EPs (Emergency Procedures) CH9 Flashcards

1
Q

EMERGENCY SHUTDOWN

A
  1. POWER LEVERS - OFF
  2. APU - OFF (if applicable)
  3. ROTOR BREAK SWITCH - BRK
  4. MSTR IGN - OFF once the rotors have stopped
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2
Q

EMERGENCY EXIT/ENTRANCE - CANOPY JETTISON

A
  1. HELMET VISORS - DOWN
  2. AREA AROUND HELICOPTER - CLEAR OF PERSONNEL
  3. CANOPY JETTISON HANDLE - OPERATE
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3
Q

WARNING: If flares are ignited and lodged in the dispenser, jettison all flare munitions and…

A

LAND AS SOON AS POSSIBLE

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4
Q

DUAL ENGINE FAILURE - LOW

A
  1. AUTOROTATE - rapidly lower collective to maintain NR within limits
  2. CHOP BUTTON - RESET if an ENGINE CHOP warning message is present
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5
Q

ABORT START PROCEDURES

A
  1. POWER LEVER - OFF

2. ENG START SWITCH - IGN ORIDE for 30s and TGT is < 540c

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6
Q

SINGLE ENGINE FAILURE - LOW

A
  1. ACHIEVE SAFE SINGLE ENGINE FLIGHT CONDITIONS OR LAND
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7
Q

ENGINE 1/2 OVERSPEED - NP Failed High

A
  1. COLLECTIVE - ADJUST to maintain NR within limits
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8
Q

NP Failed Low - Low RPM Rotor

A
  1. COLLECTIVE - ADJUST to maintain NR within limits
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9
Q

ENGINE COMPRESSOR STALL

A
  1. COLLECTIVE - REDUCE
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10
Q

MAIN TRANS TAIL ROTOR BEVEL-IDLER GEAR SET FAIL

A
  1. EMERG HYD BUTTON - PRESS ON
  2. COLLECTIVE REDUCE - COMPROMISE BETWEEN RATE OF TURN AND RATE OF DESCENT
  3. POWER LEVERS - OFF 10-20 FEET ABOVE TOUCHDOWN
  4. COLLECTIVE - INCREASE TO CUSHION TOUCHDOWN
    —Urgency to Land:
    LAND WITHOUT DELAY
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11
Q

LTR THRUST (Cruise) - CONT

A
  1. AIRSPEED - 100 KTAS MIN UNTIL 10-20 FEET ABOVE TOUCHDOWN
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12
Q

LTR THRUST (Cruise) - NON CONT

A
  1. COLLECTIVE REDUCE - COMPROMISE BETWEEN RATE OF TURN AND RATE OF DESCENT
  2. POWER LEVERS - OFF 5-10 FEET ABOVE TOUCHDOWN
  3. COLLECTIVE - INCREASE TO CUSHION TOUCHDOWN
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13
Q

TAIL ROTOR FIXED PITCH - LOW/HVR

A
  1. COLLECTIVE - ADJUST TO MINIMIZE YAW RATE
  2. CYCLIC - MINIMIZE DRIFT
    - -If pedals are jammed:
  3. BREAK INTO BUCS
  4. Proceed with BUCS ON
  5. Proceed with this procedure
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14
Q

TAIL ROTOR FIXED PITCH - FWD

A
  1. COLLECTIVE - ADJUST to minimize yaw rate
  2. CYCLIC - OPPOSE YAW
    - -If pedals are jammed:
  3. BREAK INTO BUCS
  4. Proceed with BUCS ON
  5. Proceed with this procedure
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15
Q

MAIN TRANSMISSION INPUT DRIVE CLUTCH FAIL - FLIGHT

A
  1. ACHIEVE SAFE SINGLE ENGINE FLIGHT CONDITIONS OR LAND
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16
Q

ENG 1/2 FIRE - FLIGHT

A
  1. ACHIEVE SAFE SINGLE ENGINE FLIGHT CONDITIONS OR LAND
  2. ILLUMINATED ENG FIRE BUTTON - PRESS and RDY light illuminates
  3. FIRE DISCH BUTTON(S) - PRESS
17
Q

ENG 1/2 FIRE - GROUND

A
  1. POWER LEVERS - OFF
  2. ILLUMINATED ENG FIRE BUTTON - PRESS AND RDY LIGHT ILLUMINATES
  3. FIRE DISCH BUTTON(S) - PRESS
18
Q

APU FIRE - GROUND

A
  1. APU - OFF
  2. ILLUMINATED APU FIRE BUTTON - PRESS and RDY light illuminates
  3. FIRE DISCH BUTTON(S) - PRESS
19
Q

APU FIRE - FLIGHT

A
  1. ILLUMINATED APU FIRE BUTTON - PRESS and RDY light illuminates
  2. FIRE DISCH BUTTON(S) - PRESS
20
Q

HYD FAIL - PRI AND UTIL PSI LOW

A
  1. EMERG HYD BUTTON - PRESS ON
    - -Urgency to Land:
  2. LAND WITHOUT DELAY
21
Q

EMERGENCY LANDING WOODED (POWER OFF)

A

AUTOROTATE - Apply full collective to decay rotor RPM as helicopter settles

22
Q

DITCHING - POWER OFF

A
  1. AUTOROTATE (apply full collective to decay rotor RPM as helicopter settles)
  2. CANOPY - JETTISON PRIOR TO ENTERING WATER
  3. CYCLIC - POSITION IN DIRECTION OF ROLL
  4. EXIT WHEN ROTOR HAS STOPPED
23
Q

BUCS FAIL

A
  1. TRANSFER FLIGHT CONTROLS TO REAR CREW STATION
24
Q

FLIGHT CONTROL MALFUNCTION - STABILIZATION EQUIPMENT

A
  1. FMC RELEASE BUTTON - PRESS
25
Q

NVS FAILURE

A
  1. EXIT THE NOE ENVIRONMENT

2. PILOT ON THE CONTROLS, NVS SELECT SWITCH - SELECT ALTERNATE SENSOR (PNVS or TADS)

26
Q

IHADSS FAILURE

A
  1. EXIT THE NOE ENVIRONMENT
27
Q

SINGLE MP OPERATIONS

A
  1. NVS SELECT SWITCH - RESELECT (PNVS OR TADS)

2. CREW (MEMBER NOT ON CONTROLS) - ASSUME CONTROLS

28
Q

DUAL MP FAILURE

A
  1. EXIT THE NOE ENVIRONMENT
29
Q

TAIL ROTOR HYD

A
  1. LAND AS SOON AS POSSIBLE
30
Q

ENG 1+2 FUEL PSI LOW

A
  1. FUEL PAGE, BOOST BUTTON - PRESS ON