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UH-60A+ > Chapter 9 > Flashcards

Chapter 9 Flashcards

1
Q

SINGLE ENGINE FAILURE

1.

2.

If continued flight is not possible:

3.

A
  1. ESTABLISH SINGLE-ENGINE AIRSPEED
  2. EXTERNAL CARGO/STORES - JETTISON (IF REQUIRED)

If continued flight is not possible:

  1. LAND AS SOON AS POSSIBLE
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2
Q

DUAL ENGINE FAILURE

1.

A
  1. AUTOROTATE
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3
Q

EDECU LOW SIDE FAILURE

If partial powered flight cannot be maintained:

2.

A
  1. ESTABLISH SINGLE-ENGINE AIRSPEED

If partial powered flight cannot be maintained:

  1. ENG POWER CONT LEVER (LOW % TRQ/TGT TEMP ENGINE) - LOCKOUT. MAINTAIN % TRQ APPROXIMATELY 10% BELOW OTHER ENGINE
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4
Q

EDECU HIGH SIDE FAILURE

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:

4.

A
  1. ESTABLISH SINGLE-ENGINE AIRSPEED
  2. ENG POWER CONT LEVER (HIGH % TRQ/TGT TEMP ENGINE) - RETARD. MAINTAIN % TRQ APPROXIMATELY 10% BELOW OTHER ENGINE

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:

  1. PERFORM EMER ENG SHUTDOWN (AFFECTED ENGINE)
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5
Q

% RPM INCREASING/DECREASING (OSCILLATION)

1.

A
  1. ESTABLISH SINGLE-ENGINE AIRSPEED
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6
Q

% TRQ SPLIT BETWEEN ENGINES 1 AND 2

1.

A
  1. ESTABLISH SINGLE-ENGINE AIRSPEED
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7
Q

ENGINE COMPRESSOR STALL

1.

If condition persists:

If stall condition recurs:

4.

A
  1. ESTABLISH SINGLE-ENGINE AIRSPEED

If condition persists:

  1. ENG POWER CONT LEVER (AFFECTED ENGINE) - RETARD (TGT TEMP SHOULD DECREASE)

If stall condition recurs:

  1. EMER ENG SHUTDOWN (AFFECTED ENGINE)
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8
Q

1 OR #2 OIL FLTER BYPASS CAUTION APPEARS

1.

A
  1. ESTABLISH SINGLE-ENGINE AIRSPEED
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9
Q

CHIP #1 OR #2 ENGINE, #1 OR #2 ENGINE OIL PRESS, #1 OR #2 ENGINE OIL TEMP CAUTION APPEARS

A
  1. ESTABLISH SINGLE-ENGINE AIRSPEED
  2. 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)
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10
Q

ENGINE HIGH-SPEED SHAFT FAILURE

2.

A
  1. ESTABLISH SINGLE-ENGINE AIRSPEED

2. EMER ENG SHUTDOWN (AFFECTED ENGINE). DON NOT ATTEMPT TO RESTART.

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11
Q

LIGHTNING STRIKE

1.

3.

A
  1. ESTABLISH SINGLE-ENGINE AIRSPEED
  2. ENG POWER CONT LEVERS - ADJUST AS REQUIRED TO CONTROL % RPM
  3. LAND AS SOON AS POSSIBLE
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12
Q

LOSS OF TAIL ROTOR THRUST IN CRUISE FLIGHT

1.

2.

A
  1. AUTOROTATE - MAINTAIN AIRSPEED AT OR ABOVE 80 KIAS

2. ENG POWER CONT LEVERS - OFF (DURING DECELERATION WHEN INTENDED POINT OF LAND IS ASSURED

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13
Q

LOSS OF TAIL ROTOR THRUST OR TAIL ROTOR QUADRANT CAUTION APPEARS WITH LOSS OF CONTROL AT LOW AIRSPEED/HOVER (RIGHT ROTATION)

2.

A
  1. COLLECTIVE REDUCE

2. ENG POWER CONT LEVERS - OFF (5 TO 10 FEET ABOVE TOUCHDOWN)

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14
Q

TAIL ROTOR QUADRANT CAUTION APPEARS IN CRUISE FLIGHT

1.

