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UH-60M EP > UH-60M EP Ch6 > Flashcards

UH-60M EP Ch6 Flashcards

1
Q

SINGLE-ENGINE FAILURE.

A

SINGLE-ENGINE FAILURE.

1. Collective — Adjust to maintain NR.

2. External cargo/stores — Jettison (if required).

3. Establish single-engine airspeed.

If continued flight is not possible:

4. LAND AS SOON AS POSSIBLE.

If continued flight is possible:

  1. LAND AS SOON AS PRACTICABLE.
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2
Q

DUAL-ENGINE FAILURE.

A

AUTOROTATE.

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3
Q

DECREASING NR.

A

1. Collective — Adjust to control NR.

1.1. Establish single-engine airspeed.

If single engine flight cannot be achieved or maintained:

2. ENG POWER CONT lever (low Q/TGT TEMP engine) — LOCKOUT. Maintain Q approximately 10% below other engine.

  1. LAND AS SOON AS PRACTICABLE.
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4
Q

INCREASING NR.

A

1. ENG POWER CONT lever (high Q/TGT engine) — Retard. Maintain Q approximately 10% below other engine.

  1. LAND AS SOON AS PRACTICABLE.

If the affected engine does not respond to ENG POWER CONT lever movement in the range between FLY and IDLE, the HMU may be malfunctioning internally.

If this occurs:

3. Establish single engine airspeed.

  1. Perform EMER ENG SHUTDOWN (affected
    engine) .
  2. Refer to single-engine failure emergency

procedure.

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5
Q

ENGINE COMPRESSOR STALL.

A

1. Establish single engine airspeed.

2. Collective — Reduce.

If condition persists:

3. ENG POWER CONT lever (affected engine) — Retard (TGT should decrease).

  1. ENG POWER CONT lever (affected engine) — FLY.

If stall condition recurs:

  1. EMER ENG SHUTDOWN (affected engine).
  2. Refer to single-engine failure emergency procedure.
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6
Q

ENG 1 OIL BYPASS OR ENG 2 OIL BYPASS CAUTION APPEARS.

A

1. Establish single engine airspeed.

  1. ENG POWER CONT lever — Retard.
  2. LAND AS SOON AS PRACTICABLE.
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7
Q

CHIP ENG 1 OR CHIP ENG 2, ENG 1 OIL PRESS OR ENG 2 OIL PRESS, ENG 1 OIL HOT OR ENG 2 OIL HOT CAUTION APPEARS.

A

1. Establish single engine airspeed.

  1. ENG POWER CONT lever (affected engine) — Retard (to reduce torque).

If oil pressure is below minimum limits or if oil

temperature remains above maximum limits:

  1. EMER ENG SHUTDOWN (affected engine).
  2. Refer to single engine failure emergency procedure.
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8
Q

ENGINE HIGH-SPEED SHAFT FAILURE.

A

1. Establish single engine airspeed.

2. Collective — Adjust.

3. EMER ENG SHUTDOWN (affected engine).

Do not attempt to restart.

  1. Refer to single-engine failure emergency

procedure.

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9
Q

LIGHTNING STRIKE.

A

1. ENG POWER CONT levers — Adjust (as required to control NP and NR).

2. LAND AS SOON AS POSSIBLE.

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10
Q

LOSS OF TAIL ROTOR THRUST IN CRUISE FLIGHT.

A

1. Airspeed — Adjust to 80 KIAS or above.

2. AUTOROTATE — Maintain airspeed at or above 80 KIAS.

3. ENG POWER CONT levers — OFF (during deceleration when intended point of landing is assured).

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11
Q

LOSS OF TAIL ROTOR THRUST OR T/R QUAD FAIL CAUTION APPEARS WITH LOSS OF CONTROL AT LOW AIRSPEED/HOVER (RIGHT ROTATION).

A

1. Collective — Reduce.

2. ENG POWER CONT levers — OFF (5 to 10 feet above touchdown).

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12
Q

T/R QUAD FAIL CAUTION APPEARS IN CRUISE FLIGHT.

A

1. Collective — Adjust to determine controllability (Fixed Right or Left).

  1. LAND AS SOON AS PRACTICABLE
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13
Q

LOSS OF CONTROL AT LOW AIRSPEED/HOVER OR T/R QUAD FAIL CAUTION APPEARS (LEFT ROTATION).

A

1. ENG POWER CONT lever(s) — Retard to decrease NR below 100% and begin a partial power descent.

2. Collective — Adjust to preserve NR.

3. ENG POWER CONT levers — OFF (5 to 10 feet above touchdown).

4. Collective — Adjust for landing.

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14
Q

PEDAL BIND/RESTRICTION OR DRIVE WITH NO ACCOMPANYING CAUTION.

