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UH 60M > Ch 9 > Flashcards

Ch 9 Flashcards

1
Q

The term LAND AS SOON AS POSSIBLE is defined as

A

Landing at the nearest suitable landing area (e.g., open field) without delay. (The primary consideration is to ensure the survival of the occupants.)

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2
Q

The term LAND AS SOON AS PRACTICABLE is defined as

A

Landing at a suitable landing area. (The primary consideration is the urgency of the emergency.)

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3
Q

The term AUTOROTATE is defined as

A

Adjusting the flight controls as necessary to establish an autorotational decent and landing.

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4
Q

The term EMER ENG SHUTDOWN is defined as _____.

CAUTION:
If TGT rises above 500 degrees after shutdown, _____.

A

Engine shutdown without delay.

  1. ENG POWER CONT lever(s) - OFF.
  2. ENG FUEL SYS selector(s) - OFF.
  3. FUEL BOOST PUMP switch(es) - OFF.

… place AIR SCE HT/STRT switch as required, turn ENGINE IGNITION switch OFF, and press starter to motor engine for 30 seconds or until TGT decreases below 500 degrees C.

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5
Q

The term LOCKOUT is defined as ____.

  1. _____
A

Manual control of the engine RPM while bypassing DEC/EDECU functions.

ENG POWER CONT lever - Pull down and advance full forward while maintaining downward pressure, then adjust to set NR as required.

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6
Q

The term EMER APU START is defined as _____.

  1. _____
  2. _____
A

APU start to accomplish an emergency procedure.

  1. FUEL PUMP switch - APU BOOST.
  2. APU CONT switch - ON.
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7
Q

SINGLE-ENGINE FAILURE

WARNING: 
1.
2.
3. 
If continued flight is not possible:
4. 
If continued flight is possible:
5.
A

WARNING:
Do not respond to ENG PUT warning and audio until checking TGT, NG, and NP1 and NP2.

  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:
5. LAND AS SOON AS PRACTICABLE

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8
Q

DUAL ENGINE FAILURE

WARNING
1.

A

WARNING: Do not respond to ENG OUT warning lights and audio until checking TGT and NR.

  1. AUTOROTATE
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9
Q

DECREASING NR

  1. ________________________
    1. ______________________

If single engine flight cannot be achieved or maintained:

  1. _______________________
  2. LAND AS SOON AS PRACTICABLE
A
  1. Collective - Adjust to control NR.
    1. Establish single-engine airspeed.

If single engine flight cannot be achieved or maintained:

  1. ENG POWER CONT lever (low Q/TGT engine) - LOCKOUT. Maintain Q approximately 10% below other engine.
  2. LAND AS SOON AS PRACTICABLE
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10
Q

INCREASING NR

  1. ________________
  2. LAND AS SOON AS PRACTICABLE

If they 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:

  1. _________________
  2. Perform ___________ (affected engine)
  3. Refer to single-engine failure emergency procedure.
A
  1. ENG POWER CONT lever (high Q/TGT engine) - Retard. Maintain Q approximately 10% below other engine.
  2. LAND AS SOON AS PRACTICABLE.

…… If this occurs:

  1. Establish single engine airspeed.
  2. Perform EMER ENG SHUTDOWN (affected engine).
  3. Refer to single-engine failure emergency procedure.
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11
Q

ENGINE COMPRESSOR STALL

  1. ______________________________
  2. _____________________________
    If condition persists:
  3. ______________________________
  4. ENG POWER CONT lever (affected engine) - FLY.
    If stall condition recurs:
  5. ______________________________ (affected engine).
  6. Refer to single-engine failure emergency procedure.
A
  1. Establish single engine airspeed.
  2. Collective - Reduce.
    If condition persists:
  3. ENG POWER CONT lever (affected engine) - Retard (TGT should decrease).
  4. ENG POWER CONT lever (affected engine) - FLY
    If stall condition recurs:
  5. EMER ENG SHUTDOWN (affected engine).
  6. Refer to single-engine failure emergency procedure.
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12
Q

ENG 1 or ENG 2 OIL BYPASS CAUTION APPEARS

  1. ____________________
  2. ENG POWER CONT lever (affected engine) - Retard (to reduce torque).
    If this occurs:
  3. LAND AS SOON AS PRACTICABLE.
A
  1. Establish single engine airspeed.
  2. ENG POWER CONT lever - Retard.
  3. LAND AS SOON AS PRACTICABLE.
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13
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

  1. _____________________
  2. ENG POWER CONT lever (affected engine) - Retard (to reduce torque).
    If oil pressure is below minimums limits or if oil temperature remains above maximum limits:
  3. ____________________ (affected engine).
  4. Refer to single-engine failure emergency procedure.
A
  1. Establish single engine airspeed.
  2. ENG POWER CONT lever (affected engine) - Retard (to reduce torque).
    If oil pressure is below minimums limits or if oil temperature remains above maximum limits:
  3. EMER ENG SHUTDOWN (affected engine).
  4. Refer to single-engine failure emergency procedure.
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14
Q

ENGINE HIGH-SPEED SHAFT FAILURE
1. ______________________
2. _____________________
3. _____________________ (affected engine).
Do not attempt to restart.
4. Refer to single-engine failure emergency procedure.

