EP Quiz

Emergency Procedure Quiz Hot Start/Engine Residual Fire on Ground 1. If a residual fire persists on shutdown 1. 2. 3. N: Engine Compartment Fire 1. 2. 3. 4. W: N: ECA Malfunction with the Rotor Brake On N: 1. 2. 3. 4. C: ECA Failure Upon Rotor Shutdown C: 1. 2. If the affected engine’s MNL TRIM caution light is illuminated 3. If engine still continues to run for more than 30 seconds: 4. 5. 6. 7. C: Rotor Brake Failure on Rotor Engagement Indications: rotor brake fails to come off or light stays on for more than 5 seconds 1. 2. C: 3. Ground Resonance: W: APU Compartment Fire 1. 2. 3. Failure of One Engine During Takeoff 1. 2. 3. Failure of One Engine While Hovering In Ground Effect 1. 2. Failure of One Engine While Hovering Out of Ground Effect 1. 2. 3. 4. 5. Failure of One Engine In Flight 1. 2. 3. 4. 5. 6. C: 7. W: 8. 9. 10. 11. W: W: N: N: Fuel Control Pressure Regulating Valve (PRV) Diaphragm Failure Indications: 1. C: 2. 3. 4. 5. 6. Engine Restart In Flight 1. 2. 3. 4. 5. W: Compressor Stall Indications: 1. 2. W: ECCS Failure In Flight N: W: If a MNL TRIM light illuminates: 1. If MNL TRIM resets: 2. If Manual Mode does not reset: 3. 4. N: 5. C: 6. 7. If a MNL TRIM light does not illuminate: 1. 2. 3. 4. N: Engine Shutdown While In Manual Mode: 1. 2. 3. If affected engine does not shutdown 4. 5. If affected engine does not shutdown refer to ECA failure on rotor shutdown procedures 6. Engine Compartment Fire In Flight N: 1. 2. C: 3. 4. 5. 6. 7. Electrical Fire 1. 2. If fire persists: 3. 4. Fuselage Fire 1. 2. 3. 4. 5. 6. Smoke and Fume Elimination 1. 2. 3. 4. W: Imminent Transmission Failure W: W: W: Transmission Failure 1. W: 2. 3. 4. 5. Tripped Chip Detector Flag C: 1. 2. 3. Tripped Debris Screen N: 1. 2. Dual and Single Engine Overtorque W: Engine Accessory Gear Box Chip Detector and Lube Pump Drive Shaft Failure Indications: 1. If single engine capability exists: 2. If required for landing, the engine may be restarted W: N: Power turbine Speed Shaft Signal Interruption (Flex Shaft Failure) In Flight Indications: W: C: 1. 2. N: Monitor performance instruments to determine single-engine capabilities Perform failure of one engine in flight procedures as applicable 3. 4. 5. C: 6. N: 7. W: W: 8. 9. 10. Power Turbine Speed Signal Interruption (Flex Shaft Failure) Ground W: N: 1. N: 2. 3. Lag Damper Attachment or Horizontal Hinge Pin Failure If a gradual increase in one-per-rev vibration is detected 1. If the onset of one-per-rev vibrations is sudden: 2. 3. Fuel Boost Pump Failure C: 1. C: Four Way Fuel Valve Failure 1. 2. 3. 4. Generator Failure N: 1. 2. 3. C: AC Essential Bus Failure 1. 2. 3. 4. W: W: C: DC Bus Failure 1. 2. If power is restored 3. If power is not restored 4. 5. If a generator light illuminates, follow the generator failure procedures before executing the above procedures. If a DC light illuminates by itself and no other loss of electrical power, the pilot should suspect a faulty DC bus failure relay: no corrective action is required. 1. N: Hydraulic Flight Control System Failure 1. If No. 2 system has failed and fluid loss is not evident: 2. 3. 4. W: N: Utility Hydraulic System (or subsystem) Failure 1. 2. 3. W: Utility Hydraulic System Overheating 1. 2. 3. 4. 5. Rotor Brake Failure in Flight 1. 2. W: W: 3. Uncommanded Control Inputs 1. 2. 3. N: 4. 5. 6. 7. 8. Single AFCS Failure 1. 2. 3. 4. 5. N: Dual AFCS Failure 1. 2. 3. N: LCTA Failure (Airspeed Limits) DASH Actuator Failure

Pitch Oscillation 1. If oscillations do not subside: 2. If pitch stability is regained: 3. C: Uncommanded Altitude Hold Engagement 1. 2. If uncommanded collective movement continues 3. N: N: N: If engagement is experienced in flight 4. 5. Aft Rotor Stall 1. 2. 3. To prevent susceptibility for stall reoccurrence: 4. 5. W: W: N: Autorotative Landing 1. 2. 3. W: 4. 5. 6. 7. 8. 9. 10. 11. 12. 13. C: Sprag Clutch Seizure: 1. C: 2. Sprag Clutch Slippage 1. 2. 3. Attempt to reengage sprag clutch: 4. 5. 6. 7. W: N: 8. After landing 9. C: N: N: 10. Single Engine Takeoff 1. 2. C: 3. 4. 5. 6.