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AH-64D > Chapter 9 - Emergency Procedures > Flashcards

Chapter 9 - Emergency Procedures Flashcards

1
Q

EMERGENCY EGRESS

A
  1. Helmet visors — Down.
  2. Area around helicopter — Clear of personnel.
  3. CANOPY JETTISON handle — Turn 90°, release, then push to jettison canopy.
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2
Q

DUAL ENGINE FAILURE

A
  1. AUTOROTATE.
  2. CHOP button — Rest only if engine chop warning is present.
  3. Wing Stores Jettison — As appropriate.
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3
Q

SINGLE ENGINE FAILURE

A
  1. Airspeed — Adjust as appropriate.
  2. Wing Stores Jettison — As appropriate.
  3. LAND AS SOON AS PRACTICABLE.
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4
Q

ABORTING ENGINE START

A
  1. POWER lever — OFF.

2. ENG START switch — IGN ORIDE for 30 seconds and TGT is below 540° C.

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5
Q

ENGINE OVERSPEED — Np FAILED HIGH

A
  1. Collective — Adjust to maintain Nr within limits.

If condition persists:

  1. POWER lever (affected engine) — Retard to equalize torque/Ng.
  2. LAND AS SOON AS PRACTICABLE.
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6
Q

LOW RPM ROTOR — Np FAILED LOW

A
  1. Collective — Adjust to maintain Nr within limits.

If condition persists:

  1. POWER lever (affected engine) — LOCKOUT and then retard to equalize torque output of both engines.

If manual control is not possible:

  1. POWER lever (affected engine) — IDLE.
  2. LAND AS SOON AS PRACTICABLE.
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7
Q

ENGINE COMPRESSOR STALL

A
  1. Collective — Reduce.

If condition persists:

  1. POWER lever (affected engine) — Retard.

If TGT decreases and there is no further evidence of a stall:

  1. POWER lever (affected engine) — FLY.

If stall condition recurs:

  1. POWER lever (affected engine) — IDLE.
  2. LAND AS SOON AS PRACTICABLE.
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8
Q

LOSS OF TAIL ROTOR THRUST IN CRUISE FLIGHT

Continued flight is possible:

A
  1. Airspeed — 100 KTAS minimum (until 10 to 20 feet above touchdown).
  2. Wing Stores Jettison — As appropriate.
  3. POWER levers — Retard as necessary (5 to 10 feet above touchdown).
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9
Q

LOSS OF TAIL ROTOR THRUST IN CRUISE FLIGHT

Continued flight is not possible:

A
  1. Collective reduce (compromise between rate of turn and rate of decent).
  2. Wing Stores Jettison — As appropriate.
  3. Minimize rate of descent (10 to 20 feet above touchdown).
  4. POWER levers — OFF (5 to 10 feet above touchdown).
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10
Q

LOSS OF TAIL ROTOR THRUST AT LOW AIRSPEED/HOVER

A
  1. Collective - Reduce (compromise between rate of turn and rate of decent).
  2. Wing Stores Jettison — As appropriate.
  3. Minimize Rate of Descent (10 to 20 feet above touchdown).
  4. POWER levers — OFF (5 to 10 feet above touchdown).
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11
Q

MAIN TRANSMISSION INPUT DRIVE CLUTCH FAILURE

In flight:

A
  1. POWER lever (affected engine) — IDLE.

If Np (affected engine) is below Nr (indicating the clutch is disengaged):

  1. EMERG ENG SHUTDOWN (affected engine).
  2. LAND AS SOON AS PRACTICABLE.

If Np (affected engine) does not drop below Nr (indicating the clutch has failed to disengaged):

  1. LAND AS SOON AS POSSIBLE.
  2. EMERG ENG SHUTDOWN (both engines simultaneously).
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12
Q

MAIN TRANSMISSION INPUT DRIVE CLUTCH FAILURE

On Ground:

A

With indications that a clutch has failed to engage:

  1. EMERG ENG SHUTDOWN (affected engine only).
  2. Check Ng is less than 10% (affected engine).
  3. Normal engine shutdown — Perform.

With indications that a clutch has failed to disengage:

EMERG ENG SHUTDOWN ( both engine’s simultaneously).

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13
Q

ENGINE FIRE

On Ground:

A
  1. EMERG ENG(S) SHUTDOWN.
  2. Illuminated ENG FIRE button — Press and RDY light illuminates.
  3. FIRE DISCH button(s) — Press.
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14
Q

ENGINE FIRE

In Flight:

A
  1. EMERG ENG SHUTDOWN — (affected engine) when conditions permit.
  2. Illuminated ENG FIRE button — Press and RDY light illuminates.
  3. FIRE DISCH button(s) — Press.
  4. LAND AS SOON AS POSSIBLE.
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15
Q

APU COMPARTMENTS FIRE

On Ground:

A
  1. APU — OFF
  2. Illuminated APU FIRE button — Press and RDY light illuminates.
  3. FIRE DISCH button(s) — Press.
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16
Q

APU COMPARTMENT FIRE

In Flight:

A
  1. Illuminated APU FIRE button — Press and RDY light illuminates.
  2. FIRE DISCH button(s) — Press.
  3. LAND AS SOON AS POSSIBLE.
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17
Q

DECK FIRE

A

LAND AS SOON AS POSSIBLE.

