Limitations Flashcards

1
Q

Maximum EGT during engine start (ground):

A
  • (88): 500°C (momentary)

* (90): 635°C (momentary)

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2
Q

Maximum takeoff and landing tailwind component:

A

10 kts, or as permitted by Delta 10-0 special pages.

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3
Q

Max operating altitude:

A

Max operating altitude is 37,000ft.

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4
Q

Max unrestricted rudder crosswind component:

A

30 knots

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5
Q

Turbulent air penetration speed:

A

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

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6
Q

Maximum allowable wind speeds for autoland operations:

A

Headwind: 25 kts
Crosswind: 15 kts
Tailwind: 10 knots

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7
Q

Autopilot altitude limit on takeoff:

A

500 ft AGL

Do not engage autopilot for takeoff below 500 ft AGL

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8
Q

Maximum lateral fuel imbalance:

A

1500 lbs

• Main tanks must not differ by more than 1500 pounds.

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9
Q

Flap/slat limit speeds:

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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