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Emergency Procedures > Emergency Procedures > Flashcards

Emergency Procedures Flashcards

1
Q

MAIN GEARBOX FAILURE IMMINENT

A

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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2
Q

MAIN GEARBOX FAILURE IMMINENT (Symptoms)

A

Symptoms:
1. Loss of XMSN lubrication OR illumination of a GB
CHIP warning light with an MGB CHIP annunciation
on the VEMD CAUTION/FUEL page in conjunction
with any one of the following:
Yaw kicks
Abnormal transmission noises
Unusually high power requirements
2. LOSS of XMSN lubrication AND illumination of a
GB CHIP warning light with an MGB CHIP annunciation
on the VEMD CAUTION/FUEL page.

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3
Q

MAIN GEARBOX MALFUNCTION

A

Corrective Action:

  1. MONITOR FOR SECONDARY INDICATIONS
  2. FLY AT MINIMUM SAFE ALTITUDE
  3. AVOID HIGH POWER MANEUVERS
  4. LAND AS SOON AS PRACTICABLE
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4
Q

MAIN GEARBOX FIRE

A 
Corrective Action:
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
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5
Q

ENGINE COMPARTMENT FIRE IN−FLIGHT

A

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−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
If fire NOT confirmed:
3. LAND AS SOON AS PRACTICABLE

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6
Q

ENGINE COMPARTMENT FIRE ON DECK

A 
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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7
Q 
INTERNAL FIRE (CABIN, ELECTRICAL, AND/OR
AVIONICS)
A 
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 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
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8
Q

SMOKE AND FUME ELIMINATION

A

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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9
Q

TGB CHIP DETECTED

A 
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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10
Q

ENGINE EMERGENCIES IN−FLIGHT − GENERAL

A 
FOR ANY SUSPECTED ENGINE MALFUNCTION,
THE FOLLOWING BASIC PROCEDURES APPLY
AND WILL BE REFERRED TO AS THE BIG 4:"
1. Nr − MAINTAIN
2. AIRSPEED/ALTITUDE − CONTROL AND SET
LIMITS
3. WHEELS/FLOATS − AS REQUIRED
4. ANALYZE
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11
Q

N1 DIVERGENCE/PARTIAL POWER LOSS

A

Corrective Action:

  1. COMPLETE THE BIG 4”
  2. ENGINE PARAMETERS − MONITOR
  3. LAND AS SOON AS PRACTICABLE
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12
Q

N1 DIVERGENCE/PARTIAL POWER LOSS (Symptoms)

A

NOTE
If the N1 is greater than 40%, the OEI GOV
mode page will be displayed on the VEMD. If
the N1 is less than 40%, the OEI mode page will
be displayed.
Symptoms:
1. DIF N1 Warning Light illuminated
2. OEI GOV mode page
3. N1 difference between both engines is greater than
6%

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13
Q

MAJOR FADEC/GOVERNOR FAILURE

A 
Corrective Action:
1. COMPLETE THE BIG 4"
2. TRNG SWITCH − FLT
WARNING
 With the FADEC Backup Switch in
backup, N1 matching will occur without
regard to the opposite engine’s current
N1 setting.
 The FADEC Backup Switch shall not
be in the backup position when an engine
is at training idle.
3. FADEC BACKUP SWITCH (affected engine) −
BACKUP
4. OEI − SET AS NECESSARY
5. LAND AS SOON AS PRACTICABLE
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14
Q

MINOR FADEC/GOVERNOR FAILURE

A

Corrective Action:
1. COMPLETE THE BIG 4”
2. ABORT MISSION. URGENT MISSION MAY BE
COMPLETED

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15
Q

BATTERY OVER TEMPERATURE/THERMAL

RUNAWAY

A

Corrective Action:
1. BATT RELAY SWITCHES − BOTH OF (To prevent
the battery from receiving further charge)
2. LAND AS SOON AS PRACTICABLE

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16
Q

HEATER OVERHEAT

A

Corrective Action:

1. HEAT SWITCH − OFF

17
Q

HOIST CABLE FOULED/DAMAGED

A 
If injury or damage is imminent:
1. ACTIVATE HOIST SHEAR SWITCH WHILE ANNOUNCING
SHEAR. SHEAR. SHEAR." (PAC/
SP/FM)
If conditions permit:
1. PAY OUT SLACK IN CABLE
2. ADVISE PILOT
3. DIRECT THE VESSEL’S CREW TO FREE THE
CABLE
4. IF UNABLE TO FREE THE CABLE OR THE
CABLE IS DAMAGED, AND SITUATION PERMITS,
WRAP THE AREA TO BE CUT WITH ANY
SUITABLE TAPE (TO PREVENT FRAYING) USE
THE CABLE CUTTERS AND SEVER THE
CABLE
5. IF MISSION URGENCY DICTATES A CONTINUED
HOIST, ASSEMBLE THE QUICK
SPLICE AND COMPLETE THE HOIST WITH REMAINING
CABLE LENGTH
18
Q

