Limitations Flashcards
Min CHT before engine start if engine is cold
120°C
Min CHT before engine start if engine is warm
110°C
Min CHT before engine run-up starts
140°C
Min CHT before throttle is advanced to WOT
150°C
Air vehicle shall be launched within ______ of air vehicle engine start if the temperature of the launch area exceeds ______.
20 Min
38°C
Min CHT
120°C
Max CHT
210°C
Min RPM limiter setting
3000 RPM
Max RPM limiter setting
7200 RPM
RPM at min throttle on ground and in flight
2950 - 3550 RPM
RPM at max throttle in flight
5250 - 7250 RPM
MGTOW
135 LBS
Max fuel capacity
44.1 LBS
Launcher pneumatic pressure range
150 - 2200 PSI
Normal launch speed range
20.0 - 63.3 KTS
Launch speed that requires mission abort and recovery of air vehicle as soon as possible
≥ 69.9 KTS
(Chained launch) Launch speed that requires mission abort and recovery of air vehicle as soon as possible
≥ 6.6 KTS ABOVE TARGET LAUNCH SPEED
Max allowable difference between corrected barometric altitude and GPS altitude during launch and recovery
+ / - 33 FT
Min capture speed
38.9 KTS CLOSING
SPEED
Min planned fuel for recovery
2.2 LBS
Shore-based limit (degrees perpendicular to the
plane of the retriever)
+ / - 15°
Ship-based limit (degrees perpendicular to the plane of the retriever)
+ / - 2°
Min operating altitude
0 FT MSL
Max launch/recovery altitude at MGTOW
7500 FT DA
Max operating altitude
20,000 FT DA
Max airspeed (V ne)
110 KIAS
Min commanded airspeed
3 KTS ABOVE AUTOPILOT
MIN SPEED
Max gusts (Shore-based Launch)
5 KTS
Max gusts (Shore-based Recovery)
10 KTS
Max headwind, including gusts
(Shore-based Launch and Recovery).
25 KTS
Max crosswind, including gusts
(Shore-based Launch and Recovery)
10 KTS
Max tailwind, including gusts
(Shore-based Launch and Recovery)
5 KTS
Max tailwind at DA of 7500 ft or greater including gusts (Shore-based Launch and Recovery)
0 KTS
Max gusts in flight
10 KTS
In flight max total winds in any direction, including gusts (In Flight)
60 KTS
Min operating OAT (Not derived from OAT sensor while aircraft is on deck)
- 20°C
Max operating OAT (Not derived from OAT sensor while aircraft is on deck)
49°C