ (PA)

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8
Q

Maximum T/O & Landing Altitude

A

9,500’ (PA)

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9
Q

Maximum Tailwind

A

10 Kts

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10
Q

Oxygen Pressures

A

Recommended-

  • Crew (over ocean) - 1500 psi
  • Crew (over land) - 950 psi
  • Supernumerary - 1200 psi
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11
Q

Mmo

A

.92

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12
Q

Mmo RVSM

A

.90

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13
Q

Turbulence Penetration Speed

A

290 to 310 Knots / .82 to .85 which ever is lower

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14
Q

Minimum A/P Engagement Takeoff Altitude

A

250’ AGL

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15
Q

Single Channel ILS A/P Disengagement Altitude

A

Must be disengaged before the airplane descends below 100’ AGL

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16
Q

MDA A/P Disengagement Altitude

A

Must be disengaged before the airplane descends more than 50’ below the MDA, unless it is coupled to an ILS G/S & LOC, or in the GA Mode

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17
Q

Aileron Trim Use with A/P

A

Prohibited

18
Q

Icing Conditions on the Ground and for T/O (Limitations Chapter)

A

OAT 10° C. or below and visible moisture w/ visibility of 1 mile (1600 mtrs) or less or chance of ingestion by engines or freezing on the engines, nacelles or engine sensor probes

19
Q

Icing Conditions in Flight

A

TAT 10° C. or below and visible moisture

20
Q

Maximum Flap Operating Altitude

A

20,000’

21
Q

N491EV Maximum Zero Fuel Weight (MZFW)

A
  • 635.0 - for T/O weights of 811.0 or less.

- for T/O weights above 811.0 and up to 875.0, reduce MZFW linearly to 610.0

22
Q

Brake Accumulator Precharge Pressure

A

750 psi