A
  1. Establish single engine airspeed.
  2. Collective - Adjust.
  3. EMER ENG SHUTDOWN (affected engine).
    Do not attempt to restart.
  4. Refer to single-engine failure emergency procedure.
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15
Q

LIGHTNING STRIKE

  1. ___________________
  2. ___________________
A
  1. ENG POWER CONT levers - Adjust (as required to control NP and NR).
  2. LAND AS SOON AS POSSIBLE.
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16
Q

Loss of Tail Rotor Thrust in Cruise Flight

  1. ________________
  2. ________________
  3. ________________
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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17
Q

Loss of Tail Rotor Thrust or T/R QUAD FAIL Caution Appears with Loss of Control at Low Airspeed/Hover (Right Rotation)

  1. ___________
  2. ___________
A
  1. Collective - Reduce.

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

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18
Q

T/R QUAD FAIL Caution Appears in Cruise Flight

  1. _________
  2. LAND AS SOON AS PRACTICABLE.
A
  1. Collective - Adjust to determine controllability (Fixed Right or Left).
  2. LAND AS SOON AS PRACTICABLE.
19
Q

Loss of Control at Low Airspeed/Hover or T/R QUAD FAIL Caution Appears (Left Rotation).

  1. _____________
  2. _____________
  3. _____________
  4. _____________
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.
20
Q

Pedal Bind/Restriction or Drive With No Accompanying Caution

  1. _________
  2. Check other pedals for proper operation.
  3. TAIL SERVO switch - BACKUP.
    If normal control authority is not restored:
  4. TAIL SERVO switch - BACKUP.
  5. SAS/BOOST switch - OFF.
    If normal control forces are not restored:
  6. SAS/BOOST switch - ON.
  7. Collective - Adjust to determine controllability for landing.
  8. LAND AS SOON AS PRACTICABLE.
A
  1. Apply pedal force to oppose the drive.
  2. Check other pedals for proper operation.
  3. TAIL SERVO switch - BACKUP.
    If normal control authority is not restored:
  4. TAIL SERVO switch - BACKUP.
  5. SAS/BOOST switch - OFF.
    If normal control forces are not restored:
  6. SAS/BOOST switch - ON.
  7. Collective - Adjust to determine controllability for landing.
  8. LAND AS SOON AS PRACTICABLE.
21
Q

MAIN XMISN PRESS Caution Appears/MAIN/XMSN OIL HOT Caution Appears
1. _________
If time permits:
2. Slow to 80 KIAS.
3. _________
4. GENERATORS NO. 1 and NO. 2 switches - OFF.

A 
1.  LAND AS SOON AS POSSIBLE. 
If time permits:
2. Slow to 80 KIAS.
3.  EMER APU START.
4.  GENERATORS NO. 1 and NO. 2 switches - OFF.
22
Q

CHIP L INPUT MDL or CHIP R INPUT MDL Caution Light Appears

  1. __________
  2. _________
  3. _________
A
  1. Establish single engine airspeed.
  2. ENG POWER CONT lever (affected engine) - IDLE.
  3. LAND AS SOON AS POSSIBLE.
23
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.

24
Q

MAIN TRANSMISSION FAILURE

  1. _____________
  2. ____________
A
  1. Collective - Adjust only enough to begin a descent with power remaining applied to the main transmission through the descent and landing.
  2. LAND AS SOON AS POSSIBLE.
25
Q

Engine/Fuselage Fire On Ground

1.
2.
3.
4.

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.
26
Q

APU Compartment Fire

1.
2.
3.

A
  1. APU fire T-Handle - Pull
  2. FIRE EXTGH switch - MAIN/RESERVE as required.
  3. LAND AS SOON AS POSSIBLE.
27
Q

Engine Fire In Flight

1.
2.
3.
4.
5.
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.
28
Q

Electrical Fire In Flight

1.
2.

A
  1. BATT and GENERATORS switches - OFF.

2. LAND AS SOON AS POSSIBLE.

29
Q

FUEL 1 PRESS LOW or FUEL 2 PRESS LOW Caution Appears

If the caution appears and the situation is critical:
1.
2.
3.
4.
A
  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.
30
Q

FUEL 1 PRESS LOW and FUEL 2 PRESS LOW Caution Appears

1.
2.

A
  1. LAND AS SOON AS POSSIBLE.

2. EMER ENG SHUTDOWN after landing.

31
Q

HYD PUMP 1 FAIL and HYD PUMP2 FAIL Cautions Appear

1.