HOIST FAILURE

A 
Corrective Action:
1. ADVISE THE PILOT COMMITTED" OR NOT
COMMITTED"
If not committed:
2. ABORT THE HOIST
If committed:
2. CHECK THE CABLE AND DRUM FOR FOULING
3. ACTIVATE EMERGENCY HOIST POWER AND
CONTINUE THE HOIST
If hoist power is not restored:
4. ACTIVATE MANUAL OVERRIDE AND CONTINUE
THE HOIST
19
Q

HOIST BOOM FAILURE

A

Corrective Action:
1. HOIST MASTER SWITCH − CHECK CREW POSITION
2. HOIST ACT CONTROL AND HOIST ACT POWER
CIRCUIT BREAKERS (2) − PULL, RESET
(cabin overhead panel − R1 #1 R2 #2)
If boom still does not respond to electrical control inputs:
3. HOIST ACT CIRCUIT BREAKERS (2) − PULL
4. HOIST OPERATOR PENDANT − DISCONNECT
5. MANUAL CRANK − INSTALL
6. MANUALLY CRANK BOOM TO STOWED POSITION
7. MANUAL CRANK − REMOVE
If unable to move boom:
8. CONTINUE FLIGHT AS APPROPRIATE (Observe
hatch/door speed limits, if applicable.)

20
Q

HOIST ELECTRICAL RUNAWAY

A 
Corrective Action:
1. SECURE HOIST POWER AT THE HOIST CONTROL
PANEL ONLY
2. ADVISE THE PILOT COMMITTED" OR NOT
COMMITTED"
If committed to the hoist or mission urgency dictates:
3. ACTIVATE MANUAL OVERRIDE AND CONTINUE
THE HOIST
If not committed to the hoist:
3. ABORT THE HOIST
21
Q

LOST COMMUNICATIONS DURING HOISTING

OPERATIONS

A 
Corrective Action:
1. FLIGHT MECH − TAP THE PILOT AND GIVE
HOLD SIGNAL (closed fist)
2. ADVISE THE PILOT COMMITTED" OR NOT
COMMITTED"
If not committed:
3. ABORT HOIST
If committed:
3. FLIGHT MECH − ENSURE HOT MIC IS SELECTED,
HELMETS PROPERLY CONNECTED; ATTEMPT
HOT MIC ICS COMMS
If communications are not restored:
4. PRESS PUSH−TO−TALK SWITCH; ATTEMPT
NORMAL COMMS
If communications are still not restored:
5. AUDIO CONTROL PANEL − SELECT ALTN AND
ATTEMPT COMMS (ALL CALL and HOT MIC are
inoperative in ALTN)
If communications are still not restored and you are
committed to hoist, or mission urgency dictates:
6. COMMUNICATE BY VOCAL COMMANDS AND
CONTINUE HOIST
22
Q

LOST SWIMMER

Corrective Action − DAY:

A
  1. MARK POSITION
  2. TRANSITION AND ESTABLISH RIGHT ORBIT
  3. LOOK AND LISTEN FOR RS SIGNAL
  4. WHEN VISUAL − RESUME HOVER POSITION
    If these procedures fail to relocate RS:
  5. COMPLETE LEAVING RESCUE SWIMMER ON
    SCENE PROCEDURE
23
Q

LOST SWIMMER

Corrective Action − NIGHT

A
  1. MARK POSITION
  2. FLASH LANDING/HOVER LIGHT
  3. LOOK AND LISTEN FOR RS SIGNAL
  4. WHEN VISUAL − CEASE FLASHING LIGHT
    If these procedures fail to relocate RS:
  5. COMPLETE LEAVING RESCUE SWIMMER ON
    SCENE PROCEDURE
24
Q

LEAVING RESCUE SWIMMER ON SCENE

A
  1. MARK AND RECORD POSITION
  2. DEPLOY LIGHTED RAFT
  3. DEPLOY DMB
  4. NOTIFY OPCEN OR OTHER RESCUE RESOURCE
25
Q

IMMEDIATE EMERGENCY LANDING/DITCHING

A

Corrective Action:

  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
26
Q

EMERGENCY DITCHING/LANDING PROCEDURE

A
  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:
  7. DOORS − JETTISON IN A CLIMB @ 70 KIAS IF
    ABLE; OTHERWISE @ 200 FEET @ 70 KIAS,
    STRAIGHT AND LEVEL
  8. PRIOR TO WATER ENTRY − FLOATS INFLATE
  9. ENTER WATER IN A LEVEL ATTITUDE
  10. FADEC CONTROL SWITCHES − OFF
  11. ROTOR − ALLOW TO COAST DOWN
  12. EGRESS HELICOPTER WHEN ROTOR STOPS
27
Q

EMERGENCY EGRESS PROCEDURES

A
  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
28
Q

MALFUNCTIONING CABIN

SLIDING DOOR

A

Corrective Action:
1. FLIGHT MECHANIC − REMAIN SECURED TO
AIRCRAFT

Emergency Procedures (1 decks)

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