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18
Q

FUSELAGE FIRE ON GROUND

A
  1. EMERG ENG(S) SHUTDOWN.

2. APU — OFF (if applicable).

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19
Q

ELECTRICAL FIRE IN FLIGHT

A
  1. GEN1 and GEN2 — OFF (SYS page).

2. LAND AS SOON AS POSSIBLE.

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20
Q

SMOKE AND FUME ELIMINATION

A
  1. Airspeed — Slow to 20 KTAS maximum.
  2. Canopy door (affected crew station) — Open to intermediate position.
  3. LAND AS SOON AS POSSIBLE.
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21
Q

BOTH GENERATORS FAIL / COMPLETE LOSS OF ELECTRICAL POWER.

A
  1. GEN1 and GEN2 — Reset Pilot GEN RST panel.

If condition persists:

  1. LAND AS SOON AS POSSIBLE.
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22
Q

SINGLE GENERATOR AND SINGLE RTRU FAILURE.

A
  1. Affected GEN1 or GEN2 — Reset Pilot GEN RST panel.

If condition persists:

  1. LAND AS SOON AS PRACTICABLE.
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23
Q

DUAL TRU FAILURE

A
  1. LAND AS SOON AS POSSIBLE.
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24
Q

PRIMARY HYDRAULIC PRESSURE LOW AND UTILITY HYDRAULIC PRESSURE LOW.

The EUFD will display HYDRAULIC FAIL message.

A
  1. EMERG HYD button — Press ON.
  2. LAND WITHOUT DELAY.
  3. EMERG ENG(S) SHUTDOWN.
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25
Q

PRIMARY HYDRAULIC PRESSURE LOW AND UTILITY HYDRAULIC LEVEL LOW.

The EUFD will display TAIL ROTOR HYD message.

A
  1. LAND AS SOON AS POSSIBLE.
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26
Q

EMERGENCY LANDING IN WOODED AREAS (POWER OFF)

A
  1. AUTOROTATE — Apple full collective to decay rotor RPM as helicopter settles.
27
Q

DITCHING (POWER ON)

A
  1. Approach to hover.
  2. Canopies — JETTISON Prior to entering water.
  3. Pilot Shoulder harness — Lock.
  4. CPG — Exit helicopter.
  5. Hover downwind to a safe distance.
  6. POWER levers — OFF.
  7. Perform hovering autorotation — Apply full collective to decay rotor RPM as helicopter settles.
  8. Cyclic — Position in the direction of the roll.
  9. Exit when the main rotor has stopped.
28
Q

DITCHING (POWER OFF)

A
  1. AUTOROTATE — Apple full collective to decay rotor RPM s as helicopter settles.
  2. Canopies — JETTISON Prior to entering water.
  3. Cyclic — Position in the direction of the roll.
  4. Exit when the main rotor has stopped.
29
Q

BUCS FAIL OR BUCS ON

A
  1. LAND AS SOON AS POSSIBLE.
  2. APU — ON.
  3. EMERG ENG(S) SHUTDOWN.
30
Q

MAIN ROTOR SYSTEM MALFUNCTION

A
  1. LAND AS SOON AS POSSIBLE

2. EMERG ENG(S) SHUTDOWN.

31
Q

STABILIZATION EQUIPMENT MALFUNCTION

A
  1. FMC release button — Press.

2. FMC — Re-engage unaffected FMC axes (A/C UTIL page).

32
Q

WING STORES JETTISON

All Armament Wing Stores:

A
  1. Airspeed — 130 KTAS maximum.

2. Collective JETT button — Press.

33
Q

WING STORES JETTISON

Selected Armament Stores:

A
  1. Airspeed — 130 KTAS maximum.
  2. Selected STORES JETTISON buttons— Press to ARM.
  3. JETT button — Press.
34
Q

PNVS FAILURE

A
  1. NVS selects switch (Pilot) — TADS.
35
Q

IHADSS SINGLE DP FAILURE

A
  1. NVS SELECTS switch — Reselect (PNVS or TADS).

2. Crewmember (not on the controls) — Assumes control.

36
Q

ENG OIL PSI

A
  1. EMERG ENG SHUTDOWN when conditions permit.

