Limitations (Vol I) Flashcards

0
Q

Maximum takeoff and landing tailwind component

A

10 knots, or as permitted by Delta 10-0 special pages

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1
Q

Maximum EGT during engine start (ground)

A

(88) - 500°C

(90) - 635°C

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2
Q

Operating altitude

A

The max operating altitude is 37,000ft

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3
Q

Maximum unrestricted rudder crosswind component

A

30 knots

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4
Q

Turbulent air penetration speed

A

280 +/- 5 KIAS / .77 +/- .02M (whichever is lower)

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5
Q

Maximum allowable wind speeds for autoland operations

A

Headwind - 25 knots
Crosswind - 15 knots
Tailwind - 10 knots

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6
Q

Autopilot altitude limit on takeoff

A

Do not engage autopilot for takeoff below 500 feet AGL

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7
Q

Maximum lateral fuel imbalance

A

Main tanks must not differ by more than 1500 pounds

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8
Q

Flap/slat limit speeds: Slats

A

280 KIAS / .57 MACH

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9
Q

Flap/slat limit speeds: Flaps 11°

A

280 KIAS / .57 MACH

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10
Q

Flap/slat limit speeds: Flaps 15°

A

240 KIAS / .57 MACH

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11
Q

Flap/slat limit speeds: Flaps 23°

A

220 KIAS / .57 MACH

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12
Q

Flap/slat limit speeds: Flaps 28°/40°

A

200 KIAS / .57 MACH

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13
Q

Flap/slat limit speeds: (ALL)

A
Slats - 280 KIAS / .57 MACH
Flaps 11° - 280 KIAS / .57 MACH
Flaps 15° - 240 KIAS / .57 MACH
Flaps 23° - 220 KIAS / .57 MACH
Flaps 28°/40° - 200 KIAS / .57 MACH
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