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UH-60M > Chapter 9 (underlined) (Chg 8) > Flashcards

Chapter 9 (underlined) (Chg 8) Flashcards

1
Q

Land As Soon As Possible

A

The term LAND AS SOON AS POSSIBLE is defined as landing at the nearest suitable landing area (e.g., open field) without delay. (The primary consideration is to ensure the survival of occupants.)

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2
Q

Land As Soon As Practicable

A

The term LAND AS SOON AS PRACTICABLE is defined as landing at a suitable landing area. (The primary consideration is the urgency of the emergency.)

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3
Q

Autorotate

A

The term AUTOROTATE is defined as adjusting the flight controls as necessary to establish an auto-rotational descent and landing.

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4
Q

Emergency Engine Shutdown

A

The term EMER ENG SHUTDOWN is defined as 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.

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5
Q

Lockout

A

The term LOCKOUT is defined as manual control of 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

Emergency APU Start

A

The term EMER APU START is defined as APU start to accomplish an emergency procedure.

1. FUEL PUMP switch - APU BOOST.

2. APU CONTR switch - ON.

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7
Q

Single Engine Failure

A

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

……….. is possible:

  1. ………..
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8
Q

Dual Engine Failure

A

AUTOROTATE

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9
Q

Decreasing NR

A

1. Collective - Adjust to control NR.

1.1. Establish a single-engine airspeed.

If single engine flight can not be achieved or maintained:

2. ENG POWER CONT lever (low % TRQ/TGT TEMP engine) - LOCKOUT

  1. ………
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10
Q

Increasing NR

A

1. ENG POWER CONT lever (high % TRQ/TGT TEMP engine) - Retard.

  1. …….. …….

ENG POWER CONT lever ….. FLY and IDLE… the HMU…… If this occurs:

3. Establish single engine airspeed.

  1. Perform EMER ENG SHUTDOWN (affected engine).
  2. ……
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11
Q

Engine Compressor Stall

A

1. Establish single engine airspeed

2. Collective - Reduce.

If conditions persists:

3. ENG POWER CONT lever (affected engine) - Retard

  1. …….

If stall condition recurs:

5. EMER ENG SHUTDOWN …(affected engine)…

  1. …….
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12
Q

Engine High-Speed Shaft Failure

A

1. Establish single engine airspeed.

2. Collective - Adjust.

3. EMER ENG SHUTDOWN …(affected engine).

  1. ……
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13
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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14
Q

Loss Of Tail Rotor Thrust In Flight

A

1. Airspeed - Adjust to 80 KIAS or above.

2. AUTOROTATATE - 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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15
Q

Loss Of Tail Rotor Thrust

or

Tail Rotor Quadrant 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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16
Q

Tail Rotor Quadrant Caution Appears In Cruise Flight

A

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

  1. ……
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17
Q

Loss Of Control

at

Low Airspeed/Hover

or

Tail Rotor Quadrant 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 (5-10 feet above touchdown).

4. Collective - Adjust for landing.

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18
Q

Pedal Bind/Restrictions

or

Drive With No Accompaying Caution

A

1. Apply pedal force to oppose the drive.

  1. ……
  2. ……

If…..

  1. ……
  2. ……

If…..

  1. ……
  2. ……
  3. ……
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19
Q

1 Tail RTR Servo appears

and

Back Up Pump On does not appear

or

A

1. TAIL SERVO switch - BACKUP

  1. ……
  2. ……
20
Q

Main XMSN Press (low)

or

Main XMSN Oil Temp (high)

A

1. LAND AS SOON AS POSSIBLE.

If time permits:

  1. ….. 80 ….

3. EMER APU START.

  1. ……
21
Q

Chip Input MDL - LH

or

Chip Input MDL - RH

A

1. Establish single engine airspeed.

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

3. LAND AS SOON AS POSSIBLE.

22
Q

Chip Main MDL Sump

or

Chip Access MDL LH or RH

or

Chip Tail XMSN

or

Chip INT XMSN/Tail XMSN Oil Temp

or

INT XMSN Oil Temp

A

LAND AS SOON AS POSSIBLE

23
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.

