Term
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Definition
CORRECTIVE ACTION: 1. ATTEMPT TO CONFIRM PRESENCE OF FIRE (alert crew) 2. LANDING/HOVER CHECKLIST − COMPLETE (200−ft checks at a minimum based on urgency) If fire confirmed: 3. LAND/DITCH IMMEDIATELY If fire NOT confirmed: 3. LAND AS SOON AS POSSIBLE |
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Term
Engine Compartment Fire In-Flight |
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Definition
CORRECTIVE ACTION: 1. ATTEMPT TO CONFIRM PRESENCE OF FIRE (alert crew) 2. SINGLE ENGINE FLIGHT PROFILE − ESTABLISH If fire confirmed: 3. FADEC CONTROL SWITCH (affected engine) − CONFIRM; IDLE; CONFIRM; OFF 4. EMERGENCY FUEL SHUTOFF LEVER − 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−ft 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 If fire NOT confirmed: 3. LAND AS SOON AS PRACTICABLE |
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Term
ENGINE COMPARTMENT FIRE ON DECK |
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Definition
CORRECTIVE ACTION: 1. ATTEMPT TO CONFIRM PRESENCE OF FIRE (alert crew) 2. FADEC CONTROL SWITCHES − BOTH OFF 3. EMERGENCY FUEL SHUTOFF LEVERS − 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. EMERGENCY ELECTRICAL CUTOFF − OFF 8. ROTOR BRAKE − ON 9. EVACUATE AIRCRAFT |
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Term
INTERNAL FIRE
(CABIN, ELECTRICAL, AND/OR AVIONICS) |
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Definition
CORRECTIVE ACTION: 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, 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−ft 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 AND FUME ELIMINATION |
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Term
SMOKE AND FUME ELIMINATION |
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Definition
CORRECTIVE ACTION: 1. HEAT/COOL SWITCHES − OFF 2. RAM AIR − OPEN 3. CABIN SLIDING DOOR − OPEN 4. PILOT WINDOWS − OPEN 5. LAND AS SOON AS PRACTICABLE |
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Term
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Definition
CORRECTIVE ACTION: 1. ESTABLISH SAFE ALTITUDE AND AIRSPEED FOR POSSIBLE LOSS OF TAIL ROTOR THRUST 2. LAND AS SOON AS POSSIBLE |
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Term
ENGINE EMERGENCIES IN−FLIGHT
GENERAL |
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Definition
BIG 4: 1. Nr − MAINTAIN 2. AIRSPEED/ALTITUDE − CONTROL AND SET LIMITS 3. WHEELS/FLOATS − AS REQUIRED 4. ANALYZE |
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Term
N1 DIVERGENCE/PARTIAL POWER LOSS |
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Definition
CORRECTIVE ACTION: 1. COMPLETE THE BIG 4" |
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Term
MAJOR FADEC/GOVERNOR FAILURE |
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Definition
CORRECTIVE ACTION: 1. COMPLETE THE BIG 4" 2. TRNG SWITCH − FLT
3. FADEC BACKUP SWITCH (affected engine) − BACKUP |
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Term
MINOR FADEC/GOVERNOR FAILURE |
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Definition
CORRECTIVE ACTION: 1. COMPLETE THE BIG 4" |
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Term
PRIMARY HYDRAULIC SYSTEM FAILURE
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Definition
CORRECTIVE ACTION: 1. CRUISE AIRSPEED − 75 TO 100 KIAS 2. AVOID ABRUPT MANEUVERS |
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Term
LANDING GEAR MALFUNCTIONS
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Definition
If wheels fail to extend: 8. CONSIDER EXTERNAL ACTIVATION OF LANDING GEAR BLOWDOWN BOTTLE TO EXTEND LANDING GEAR − ACTIVATE FROM THE GROUND BY REMOVING FLAGGED SAFETY PIN AND ACTUATOR PIN (located in chine panel forward of the left main mount) If wheels still fail to extend: 9. CONSIDER USE OF EXTERNAL NITROGEN CANISTER VIA THE LANDING GEAR NITROGEN LINE T−FITTING TO EXTEND LANDING GEAR (located in chine panel forward of the left main mount) |
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Term
BATTERY OVER TEMPERATURE/ THERMAL RUNAWAY |
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Definition
CORRECTIVE ACTION: 1. BATT RELAY SWITCHES − BOTH OFF (to prevent the battery from receiving further charge) |
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Term
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Definition
CORRECTIVE ACTION: 1. PILOT AND COPILOT AUDIO BYPASS SWITCHES − BYPASS |
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Term
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Definition
CORRECTIVE ACTION: 1. HEAT SWITCH − OFF |
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Term
EMERGENCY EGRESS PROCEDURES |
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Definition
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 |
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Term
MALFUNCTIONING CABIN SLIDING DOOR |
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Definition
CORRECTIVE ACTION: 1. FLIGHT MECHANIC − REMAIN SECURED TO AIRCRAFT |
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Term
MAIN GEARBOX FAILURE IMMINENT
(MGB CHIP LIGHT) |
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Definition
CORRECTIVE ACTION: 1. LANDING/HOVER CHECKLIST − COMPLETE (200−foot checks at a minimum based on urgency) 2. LAND/DITCH IMMEDIATELY (POWER ON) |
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Term
ENGINE POST−SHUTDOWN FIRE
(Engine compartment fire)
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Definition
1. FADEC CONTROL SWITCH − CHECK OFF
2. BOOST PUMPS − CHECK OFF
3. EMERGENCY FUEL SHUTOFF LEVER − SHUT
OFF (ENSURE 10 SECONDS HAVE ELAPSED
PRIOR TO SHUTOFF)
4. CRANK BUTTON− DEPRESS UNTIL TOT DECREASES
If TOT continues to rise or does not decrease:
5. EMERGENCY ELECTRICAL CUTOFF − OFF
6. ROTOR BRAKE − ON
7. EVACUATE AIRCRAFT
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Term
ENGINE OIL COOLER FAN FAILURE
(OIL TEMP LIGHT)
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Definition
IF BOTH ENGINES ARE OVERHEATED:
1. CRUISE AIRSPEED - 120 KIAS MIN
2. LAND AS SOON AS PRACTICABLE
3. SHUT DOWN ENGINES AS SOON AS POSSIBLE
IF ONE ENGINE IS OVERHEATED:
1. CRUISE AIRSPEED − 75 KIAS MIN
2. FADEC CONTROL SWITCH (affected engine) −
CONFIRM; IDLE
3. ENGINE OIL TEMPERATURE − MONITOR
4. LAND AS SOON AS PRACTICABLE (If additional
power is required for landing, affected FCS may be
switched to flight position)
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Term
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Definition
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
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