Emergency Engine Shutdown on the Ground
Abort Start Procedure
EMERGENCY GROUND EGRESS
IF CANOPY CANNOT BE OPENED OR SITUATION REQUIRES RIGHT SIDE EGRESS
Abort
2. BRAKES-AS REQUIRED
Engine Failure Immediately After Takeoff
Sufficient Runway Remaining Straight Ahead
Engine Failure During Flight
IF CONDITIONS DO NOT WARRENT AN AIRSTART
Immediate Airstart (PMU NORM)
IF AIRSTART IS UNSUCCESSFUL
IF AIR START IS SUCCESSFUL
Uncommanded Power Changes/
Loss of Power/
Uncommanded Propeller Feather
IF POWER IS SUFFICIENT FOR CONTINUED FLIGHT:
IF POWER IS INSUFFICIENT TO COMPLETE PEL
Compressor Stalls
IF POWER IS SUFFICIENT FOR CONTINUED FLIGHT
IF POWER IS INSUFFICIENT TO COMPLETE PEL
Inadvertent Departure from Controlled Flight
Fire in Flight
IF FIRE IS CONFIRMED
IF FIRE IS EXTINGUISHED
IF FIRE IS NOT EXTINGUISHED
IF FIRE IS NOT CONFIRMED
Chip Detector Warning
Oil System Malfunction or Low Oil Pressure
IF ONLY AMBER OIL PX CAUTION ILLUMINATES
IF RED OIL PX ILLUMINATES AND/OR AMBER OIL PX CAUTION REMAINS ILLUMINATED FOR 5 SECONDS:
Low Fuel Pressure
OBOGS System Malfunction
OBOGS INOPERATIVE
EJECT
Forced Landing
Precautionary Emergency Landing
Takeoff/Max
Torque 100% ITT Max 820 N1 104% NP (2) 100% Oil Pressure (6) 90 to 120psi Oil Temp 10 to 105
Idle
Torque (9) 3-8%
ITT Max 750
N1 60-61% Ground
67% Flight
NP 46-50% Ground
Oil Pressure 90 psi min
Oil Temp -40-105 Ground
10-105 Flight
106-110 (7)Start
ITT Max 1000 for 5 sec
Oil PX. 200 psi max
Oil Temp -40 min
Transient
Torque (8) 131%for 20 sec
ITT Max 870 for 20 sec
N1 104%
NP 102% for 20 sec
110% (3)
Oil Pressure (5) 40-130psi
Oil Temp 106-110 for 10 minutes(1)
N1 values presented for PMU ON. With PMU OFF, N1 may vary from these values