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Apache AH64E AQC > Emergency Procedures - Immediate Actions - FRCs > Flashcards

Emergency Procedures - Immediate Actions - FRCs Flashcards

1
Q

Define ‘Land without Delay

A

A landing in which the primary consideration is continued control of the aircraft and survival of the occupants. It is meant to be more urgent than Land As Soon As Possible. The situation may not not permit the crew to continue to manoeuvre the aircraft to a suitable landing area (e.g. open field). If manoeuvring to an open area is not practical, then the crew must make the decision to land in an area that will have the least amount of negative impact on crew survivability, (e.g. over dense forest, select an area with the smallest trees, in a mountainous area, choose an area with the least amount of slope).

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2
Q

Define ‘ Land As Soon As Possible’

A

A landing at the nearest suitable landing area (e.g. open field). The primary consideration is to ensure the survival of occupants.

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3
Q

Define ‘ Land as Soon as Practicable’

A

A landing at the nearest suitable landing area. The primary consideration is the urgency of the emergency.

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4
Q

Emergency Shutdown

A

POWER LEVERS - OFF
APU - OFF (if applicable)
ROTOR BRAKE switch - BRK
MSTR IGN - OFF once the rotors have stopped

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5
Q

Main Transmission Tail Rotor Bevel_Idler Gear Set Failure

A

EMERG HYD button - Press ON
Collective Reduce - Compromise between rate of turn and rate of descent
POWER LEVERS - OFF (10 - 20 feet above touchdown)
Collective - Increase to cushion touchdown

LAND WITHOUT DELAY

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6
Q

HYDRAULIC FAILURE - Primary & Utility Hydraulic PSI Low

A

EMERG HYD Button - Press On

LAND WITHOUT DELAY

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7
Q

DUAL ENGINE FAILURE

A

AUTOROTATE - Rapidly lower collective to maintain Nr within limits

CHOP Button - Reset if an ENGINE CHOP warning message is present

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8
Q

EMERGENCY LANDING IN WOODED AREAS (POWER OFF)

A

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

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9
Q

SINGLE ENGINE FAILURE

A

Achieve safe single engine flight conditions or land

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10
Q

ENGINE 1 or ENGINE 2 OVERSPEED

A

Collective - adjust to maintain Nr within limits

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11
Q

Nr FAILED LOW - LOW ROTOR RPM

A

Collective - Adjust to maintain Nr within limits

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12
Q

ENGINE COMPRESSOR STALL

A

Collective - Reduce

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13
Q

APU FIRE - IN FLIGHT

A

Illuminated APU FIRE button - Press and RDY light illuminates.
FIRE DISCH button(s) - Press

LAND AS SOON AS POSSIBLE

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14
Q

ELECTRICAL FIRE - IN FLIGHT

A

GEN 1 and GEN 2 switches - OFF (see WARNING)

After Landing

EMERGENCY SHUTDOWN (CARD W-4) - Perform

LAND AS SOON AS POSSIBLE

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15
Q

AFT FIRE OR FUSELAGE FIRE - IN FLIGHT OR ON GROUND.

A

After landing or ON GROUND
- EMERGENCY SHUTDOWN (CARD W-4) - Perform

LAND AS SOON AS POSSIBLE

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16
Q

SMOKE AND FUME ELIMINATION

A 
Airspeed - Slow to 20 KTAS maximum
Canopy door (affected crew station) - Open to intermediate position

After Landing

  • EMERGENCY SHUTDOWN (CARD W-4) - Perform

LAND AS SOON AS POSSIBLE

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17
Q

ENGINE 1 or ENGINE 2 FIRE - ON GROUND

A

POWER LEVERS - OFF
Illuminated ENG FIRE button - Press and RDY light illuminates
FIRE DISCH button(s) - Press

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18
Q

APU FRE - ON GROUND

A

APU - OFF
Illuminated APU FIRE button - Press and RDY light illuminates
FIRE DISCH button(s) - Press

19
Q

LOSS OF TAIL ROTOR THRUST - CONTINUED FLIGHT NOT POSSIBLE / LOW AIRSPEED OR HOVER

A

Collective - Reduce (compromise between rate of turn and rate of descent)
POWER LEVERS - OFF (5-10 feet above touchdown)
Collective - Increase to cushion touchdown

20
Q

LOSS OF TAIL ROTOR THRUST - CONTINUED FLIGHT POSSIBLE

A

Airspeed - 100 KTAS minimum (until 10 - 20 feet above touchdown)

21
Q

TAIL ROTOR FIXED PITCH - LOW AIRSPEED OR HOVER

A

Collective - Adjust to minimise yaw rate
Cyclic - minimise drift

If pedals are jammed:

Break into BUCS

If yaw control is restored - proceed with BUCS ON (CARD C-5R)
If yaw control is NOT restored - continue with this card

22
Q

TAIL ROTOR FIXED PITCH - FORWARD FLIGHT

A

Collective - Adjust to minimise yaw rate
Cyclic - minimise drift

If pedals are jammed:

Break into BUCS

If yaw control is restored - proceed with BUCS ON (CARD C-5R)
If yaw control is NOT restored - continue with this card

23
Q

MAIN ROTOR COMPONENTS

A 
After landing: 
EMERGENCY SHUTDOWN (Card W-4) - Perform
24
Q

FLIGHT CONTROL MALFUNCTION

A

FMC release button - Press

25
MAIN XMSN INPUT DRIVE CLUTCH FAILURE - ON GROUND
Fails to Engage: - POWER LEVER (affected ENG) - OFF - Check Ng (affected ENG) - Check less than 10% - Normal engine shutdown - Perform (see CAUTION 1) Fails to Disengage - POWER LEVERS - OFF both engines simultaneously (see CAUTION 2)
26
MAIN XMSN INPUT DRIVE CLUTCH FAILURE - IN FLIGHT
Achieve safe single engine flight conditions or land
27
NVS FAILURE
Exit the NOE environment | Pilot on the controls, NVS select switch - Select alternate sensor (PNVS or TADS)
28
CANOPY JETTISON
Helmet visors - Down Area around helicopter - Clear of personnel CANOPY JETTISON handle - Operate (CAUTION 2)
29
WINGS STORES JETTISON
Airspeed - 130 KTAS (armament) or 100 KTAS (fuel) maximum | COLLECTIVE JETT button - Press
30
SELECTIVE STORES JETTISON
- Airspeed - 130 KTAS (armament) or 100 KTAS (fuel) maximum - Selected Stores Jettison button - Press to ARM - JETT button - Press
31
DITCHING POWER OFF
- Autorotate (apply full collective to decay rotor RPM as helicopter settles) - Canopy - JETTISON prior to entering water - Cyclic - Position in direction of roll - Exit when rotor has stopped
32
DITCHING POWER ON
- Approach to a hover - Canopy - JETTISON prior to entering water - Pilot shoulder harness - Lock - CPG - Exit helicopter - Hover downwind a safe distance - POWER Levers - OFF - Perform hovering autorotation - Apply full collective to decay rotor RPM as helicopter settles - Cyclic - Position in direction of roll - Exit when main rotor has stopped
33
SINGLE MP OPERATION
- NVS SELECT Switch - Reselect (PNVS or TADS) or - Crewmember (not on controls) - Assume control
34
DUAL MP FAILURE - MP1 and MP2 FAIL
``` At night (NVS Flight) - Exit the NOE environment ``` LAND AS SOON AS POSSIBLE
35
EMERGENCY RESPONSE METHOD
``` F - Fly the aircraft A - Alert the crew D - Diagnose the emergency E - Execute emergency procedures C - Communicate the plan F - Fly the aircraft ```
36
AC BUS TIE FAIL
- GEN switch (affected AC BUS TIE) - OFF/RESET, then ON If message is not cleared - GEN switch (affected AC BUS TIE) - OFF
37
AIRDATA MISCOMPARE ALTITUDE (ALT) OR AIRSPEED (A/S)
- CMPR page - Select, Reference the applicable status window (Barometric Altitude or Indicated Airspeed) as depicted by the flight page ALT or A/S indication. - Compare the applicable status window (Barometric Altitude or Indicated Airspeed) information to the SFD. - Select the desired ALT or A/S source (HADS or FMC) that is closest to the SFD altitude or airspeed indication
38
APU ON
APU Button - Press
39
BUCS FAIL
Transfer Flight controls to rear crew station
40
BUCS ON
- EUFD check - Confirm crew station indicated in the BUCS ON Caution message is on the flight controls (BUCS ON PLT* or BUCS ON CPG*) After landing: - APU - Press on - POWER LEVERS - OFF LAND AS SOON AS POSSIBLE
41
DUAL ENGINE FUEL PSI LOW
FUEL Page, BOOST button - Press ON LAND AS SOON AS POSSIBLE
42
ENGINE 1 or ENGINE OIL BYPASS
- Achieve safe single engine flight conditions or land | - POWER LEVER (affected engine) - IDLE
43
IHADSS HOT
- WPN UTIL page - IHADSS TEMP ORID button select if continued use is required.
44
IHADSS FAIL OR IHADSS STALE
``` At night (NVS flight) - Exit the NOE environment ```

Apache AH64E AQC (4 decks)

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