Engine Compartment Fire

(In Flight)

1. Attempt to confirm presence of fire (Alert Crew)

2. Single engine flight profile - Establish 

If fire confirmed:

3. FSC (affected engine)- Confirm; IDLE; Confirm; OFF

 4. EFSL - Confirm; OFF

5. Boost Pumps (affected engine) - OFF

6. PRI Fire Extinguisher Button (affected engine) - Confirm; Push

7. SEC Fire Extinguisher Button (affected engine) - PUSH

8. Landing/Hover Checklist - Complete

(200-foot checks at a minimum based on urgency)

If fire still persists:

9. Land/Ditch immediately

 If fire no longer evident:

 9. Land as soon as possible

Engine Compartment Fire

(On Deck)

1. Attempt to confirm presence of fire (alert crew) 

2. FSC Switches - Both OFF

3. EFSL - Both OFF

4. Boost pumps - All OFF

If fire confirmed:

 5. PRI Fire Extinguisher Button (affected engine) - Confirm; PUSH

 6. SEC Fire Extinguisher Button (affected engine) - PUSH

7. EEC - OFF

8. Rotor Brake - ON

9. Evacuate Aircraft

Engine Compartment Fire

(Post-Shutdown)

1. FCS Switch - Check OFF

2. Boost Pumps - Check OFF

3. EFSL - Shut OFF (Ensure 10 sec have elasped prior to shutoff)

4. Crank Button - Depress until TOT decreases

If TOT continues to rise or does not decrease:

EEC - OFF

 6. Rotor Brake - ON

7. Evacuate Aircraft

Main Gearbox Fire

1. ATTEMPT TO CONFIRM PRESENCE OF FIRE (alert crew)

2. LANDING/HOVER CHECKLIST − COMPLETE

(200−foot checks at a minimum based on urgency)

If fire confirmed:

 3. LAND/DITCH IMMEDIATELY

If fire  NOT confirmed:

 3. LAND AS SOON AS POSSIBLE

Internal Fire

(Cabin, Electrical, and/or Avionics)

1. DESIGNATE CREWMEMBER TO FIGHT FIRE

2. AFFECTED EQUIPMENT − OFF

3. HEAT/COOL SWITCHES − OFF

4. RAM AIR − CLOSED

5. CABIN SLIDING DOOR − CLOSED

6. PILOT WINDOWS − CLOSED

7. RACK BLOWER CIRCUIT BREAKER − PULL

(for avionics rack fire only − avionics rack panel R4

#4 in HH−65, R5 #4 in MH−65)

8. CIRCUIT BREAKERS − PULL (for affected circuits)

9. LANDING/HOVER CHECKLIST − COMPLETE

(200−foot checks at a minimum based on urgency

 If electrical or avionics fire persists:

10. EMERGENCY ELECTRICAL CUTOFF − OFF

 If electrical or avionics fire persists:

11. LAND/DITCH IMMEDIATELY

 If fire goes out:

11. LAND AS SOON AS POSSIBLE

Smoke & Fume Elimination

1. HEAT/COOL SWITCHES − OFF

2. RAM AIR − OPEN

3. CABIN SLIDING DOOR − OPEN

4. PILOT WINDOWS − OPEN

5. LAND AS SOON AS PRACTICABLE

Heater Overheat Light

 1. HEAT SWITCH − OFF

2. HEATER (LOWER) NOZZLES − ALL OPEN

3. ECS CIRCUIT BREAKER − RESET IF POPPED

(copilot forward panel, R2 #4)

If O/HEAT light remains illuminated:

4. LAND AS SOON AS PRACTICABLE

If O/HEAT light extinguishes:

4. CONTINUE FLIGHT AS APPROPRIATE

BATT TEMP Light

1. BATT RELAY SWITCHES − BOTH OF

(To prevent the battery from receiving further charge)