A
  1. COLLECTIVE - ADJUST TO DETERMINE CONTROLLABILITY (FIXED RIGHT OR LEFT)
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15
Q

LOSS OF CONTROL AT LOW AIRSPEED/HOVER OR TAIL ROTOR QUADRANT CAUTION APPEARS (LEFT ROTATION)

2.

3.

4.

A
  1. ENG POWER CONT LEVER(S) - RETARD TO DECREASE % RPM R BELOW 100% AND BEGIN A PARTIAL POWER DECENT
  2. COLLECTIVE - ADJUST TO PRESERVE % RPM R
  3. ENG POWER CONT LEVERS - OFF (5 TO 10 FEET ABOVE TOUCHDOWN)
  4. COLLECTIVE - ADJUST FOR LANDING
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16
Q

PEDAL BIND/RESTRICTION OR DRIVE WITH NO ACCOMPANYING CAUTION

1.

A
  1. APPLY PEDAL FORCE TO OPPOSE THE DRIVE
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17
Q

1 TAIL RTR SERVO CAUTION AND BACK-UP ON ADVISORY DOES NOT APPEAR OR # 2 TAIL RTR SERVO ON ADVISORY DOES NOT APPEAR

1.

2.

A
  1. TAIL SERVO SWITCH - BACKUP

2. BACK-UP HYD PUMP SWITCH - ON

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18
Q

MAIN XMSN OIL PRESS OR MAKN XMSN OIL TEMP CAUTION / XMSN OIL PRESS LOW / XMSN OIL TEMP HIGH

If time permits:

3.

A

If time permits:

  1. EMER APU START
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19
Q

CHIP INPUT MDL LH KR RH CAUTION

1.

2.

3.

A
  1. ESTABLISH SINGLE-ENGINE AIRSPEED
  2. ENG POWER CONT LEVER (AFFECTED ENGINE) - IDLE
  3. LAND AS SOON AS POSSIBLE
20
Q

CHIP MAIN MDL SUMP, CHIP ACCESS MDL LH OR RH, CHIP TAIL XMSN OR CHIP INT XMSN / TAIL XMSN OIL TEMP OR INT XMSN OIL TEMP CAUTION

1.

A
  1. LAND AS SOON AS POSSIBLE
21
Q

MAIN TRANSMISSION FAILURE

2.

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
22
Q

ENGINE FIRE IN FIGHT

1.

2.

3.

4.

5.

A
  1. ESTABLISH SINGLE-ENGINE AIRSPEED
  2. ENG POWER CONT LEVER - OFF (AFFECTED ENGINE)
  3. ENG EMER OFF HANDLE - PULL
  4. FIRE EXTINGUISHER SWITCH - MAIN/RESERVE
  5. LAND AS SOON AS POSSIBLE
23
Q

ENGINE/FUSELAGE FIRE ON GROUND

1.

2.

3.

A
  1. ENG POWER CONT LEVER(S) - OFF
  2. ENG EMER OFF HANDLE(S) - PULL IF APPLICABLE
  3. FIRE EXTGH SWITCH - MAIN/RESERVE AS REQUIRED
24
Q

APU COMPARTMENT FIRE

1.

2.

A
  1. APU FIRE T-HANDLE - PULL

2. FIRE EXTGH SWITCH - MAIN/RESERVE AS REQUIRED

25
Q

ELECTRICAL FIRE IN FLIGHT

1.

2.

A
  1. BATT AND GENERATORS SWITCHES - OFF

2. LAND AS SOON AS POSSIBLE

26
Q

1 AND FUEL FLTR BYPASS CAUTION

1.

A
  1. LAND AS SOON AS POSSIBLE
27
Q

1 AND #2 FUEL LOW CAUTION

1.

A
  1. LAND AS SOON AS PRACTICABLE
28
Q

1 OR #2 FUEL PRESS CAUTION

1.

2.

3.

4.

A
  1. ENG FUEL SYS SELECTOR ON AFFECTED ENGINE - XFD
  2. FUEL BOOST PUMP CONTROL SWITCH ON SIDE BEING USED - ON
  3. LAND AS SOON AS POSSIBLE
  4. EMER ENG SHUTDOWN AFTER LANDING
29
Q

1 AND #2 FUEL PRESS CAUTION

2.

A
  1. LAND AS SOON AS POSSIBLE

2. EMER ENG SHUTDOWN AFTER LANDING

30
Q

1 AND #2 GENERATOR FAILURE (#1 AND #2 CONV AND AC ESS BUS OFF CAUTION)

6.