24
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

25
Q

APU Compartment Fire

A

1. APU fire T-handle - Pull.

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

3. LAND AS SOON AS POSSIBLE

26
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.

27
Q

Electrical Fire In-Flight

A

1. BATT and GENERATORS switches - OFF.

2. LAND AS SOON AS POSSIBLE.

28
Q

Fuel 1 Bypass

and

Fuel 2 Bypass

A

LAND AS SOON AS POSSIBLE

29
Q

1 Fuel Press Low

or

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.

………. is not critical:

  1. ……
  2. ……
  3. ……
30
Q

1 Fuel Press

and

A

1. LAND AS SOON AS POSSIBLE.

2. EMER ENG SHUTDOWN after landing.

31
Q

1 HYD Pump

and

A

LAND AS SOON AS POSSIBLE. ……restrict control……

32
Q

1 HYD Pump

or

and

Back Up Pump On does not appear

A

1. Airspeed - Adjust ……comfortable……

2. BACKUP HYD PUMP switch - ON.

If BACK-UP PUMP ON advisory appears:

  1. ……

If BACK-UP PUMP ON advisory still does not appear:

4. FPS and SAS/BOOST switches - Press off (switch lights off for HYD PUMP 2 fail caution).

5. LAND AS SOON AS POSSIBLE.

33
Q

1 PRI Servo Press

or

A

1. SVO OFF switch - Check centered.

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

3. LAND AS SOON AS POSSIBLE.

34
Q

1 RSVR Low

and

with

Back-Up Pump on

A
  1. ……

If the BACK-UP RSVR LOW caution also appears:

2. SVO OFF switch - 1ST STG.

3. LAND AS SOON AS POSSIBLE.

35
Q

2 RSVR Low

and

with

Back-Up Pump on

A
  1. ……
  2. ……

If the BACK-UP RSVR LOW caution also appears:

3. SVO OFF switch - 2ND STG.

4. LAND AS SOON AS POSSIBLE.

36
Q

Collective Boost Servo Hard Over

or

Power Piston Failure

A

1. SAS/BOOST switch - Off.

  1. ……
  2. ……
37
Q

Boost Servo Off Caution Appears

A

1. SAS/BOOST switch - Off.

  1. ……
  2. ……
38
Q

Emergency Landing In Wooded Areas - Power Off

A

1. AUTOROTATE. ……

2. Collective adjust ……

39
Q

Ditching - Power Off

A

1. AUTOROTATE.

  1. ……
  2. ……
  3. ……
  4. ……
40
Q

Flight Control

or

Main-Rotor System Malfunctions

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

A
  1. Cyclic mounted stabilator slew-up switch - Adjust if necessary ……
  2. AUTO CONTROL RESET switch - Press ON once after establishing a comfortable airspeed.

If automatic control is not regained:

  1. ……
  2. ……

If manual control is not possible:

  1. ……
  2. ……
42
Q

Uncommanded Nose Down Pitch Attitude Change

A

1. Cyclic - Adjust as required.

2. Collective - Maintain or increase.

3. Cyclic mounted stabilator slew-up switch - Adjust as required ……

  1. ……
  2. ……
43
Q

Uncommanded Nose Up Pitch Attitude Change

A

1. Cyclic - Adjust as required.

2. Collective - Reduce as required.

  1. ……
  2. ……
44
Q

STAB UNLOCKED Caution Appears

A

In flight - LAND AS SOON AS POSSIBLE

45
Q

Dual EGI Failure

A
  1. Transition to ESIS display
  2. ……
  3. ……
46
Q

FLT DIR FAIL

and

FD COUPLE FAIL Caution Appears

A
  1. Check FD/DCP to verify which flight director modes are functioning.
  2. ……
  3. ……
  4. ……
  5. ……

UH-60M (2 decks)

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