2. LAND AS SOON AS PRACTICABLE

Main Gearbox Overtemp/

OIL TEMP Light

1. CRUISE AIRSPEED − 120 KIAS MINIMUM

 2. LAND AS SOON AS PRACTICABLE

MGB Chip Light

1. MONITOR FOR SECONDARY INDICATIONS

2. FLY AT MINIMUM SAFE ALTITUDE

3. AVOID HIGH POWER MANEUVERS

4. LAND AS SOON AS PRACTICABLE

TGB CHIP Light

1. ESTABLISH SAFE ALTITUDE AND AIRSPEED FOR POSSIBLE LOSS OF TAIL ROTOR THRUST

2. LAND AS SOON AS POSSIBLE

MINOR FADEC/GOVERNOR FAILURE

1. COMPLETE THE "BIG 4"

2. ABORT MISSION. URGENT MISSION MAY BE

COMPLETED

MAJOR FADEC/GOVERNOR FAILURE

1. COMPLETE THE "BIG 4"

2. TRNG SWITCH − FLT

 3. FADEC BACKUP SWITCH (affected engine) − BACKUP

N1 DIVERGENCE/PARTIAL POWER LOSS

1. COMPLETE THE BIG 4"

NOSEWHEEL SHIMMY DAMPER FAILURE

1. LIFT AIRCRAFT OFF GROUND IMMEDIATELY

OR REDUCE TAXI SPEED

 2. PERFORM VERTICAL LANDINGS OR TAKEOFFS

3. CONTINUE FLIGHT AS APPROPRIATE

 AUDIO SYSTEM FAILURE

1. PILOT AND COPILOT AUDIO BYPASS SWITCHES − BYPASS

2. ICS CIRCUIT BREAKERS (2) − PULL, RESET

(cockpit avionics panel R1 #5 and R5 #5)

3. CONTINUE FLIGHT AS APPROPRIATE

Emergency Egress Procedures

1. WAIT FOR ALL VIOLENT MOTION TO STOP 

2. REFERENCE POINT − HOLD

3. EMERGENCY RELEASE HANDLE − JETTISON

4. CORDS − DISCONNECT

5. SEATBELT/HARNESS − RELEASE AND MAINTAIN

REFERENCE

6. EGRESS

7. VEST − INFLATE WHEN CLEAR OF AIRCRAFT

Emergency Entrance

1. Attempt to open any of the doors in the normal manner.

2. Use the emergency door release handles to jettison the pilot, copilot, and passenger doors.

3. Swimmer window located aft of the sliding door may be jettisoned by pulling outward onthe red tabbed lanyard and pushing inward on the window.

4. Access to the passenger compartment can also be accomplished through the baggage compartment door. 

Immediate Emergency Landing/Ditching

1. CREW AND PASSENGERS − ALERTED

2. WHEELS/FLOATS − AS REQUIRED

3. LAND/DITCH AIRCRAFT

4. EFSLS − BOTH OFF (after landing/water entry)

5. EMERGENCY ELECTRICAL CUTOFF − AS REQUIRED

6. ROTOR BRAKE (land only)

7. EMERGENCY EGRESS PROCEDURE − EXECUTE

Emergency Ditching/Landing Procedure

 1. CREW AND PASSENGERS − ALERTED

2. DISTRESS − TRANSMIT

3. PERSONAL EQUIPMENT − CHECKED

4. LANDING/HOVER CHECKLIST − COMPLETE

If DUAL ENGINE:

5. DOORS − JETTISON IN A HOVER

6. FLOATS − INFLATE IN A HOVER

If SINGLE ENGINE:

5. DOORS − JETTISON IN A CLIMB @ 70 KIAS IF

ABLE; OTHERWISE @ 200 FEET @ 70 KIAS,

STRAIGHT AND LEVEL

6. PRIOR TO WATER ENTRY − FLOATS INFLATE

7. ENTER WATER IN A LEVEL ATTITUDE

8. FADEC CONTROL SWITCHES − OFF

9. ROTOR − ALLOW TO COAST DOWN

10. EGRESS HELICOPTER WHEN ROTOR STOPS