1
Q
Maximum EGT during engine start (ground):
A
- (88): 500°C (momentary)
* (90): 635°C (momentary)
2
Q
Maximum takeoff and landing tailwind component:
A
10 kts, or as permitted by Delta 10-0 special pages.
3
Q
Max operating altitude:
A
Max operating altitude is 37,000ft.
4
Q
Max unrestricted rudder crosswind component:
A
30 knots
5
Q
Turbulent air penetration speed:
A
280 ± 5 KIAS / .77 ± .02M (whichever is lower).
6
Q
Maximum allowable wind speeds for autoland operations:
A
Headwind: 25 kts
Crosswind: 15 kts
Tailwind: 10 knots
7
Q
Autopilot altitude limit on takeoff:
A
500 ft AGL
Do not engage autopilot for takeoff below 500 ft AGL
8
Q
Maximum lateral fuel imbalance:
A
1500 lbs
• Main tanks must not differ by more than 1500 pounds.
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
