B767-300 Limitations Flashcards

1
Q

Max certified altitude

A

43100’

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2
Q

Max Take off and Landing elevation

A

8400’

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3
Q

Rough air penetration speed

A

290 / M0.78

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4
Q

Max RWY slope

A

+/- 2%

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5
Q

Maximum tailwind component
(non autoland)

A

10 kts

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6
Q

Maximum cross wind
(non autoland)

A

Not defined

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7
Q

Maximum head wind component
(autoland)

A

25 kts

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8
Q

Maximum cross wind component
(autoland)

A

25 kts

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9
Q

Maximum tail wind component
(autoland)

A

10 kts

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10
Q

Minimum autopilot engagement height

A

200’ RA

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11
Q

Maximum flap extension altitude

A

20000’ MSL

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12
Q

Minimum speedbrake height

A

800’ AGL

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13
Q

Cargo door wind limitations

A

40 kts operations (60 kts open)

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14
Q

Max center tank capacity when fuel main tanks are NOT full

A

22050 lbs

(structual limitation)

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15
Q

B767 taxi fuel

A

600 lbs

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16
Q

B767 MTW (OY-SRU)

A

413,000 lbs

17
Q

B767 MTOW (OY-SYA)

A

412,000 lbs

18
Q

B767 MLW (OY-SYA)

A

326,000 lbs

19
Q

B767 MZFW (OY-SRU)

A

309,000 lbs