2. LAND AS SOON AS PRACTICABLE.

37
Q

ACC OIL PSI LOW

A

APU only: Shutdown as soon as possible.

In Flight: LAND AS SOON AS PRACTICABLE.

38
Q

ROTOR BRAKE ON/LK

A
  1. RTR BRK switch — OFF

2. LAND AS SOON AS POSSIBLE.

39
Q

XFEED VALVE FAIL

A

Achieve safe single engine air speed.

— If CAUTION message extinguishs, continue mission.

— If CAUTION message remains, be prepared for single engine flameout. LANDS AS SOON AS PRACTICABLE.

40
Q

Both ENG1 FUEL PSI LOW and ENG2 FUEL PSI LOW

A
  1. Fuel page, BOOST button — Press ON.

2. LAND AS SOON AS POSSIBLE.

41
Q

ENG FUEL PSI LOW

A
  1. Achieve safe single engine air speed.

2. LAND AS SOON AS PRACTICABLE.

42
Q

GEARBOX TEMP HIGH

A

LAND AS SOON AS PRACTICABLE

IGB or TRGB

43
Q

GEARBOX VIBRATION

A

LAND AS SOON AS POSSIBLE

IGB, TRGB, or APU Clutch

44
Q

GENERATOR FAIL

A
  1. GEN RST Panels — GEN#If condition persists
  2. LAND AS SOON AS PRACTICABLE.
45
Q

MAIN XMSN CHIPS

A

LAND AS SOON AS POSSIBLE

46
Q

FUEL LOW

A

LAND AS SOON AS PRACTICABLE

47
Q

AUTO/MAN STAB FAIL

A

LAND AS SOON AS PRACTICABLE

48
Q

Both RECTIFIER 1 and RECTIFIER 2 FAIL

A

LAND AS SOON AS POSSIBLE

49
Q

XMSN OIL HOT

A

LAND AS SOON AS PRACTICABLE

50
Q

Both XMSN 1 OIL HOT and XMSN 2 OIL HOT.

A

LAND AS SOON AS POSSIBLE

51
Q

XMSN OIL PSI LOW

A

LAND AS SOON AS PRACTICABLE

52
Q

Both XMSN 1 OIL PSI LOW and XMSN 2 OIL PSI LOW

A

LAND AS SOON AS POSSIBLE

53
Q

HYD BYP

A

LAND AS SOON AS PRACTICABLE

54
Q

HYD LEVEL LOW

A

LAND AS SOON AS PRACTICABLE

55
Q

HYD PSI LOW

A

LAND AS SOON AS POSSIBLE

56
Q

Which EUFD Messages require the following action?

  1. POWER lever — IDLE when conditions permit.
  2. LAND AS SOON AS PRACTICABLE
A

ENG CHIPS
ENG FUEL BYPASS
ENG OIL BYPASS

GEARBOX CHIPS
GEARBOX OIL HOT
GEARBOX OIL PSI LOW

57
Q

ENG CHIPS

A
  1. POWER lever — IDLE when conditions permit.

2. LAND AS SOON AS PRACTICABLE

58
Q

ENG FUEL BYPASS

A
  1. POWER lever — IDLE when conditions permit.

2. LAND AS SOON AS PRACTICABLE

59
Q

ENG OIL BYPASS

A
  1. POWER lever — IDLE when conditions permit.

2. LAND AS SOON AS PRACTICABLE

60
Q

GEARBOX CHIPS

A
  1. POWER lever — IDLE when conditions permit.

2. LAND AS SOON AS PRACTICABLE

61
Q

GEARBOX OIL HOT

A
  1. POWER lever — IDLE when conditions permit.

2. LAND AS SOON AS PRACTICABLE

62
Q

GEARBOX OIL PSI

A
  1. POWER lever — IDLE when conditions permit.

2. LAND AS SOON AS PRACTICABLE

63
Q

Which EUFD Messages require the following action?

LAND AS SOON AS PRACTICABLE (7)

A
  • AUTO/MAN STAB FAIL
  • FUEL LOW
  • GEARBOX TEMP HIGH (IGB or TRGB)
  • HYD BYP
  • HYD LEVEL LOW
  • XMSN OIL HOT
  • XMSN PSI LOW
64
Q

Which EUFD Messages require the following action?

LAND AS SOON AS POSSIBLE (6)

A
  • GEARBOX VIBRATION (IGB, TRGB or APU Clutchp)
  • HYD PSI LOW
  • MAIN XMSN CHIPS
  • Both RECTIFIER 1 FAIL and RECTIFIER 2 FAIL
  • Both XMSN 1 OIL HOT and XMSN 2 OIL HOT
  • Both XMSN 1 OIL PSI LOW and XMSN 2 OIL PSI LOW

AH-64D (2 decks)

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