Limits Flashcards
- Max aircraft mass for normal landing, and max RoD.
- C/Line, 2 crew, at what fuel is this mass achieved
- 5900 kg, 780 ft/min
- 1,050kg
What is the maximum take-off mass for the Hawk T-165 (at sea level)?
8561 kg
Max heavyweight landing mass and RoD
8561 kg
625 ft/min
Max cleared altitude
48,000’
Aircaft OAT operating limit
-26 to 50C
At ground level
Aircraft configuration restriction in visible icing
Full flap prohibited
Must land with half flap
Aircraft airspeed limits
- 575KCAS up to 0.9M
- 0.9M up to 500KCAS
- 500KCAS up to 1.2M
- 1.2M up to 48,000’
Basic aircraft
Gear Overspeed limits
- 200-210 KCAS: continue sortie
- > 210KCAS: abort sortie
Combat Flap speed limit
350KCAS/0.8M
Flaps G limits
Combat flap: -2 to +8G
1/2, 3/4, or full flap: 0 to +2.5G
Zero/negative G time limit
30sec
Must be followed by an eqaul or greater time of +ve G
Prohibited Manouvres
- Flick/snap manouvres
- Inverted spins
- Stall turns
- Tail slides
- Autopilot with O/B stores and only wingtip fairings/clean wingtips
Max speed for rudder use to enhance manouvres
200 KCAS
Single aircraft crosswind limit
30kts for takeoff or landing (wet or dry)
If >25kts, brakechute must not be streamed, except for emergency on T/O
Formation crosswind limit
15kts
Takeoff or landing
EEC controlled RPM/T6 limit
- 104% NH
- 880 degC
108% NL
Ground start T6 limit
637 degC