Chapter 9 Flashcards

Emergency Procedures

1
Q

Emergency Shutdown - Immediate Actions

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

CANOPY JETTISON - Immediate Actions

A
  1. Helmet visors - Down.
  2. Area around helicopter - Clear of personnel.
  3. CANOPY JETTISON handle – Operate
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2
Q

Dual Engine Failure- Low Altitude/ Low Airspeed and Cruise - Immediate Actions

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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3
Q

ABORT START PROCEDURES

A
  1. POWER lever - OFF.
  2. ENG START switch - IGN ORIDE for 30 seconds and TGT is below 540° C.
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4
Q

Single Engine Failure - Low Altitude/ Low Airspeed and Cruise - Immediate Actions

A
  1. Achieve safe single engine flight conditions or land
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5
Q

Engine 1 or 2 Overspeed - Np Failed High - Immediate Actions

A
  1. Collective - Adjust to maintain NR within limits.
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6
Q

Np Failed Low - Low RPM Rotor - Immediate Actions

A
  1. Collective - Adjust to maintain NR within limits.
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7
Q

Engine Compressor Stall - Immediate Actions

A
  1. Collective - Reduce.
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8
Q

Main Transmission Tail Rotor Bevel-Idler Gear Set Failure - Immediate Actions

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
  5. LAND WITHOUT DELAY
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9
Q

LOSS OF TAIL ROTOR THRUST IN CRUISE FLIGHT - CONTINUED FLIGHT POSSIBLE - Immediate Actions

A
  1. Airspeed - 100 KTAS minimum (until 10 to 20 ft above touchdown).
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10
Q

LOSS OF TAIL ROTOR THRUST IN CRUISE FLIGHT - CONTINUED FLIGHT NOT POSSIBLE - Immediate Actions

A
  1. Collective - Reduce (compromise between rate of turn and rate of descent)
  2. POWER LEVERS - OFF (5 to 10 feet above touchdown).
  3. Collective - Increase to cushion touchdown
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11
Q

TAIL ROTOR FIXED PITCH - LOW AIRSPEED OR HOVER - Immediate Actions

A
  1. Collective - Adjust to minimize Yaw rate
  2. Cyclic - Minimize drift
    If pedals are jammed:
  3. Break into BUCS
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12
Q

TAIL ROTOR FIXED PITCH - FORWARD FLIGHT - Immediate Actions

A
  1. Collective - Adjust to minimize Yaw rate
  2. Cyclic - Oppose Yaw
    If pedals are jammed:
  3. Break into BUCS
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13
Q

MAIN TRANSMISSION INPUT DRIVE CLUTCH FAILURE - IN FLIGHT - Immediate Actions

A
  1. Achieve safe single engine flight conditions or land
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14
Q

ENGINE 1 OR ENGINE 2 FIRE - IN FLIGHT - Immediate Actions

A
  1. Achieve safe single engine flight condition or land
  2. Illuminated ENG FIRE button - Press and RDY light illuminates.
  3. FIRE DISCH button(s) - Press.
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15
Q

ENGINE 1 OR ENGINE 2 FIRE - ON GROUND - Immediate Actions

A
  1. POWER LEVERS - OFF
  2. Illuminated ENG FIRE button - Press and RDY light illuminates.
  3. FIRE DISCH button(s) - Press.
16
Q

APU FIRE - ON GROUND - Immediate Actions

A
  1. APU - OFF.
  2. Illuminated APU FIRE button - Press and RDY light illuminates.
  3. FIRE DISCH button(s) - Press.
17
Q

APU FIRE - IN FLIGHT - Immediate Actions

A
  1. Illuminated button APU FIRE Button - Press and RDY light illuminates.
  2. FIRE DISCH button(s) - Press.
18
Q

HYDRAULIC FAILURE - PRIMARY & UTILITY HYDRAULIC PSI LOW - Immediate Actions

A
  1. EMERG HYD button - Press ON.
  2. LAND WITHOUT DELAY
19
Q

EMERGENCY LANDING IN WOODED AREAS (POWER OFF) - Immediate Actions

A
  1. AUTOROTATE - Apply full collective to decay rotor RPM as helicopter settles.
20
Q

DITCHING (POWER OFF) - Immediate Actions

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 main rotor has stopped.
21
Q

BUCS Fail - Immediate Actions

A
  1. Transfer flight controls to rear crew station
22
Q

FLIGHT CONTROL MALFUNCTION - STABILIZATION EQUIPMENT/FORCE TRIM - Immediate Actions

A
  1. FMC release button - Press.
23
Q

NVS Failure - Immediate Actions

A
  1. Exit the NOE environment
  2. Pilot on the controls, NVS Select Switch - Select alternate sensor (PNVS or TADS)
24
Q

IHADSS/HDU Failure or IHADSS STALE - Immediate Actions

A

At night (NVS flight)
1. Exit the NOE environment

25
Q

Single MP Operation - Immediate Actions

A
  1. NVS SELECT Switch - Reselect (PNVS or TADS).
    or
  2. Crewmember (not on controls) - Assume control
26
Q

Dual MP Failure - Immediate Actions

A

At Night (NVS Flight)
1. Exit the NOE environment

27
Q

Both ENG 1 FUEL PSI LOW and ENG 2 FUEL PSI LOW

A

FUEL Page BOOST button – Press ON