A
  1. EMER APU START
31
Q

LFT OR RT PITOT HEAT AND MASTER CAUTION OR ARE FLASHING

If LFT or RT PITOT HEAT and MASTER cautions still appear:

4.

A

If LFT or RT PITOT HEAT and MASTER cautions still appear:

  1. LAND AS SOON AS POSSIBLE
32
Q

1 AND #2 HYD PUMP CAUTION AND BACK-UP PUMP ON ADVISORY DOES NOT APPEAR

2.

If BACK- UP PUMP advisory still does not appear:

4.

5.

A
  1. AIRSPEED - ADJUST TO A COMFORTABLE AIRSPEED
  2. BACK-UP HYD PUMP SWITCH - ON

If BACK- UP PUMP advisory still does not appear:

  1. FPS AND BOOST SWITCHES - OFF (FOR #2 HYD PUMP CAUTION)
  2. LAND AS SOON AS POSSIBLE
33
Q

1 OR #2 PRI SERVO PRESS CAUTION

3.

A
  1. SVO OFF SWITCHES - CHECK BOTH ARE 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 #1 HYD PUMP CAUTION WITH BACK-UP PUMP ON ADVISORY

If the BACK-UP RSVR LOW caution also appears:

2.

3.

A

If the BACK-UP RSVR LOW caution also appears:

  1. SVO OFF SWITCH - 1ST STG
  2. LAND AS SOON AS POSSIBLE
35
Q

2 RSVR LOW AND #2 HYD PUMP CAUTION WITH BACK-UP PUMP ON ADVISORY

If BACK-UP RSVR LOW caution also appears:

3.

4.

A

If BACK-UP RSVR LOW caution also appears:

  1. SVO OFF SWITCH - 2ND STG
  2. LAND AS SOON AS POSSIBLE
36
Q

COLLECTIVE BOOST SERVO HARDOVER/POWER PISTON FAILURE

1.

A
  1. BOOST SWITCH - OFF
37
Q

EMERGENCY LANDING IN WOODED AREAS - POWER OFF

1.

2.

A
  1. AUTOROTATE. DECELERATE HELICOPTER TO STOP ALL FORWARD SPEED AT TREETOP LEVEL.
  2. COLLECTIVE ADJUST TO MAXIMUM BEFORE MAIN ROTOR CONTACTS TREE BRANCHES
38
Q

DITCHING POWER - OFF

1.

A
  1. AUTOROTATE
39
Q

FLIGHT CONTROL/MION-ROTOR SYSTEM MALFUNCTIONS

If the main rotor system malfunctions:

1.

2.

A

If the main rotor system malfunctions:

  1. LAND AS SOON AS POSSIBLE
  2. EMERGENCY ENG(S) SHUTDOWN AFTER LANDING
40
Q

STABILATOR MALFUNCTION - AUTO MODE FAILURE

1.

2.

A
  1. CYCLIC MOUNTED STABILATOR SLEW-UP SWITCH - ADJUST AS REQUIRED TO ARREST OR PREVENT NOSE DOWN PITCH RATE
  2. AUTO CONTROL SWITCH - PRESS ON ONCE AFTER ESTABLISHING A COMFORTABLE AIRSPEED
41
Q

U COMMANDED NOSE DOWN/UP PITCH ATTITUDE CHANGE

If an uncommanded nose down pitch attitude occurs:

2.

If an uncommanded nose up pitch attitude occurs:

2.

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

If an uncommanded nose up pitch attitude occurs:

  1. CYCLIC - ADJUST AS REQUIRED
  2. COLLECTIVE - REDUCE AS REQUIRED
42
Q

LAND AS SOON AS POSSIBLE

A

Land at the nearest suitable landing area without delay

43
Q

AUTOROTATE

A

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

44
Q

ESTABLISH SINGLE ENGINE AIRSPEED

A

Maneuver the aircraft to an appropriate AIRSPEED that will allow for flight under partial power conditions to a suitable recovery area.

45
Q

LOCKOUT

A

Manual control of engine RPM while bypassing the DECU functions

46
Q

ENG POWER CONT

A

Pull down and advance forward while maintaining downward pressure, then adjust to set % RPM R as required.

UH-60A+ (4 decks)

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