A

1. Apply pedal force to oppose the drive.

  1. Check other pedals for proper operation.
  2. TAIL SERVO switch — BACKUP.

If normal control authority is not restored:

  1. TAIL SERVO switch — NORMAL.
  2. SAS/BOOST switch — OFF.

If normal control forces are not restored:

  1. SAS/BOOST switch — ON.
  2. Collective — Adjust to determine controllability for landing.
  3. LAND AS SOON AS PRACTICABLE.
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15
Q

T/R SERVO 1 FAIL CAUTION APPEARS AND BACK UP PUMP ON ADVISORY DOES NOT APPEAR OR T/R SERVO 2 ON ADVISORY DOES NOT APPEAR.

A

Automatic switch over did not take place.

1. TAIL SERVO switch — BACKUP.

  1. BACKUP HYD PUMP switch — ON.
  2. LAND AS SOON AS PRACTICABLE.
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16
Q

MAIN XMSN PRESS CAUTION APPEARS/MAIN XMSN OIL HOT CAUTION APPEARS.

A

1. LAND AS SOON AS POSSIBLE.

If time permits:

  1. Slow to 80 KIAS.
  2. EMER APU START.
  3. GENERATORS NO. 1 and NO. 2 switches — OFF.
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17
Q

CHIP L INPUT MDL OR CHIP R INPUT MDL CAUTION APPEARS.

A

1. Establish single engine airspeed.

2. ENG POWER CONT lever (affected engine) — IDLE.

3. LAND AS SOON AS POSSIBLE.

18
Q

CHIP MAIN MDL SUMP, CHIP L ACC MDL OR CHIP R ACC MDL, CHIP TAIL XMSN, TAIL XMSN OIL HOT, CHIP INT XMSN OR INT XMSN OIL HOT CAUTION APPEARS.

A

LAND AS SOON AS POSSIBLE.

19
Q

MAIN TRANSMISSION FAILURE.

A

1. Collective — Adjust only enough to begin a descent with power remaining applied to the main transmission throughout the descent and landing.

2. LAND AS SOON AS POSSIBLE.

20
Q

ENGINE/FUSELAGE FIRE ON GROUND.

A

1. ENG POWER CONT levers — OFF.

2. ENG EMER OFF T-handle — Pull if applicable.

3. FIRE EXTGH switch — MAIN/RESERVE as

required.

4. Rotor Brake — As required.

21
Q

APU COMPARTMENT FIRE.

A

1. APU fire T-handle — Pull.

2. FIRE EXTGH switch — MAIN/RESERVE as required.

22
Q

ENGINE FIRE IN FLIGHT.

A

1. Establish single engine airspeed.

2. ENG POWER CONT lever (affected engine) — OFF.

3. ENG EMER OFF handle — Pull.

4. FIRE EXTGH switch — MAIN/RESERVE as required.

5. LAND AS SOON AS POSSIBLE.

23
Q

ELECTRICAL FIRE IN FLIGHT.

A

1. BATT and GENERATORS switches — OFF.

2. LAND AS SOON AS POSSIBLE.

24
Q

FUEL 1 BYPASS AND FUEL 2 BYPASS CAUTIONS APPEAR.

A

LAND AS SOON AS POSSIBLE.

25
Q

FUEL 1 PRESS LOW OR FUEL 2 PRESS LOW CAUTION APPEARS.

A

If the caution appears and the situation is critical:

1. ENG FUEL SYS selector on affected engine — XFD.

2. FUEL BOOST PUMP switch on side being used — ON.

3. LAND AS SOON AS POSSIBLE.

4. EMER ENG SHUTDOWN after landing.

If the caution appears, and the situation is not critical:

  1. ENG FUEL SYS selector on affected engine — XFD.
  2. FUEL BOOST PUMP CONTROL switches — NO. 1 PUMP and NO. 2 PUMP — OFF (As applicable).
  3. LAND AS SOON AS PRACTICABLE.
26
Q

FUEL 1 PRESS LOW AND FUEL 2 PRESS LOW CAUTIONS APPEAR.

A

1. LAND AS SOON AS POSSIBLE.

2. EMER ENG SHUTDOWN after landing.

27
Q

HYD PUMP 1 FAIL AND HYD PUMP 2 FAIL CAUTIONS APPEAR.

A

LAND AS SOON AS POSSIBLE. Restrict control movement to moderate rates.

28
Q

HYD PUMP 1 FAIL OR HYD PUMP 2 FAIL CAUTION APPEARS AND BACK UP PUMP ON ADVISORY DOES NOT APPEAR.

A

1. Airspeed — Adjust to a comfortable airspeed.

2. BACKUP HYD PUMP switch — ON.

If BACKUP PUMP ON advisory still does not appear:

3. FPS and SAS/BOOST switches — Press off (switch lights off, for HYD PUMP 2 FAIL caution).

4. LAND AS SOON AS POSSIBLE.

29
Q

PRI SERVO 1 FAIL OR PRI SERVO 2 FAIL CAUTION APPEARS.