A
  1. LAND AS SOON AS POSSIBLE. Restrict control movement to moderate rates.
32
Q

HYD PUMP 1 FAIL or HYD PUMP 2 FAIL Caution Light Appears and BACK-UP PUMP ON Advisory Does Not Appear

  1. _______ to a comfortable airspeed
  2. _______.
    If BACK UP PUMP ON advisory appears:
  3. _______.
    If BACKUP PUMP ON advisory still does not appear:
  4. _______.
  5. _______.
A
  1. _______ to a comfortable airspeed
  2. BACKUP HYD PUMP switch - ON.

If BACK UP PUMP ON advisory appears:
3. Refer to HYD PUMP 1 FAIL or HYD PUMP 2 FAIL caution appears emergency procedure.

If BACKUP PUMP ON advisory still does not appear:

  1. FPS and SAS/BOOSTS switches - Press off (switch lights off, for HYD PUMP 2 FAIL caution).
  2. LAND AS SOON AS POSSIBLE.
33
Q

PRI SERVO 1 FAIL or PRI SERVO 2 FAIL Caution Appears

1.
2.
3.

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.
34
Q

RSVR 2 LOW and HYD PUMP 2 FAIL Cautions Appear With BACK UP PUMP ON Advisory Appearing.

  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.
4.

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:

  1. SERVO OFF switch - 2ND STG.
  2. LAND AS SOON AS POSSIBLE.
35
Q

RSVR 1 LOW and HYD PUMP 1 FAIL Cautions Appear With BACK UP PUMP ON Advisory Appearing.

  1. LAND AS SOON AS PRACTICABLE.

If the BACK UP RSVR LOW caution also appears:
2.
3.

A
  1. LAND AS SOON AS PRACTICABLE.

If the BACK UP RSVR LOW caution also appears:

  1. SERVO OFF switch - 1ST STG.
  2. LAND AS SOON AS POSSIBLE
36
Q

Collective Boost Servo Hardover/Power Piston Failure

1.

  1. FPS switch - Off.
  2. LAND AS SOON AS PRACTICABLE.
A
  1. SAS/BOOST switch - Off.
37
Q

BOOST SERVO OFF Caution Appears

1.
2. LAND AS SOON AS PRACTICABLE.

A
  1. SAS/BOOST and FPS switches - Off
38
Q

Emergency Landing in Wooded Areas - Power Off.

  1. __________. Decelerate helicopter to stop all forward speed at treetop level.
  2. __________________ to maximum before main rotor contacts tree branches.
A
  1. AUTOROTATE. Decelerate helicopter to stop all forward speed at treetop level.
  2. Collective adjust to maximum before main rotor contacts tree branches.
39
Q

Ditching - Power Off

  1. _________________
  2. Cockpit doors jettison and cabin doors open prior to entering water.
  3. Apply full collective to decay rotor rpm as helicopter settles.
  4. Position cyclic in direction of roll.
  5. Exit when main rotor has stopped.
A
  1. Approach to a hover.
40
Q

FLIGHT CONTROL/MAIN-ROTOR SYSTEM MALFUNCTIONS

If the main rotor system malfunctions:
1.
2.
3.

A
  1. LAND AS SOON AS POSSIBLE.
  2. EMER ENG(S) SHUTDOWN after landing.
  3. Rotor Brake - As Required.
41
Q

STABILATOR MALFUNCTION-AUTO MODE FAILURE

If an AUTO Mode Failure occurs:
1.
2.

If automatic control is not regained:

  1. Manually slew stabilator - Adjust to 0 degrees for flight above 40 KIAS or full down when airspeed is below 40 KIAS. The preferred method of manually skewing the stabilator up is to use the cyclic mounted stabilator slew up switch.
  2. LAND AS SOON AS PRACTICABLE

If manual control is not possible, the airspeed limit indicator 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.
  2. LAND AS SOON AS PRACTICABLE.
A
  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.
42
Q

UNCOMMANDED NOSE DOWN PITCH ATTITUDE CHANGE

If an uncommanded nose down pitch attitude occurs:
1.
2.
3.
4. MAN SLEW switch - Adjust to 0 degrees at airspeeds above 40 KIAS and full down at airspeeds below 40 KIAS.
5. LAND AS SOON AS PRACTICABLE.

A
  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.
43
Q

DUAL EGI FAILURE

1.

  1. EGI switches - OFF, then ON. If successful, an EGI in-flight alignment will automatically be done.
  2. LAND AS SOON AS PRACTICABLE.
A
  1. Transition to ESIS display.
44
Q

FLT DIR FAIL, FD COUPLE FAIL Cautions Appear

1.

  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. Re engage affected mode when able.
  4. Fly affected axis manually if not restored.
A
  1. Check FD/DCP to verify which flight director modes are functioning.

UH 60M (2 decks)

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