Chapter 9 Flashcards
EMER ENG SHUTDOWN
engine shutdown without delay
EPCLs - OFF.
ENG FUEL SYS selector(s) - OFF.
FUEL BOOST PUMP switches - OFF switch(es) - OFF.
If TGT is above 538°C after shutdown: 4. AIR SOURCE HEAT/START switch - As required. 5. ENGINE IGNITION switch - OFF. 6. Starter button - Press to motor engine for 30 seconds or until TGT TEMP decreases below 538°C.
LOCKOUT
manual control of engine RPM while bypassing DEC functions
EPCL - Pull down and advance full forward while maintaining downward pressure, then
adjust to set % RPM R as required
EMER APU START
FUEL PUMP switch - APU BOOST
APU CONTR switch - ON.
SINGLE-ENGINE FAILURE
Collective - Adjust to maintain % RPM R
External cargo/stores - Jettison (if required)
Establish single-engine airspeed
If continued flight is not possible:
LAND AS SOON AS POSSIBLE
If continued flight is possible
LAND AS SOON AS PRACTICABLE
DECREASING % RPM R
Collective - Adjust to control % RPM R.
Establish single-engine airspeed.
EPCL- (low % TRQ/TGT TEMP engine) - LOCKOUT. Maintain apx 10% TRQ below other engine
LAND AS SOON AS PRACTICABLE.
INCREASING % RPM R
ENG POWER CONT lever (high % TRQ/
TGT TEMP engine) - Retard.
LAND AS SOON AS PRACTICABLE
If EPCL doesnt change % RPMR Establish single engine airspeed. Perform EMER ENG SHUTDOWN (affected engine). Refer to single-engine failure emergency procedure.
% RPM INCREASING/DECREASING
OSCILLATION
Establish single engine airspeed
-nonunderlined steps-
ENGINE COMPRESSOR STALL
Collective - Reduce.
If condition persists:
ECPL (affected engine)- Retard (TGT TEMP decreases).
3. ECPL (affected engine) - FLY.
If stall condition recurs: Establish single engine airspeed. EMER ENG SHUTDOWN (affected engine). Refer to single-engine failure emergency procedure.
#1 OIL FLTR BYPASS OR #2 OIL FLTR BYPASS CAUTION APPEARS
Establish single engine airspeed.
EPCL - Retard.
LAND AS SOON AS PRACTICABLE
CHIP #1 ENGINE OR CHIP #2 ENGINE, #1
ENGINE OIL PRESS OR #2 ENGINE OIL PRESS, #1 ENGINE OIL TEMP OR #2 ENGINE OIL TEMP CAUTION APPEARS.
Establish single engine airspeed. EPCL (affected engine) - Retard (to reduce torque). EMER ENG SHUTDOWN (affected engine). Refer to single engine failure emergency procedure.
ENGINE HIGH-SPEED SHAFT FAILURE
Collective - Adjust. Establish single engine airspeed. EMER ENG SHUTDOWN (affected engine). Do not attempt to restart. Refer to single-engine failure emergency procedure.
LIGHTNING STRIKE
ENG POWER CONT levers - Adjust as
required to control % RPM.
LAND AS SOON AS POSSIBLE.
Tail Rotor EPs
.
Loss of Tail Rotor Thrust in Cruise Flight
Airspeed - Adjust to 80 KIAS or above.
AUTOROTATE - Maintain airspeed at or
above 80 KIAS.
EPCLs - OFF (during deceleration when intended point of landing is assured).
Loss of Tail Rotor Thrust or TAIL ROTOR
QUADRANT Caution Appears with Loss of Control at Low Airspeed/Hover (Right Rotation)
Collective - Reduce.
EPCLs - OFF (5 to 10 feet above touchdown).
TAIL ROTOR QUADRANT Caution Appears
in Cruise Flight
Collective - Adjust to determine controllability
(Fixed Right or Left).
LAND AS SOON AS PRACTICABLE
Loss of Control at Low Airspeed/Hover or
TAIL ROTOR QUADRANT Caution Appears (Left Rotation)
EPCLs - Retard to decrease %RPM R below 100% and begin a partial power descent. Collective - Adjust to preserve %RPM R. ENG POWER CONT levers - OFF (5 to 10 feet above touchdown). Collective - Adjust for landing
Pedal Bind/Restriction or Drive With No
Accompanying Caution
Apply pedal force to oppose the drive
+nonunderlined