A

1. SERVO OFF switch — Check centered.

2. If the caution appears with the SERVO OFF switch centered, move the SERVO OFF switch to turn off the malfunctioning servo.

3. LAND AS SOON AS POSSIBLE.

30
Q

RSVR 1 LOW AND HYD PUMP 1 CAUTIONS APPEAR WITH BACK UP PUMP ON ADVISORY APPEARING.

A
  1. LAND AS SOON AS PRACTICABLE.

If the BACK UP RSVR LOW caution also appears:

2. SERVO OFF switch — 1ST STG.

3. LAND AS SOON AS POSSIBLE.

31
Q

RSVR 2 LOW AND HYD PUMP 2 FAIL CAUTIONS APPEAR WITH BACK UP PUMP ON ADVISORY APPEARING.

A
  1. AUTO FLIGHT CONTROL panel CPTR 1 and/or CPTR 2 switches (if illuminated) — Press to reset FCC.
  2. LAND AS SOON AS PRACTICABLE.

If BACK UP RSVR LOW caution also appears:

3. SERVO OFF switch — 2ND STG.

4. LAND AS SOON AS POSSIBLE.

32
Q

COLLECTIVE BOOST SERVO HARDOVER/POWER PISTON FAILURE.

A

1. SAS/BOOST switch — Off.

  1. FPS switch — Off.
  2. LAND AS SOON AS PRACTICABLE
33
Q

BOOST SERVO OFF CAUTION APPEARS.

A

1. SAS/BOOST switch — Off.

  1. FPS switch — Off.
  2. LAND AS SOON AS PRACTICABLE.
34
Q

EMERGENCY LANDING IN WOODED AREAS — POWER OFF.

A

1. AUTOROTATE. Decelerate helicopter to stop all forward speed at treetop level.

2. Collective adjust to maximum before main rotor contacts tree branches.

35
Q

FLIGHT CONTROL/MAIN-ROTOR SYSTEM MALFUNCTIONS.

A

If the main rotor system malfunctions:

1. LAND AS SOON AS POSSIBLE.

2. EMER ENG(S) SHUTDOWN after landing.

3. Rotor Brake — As required.

36
Q

STABILATOR MALFUNCTION — AUTO MODE FAILURE.

A

If an AUTO mode failure occurs:

1. Cyclic mounted stabilator slew-up switch — Adjust if necessary to arrest or prevent nose down pitch rate.

2. AUTO CONTROL RESET switch — Press ON once after establishing a comfortable airspeed.

If automatic control is not regained:

  1. Manually slew stabilator — Adjust to 0° for

flight above 40 KIAS or full down when airspeed

is below 40 KIAS. The preferred method

of manually slewing the stabilator up is to use

the cyclic mounted stabilator slew-up switch.

  1. LAND AS SOON AS PRACTICABLE.

If manual control is not possible, the airspeed limit

indication will show the adjusted airspeed limit with a red

arc.

  1. Airspeed indicator — Check and fly at or below

red arc shown on the indicator.

  1. LAND AS SOON AS PRACTICABLE.
37
Q

UNCOMMANDED NOSE DOWN/UP PITCH ATTITUDE CHANGE.

A

If an uncommanded nose down pitch attitude occurs:

1. Cyclic — Adjust as required.

2. Collective — Maintain or increase.

3. Cyclic mounted stabilator slew-up switch — Adjust as required to arrest nose down pitch rate.

  1. MAN SLEW switch — Adjust to 0° at airspeeds above 40 KIAS and full down at airspeeds below 40 KIAS.
  2. LAND AS SOON AS PRACTICABLE.

If an uncommanded nose up pitch attitude occurs:

1. Cyclic — Adjust as required.

2. Collective — Reduce as required.

  1. MAN SLEW switch — Adjust to 0° a t airspeeds above 40 KIAS and full down at airspeeds below 40 KIAS.
  2. LAND AS SOON AS PRACTICABLE.
38
Q

STAB UNLOCKED CAUTION APPEARS.

A

In flight — LAND AS SOON AS POSSIBLE.

39
Q

DUAL EGI FAILURE.

A

1. Transition to ESIS display.

  1. EGI switches — OFF, then ON. If successful,

an EGI inflight alignment will automatically be

done.

  1. LAND AS SOON AS PRACTICABLE.
40
Q

FLT DIR FAIL, FD COUPLE FAIL CAUTIONS APPEAR.

A

1. Check FD/DCP to verify which flight director modes are functioning.

  1. FAILURE RESET CPTR 1 and/or CPTR 2 — Press to clear flight director cautions.
  2. Check AFCS and FCC status page. Clear BITE codes if necessary.
  3. Reengage affected mode when able.
  4. Fly affected axis manually if not restored.
41
Q
A

UH-60M EP (1 decks)

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