Propulsion System Failure
Autopilot Failure
Engine Failure Above 2,000 FT AGL
AV Fire on Launcher
Oil Starvation (HUMS Caution & Alert)
TALS Abort Below Decision Point
Low Oil Pressure
Fuel System Failure (Fule Flow Alert (HUMS Alert)
Magnetometer Failure
Engine Failure Below 2,000 FT AGL
In-Flight Servo Failure
Uncontrolled Flight
Stuck throttle (Low RPM)
Auto launch Abort
GCS Electrical Power Failure
AV Fire On Ground
High Engine Temperature
No Oil Pressure
Uncommanded Firing of LDRF/LP (Physical)
Max Operational RPM
8000 RPM for 2 min
Max Continuous Climb RPM
7800 RPM
Max Continuous Cruise RPM
7500 RPM
Min Inflight RPM
3800 RPM
Max Static Full Throttle RPM
7200 RPM