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UH-60 A/L 5/9 with guidance for test > CHAPTER 9 EMERGENCY PROCEDURES > Flashcards

CHAPTER 9 EMERGENCY PROCEDURES 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 DESCENT AND LANDING

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4
Q

The term EMER ENG SHUTDOWN is defined as ___

EP:

  1. _______________
  2. _______________
  3. _______________

If TGT is above 538°C after shutdown:

  1. _______________
  2. _______________
  3. _______________
A

The term EMER ENG SHUTDOWN is defined as ENGINE SHUTDOWN WITHOUT DELAY

EP:

  1. EPCL (S)- OFF
  2. ENG FUEL SYS SELECTOR (S)- OFF
  3. FUEL BOOST PUMP CONTROL SWITCH(ES)- OFF

If TGT is above 538°C after shutdown:

  1. AIR SOURCE HEAT/START SWITCH - AS REQUIRED
  2. ENGINE IGNITION SWITCH - OFF
  3. STARTER BUTTON - PRESS
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5
Q

The term LOCKOUT is defined as ________________

EP:

  1. ________________
A

The term LOCKOUT is defined as MANUAL CONTROL OF THE ENGINE RPM WHILE BYPASSING THE DEC FUNCTIONS

EP:

  1. EPCL- PULL DOWN AND ADVANCE FORWARD WHILE MAINTAINING DOWNWARD PRESSURE, THEN ADJUST TO SET % RPM R AS REQUIRED
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6
Q

The term EMER APU START is defined as ____________________________

EP:

  1. ___________________________
  2. __________________________
A

The term EMER APU START is defined as APU START TO ACCOMPLISH AN EMERGENCY PROCEDURE

EP:

  1. FUEL PUMP SWITCH - APU BOOST
  2. APU CONTROL SWITCH - ON
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7
Q

SINGLE ENGINE FAILURE

  1. _____________
  2. _____________
  3. _____________

If continued flight is not possible:

  1. _____________

If continued flight is possible:

  1. LAND AS SOON AS PRACTICABLE.
A
  1. COLLECTIVE - ADJUST TO MAINTAIN % RPM R
  2. EXTERNAL CARGO/STORES - JETTISON (IF REQUIRED)
  3. ESTABLISH SINGLE ENGINE AIRSPEED

If continued flight is not possible:

  1. LAND AS SOON AS POSSIBLE

If continued flight is possible:

  1. LAND AS SOON AS PRACTICABLE.
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8
Q

DUAL ENGINE FAILURE

____________________

A

AUTOROTATE

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9
Q

DECREASING % RPM R

  1. ____________
  2. ____________
  3. ____________
  4. LAND AS SOON AS PRACTICABLE.
A
  1. COLLECTIVE - ADJUST TO CONTROL % RPM R
  2. ESTABLISH SINGLE-ENG AIRSPEED
  3. EPCL (LOW % TRQ/TGT TEMP ENGINE) - LOCKOUT.
  4. LAND AS SOON AS PRACTICABLE.
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10
Q

INCREASING % RPM R

  1. ______________________\_
  2. 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:

  1. Establish single engine airspeed.
  2. Perform __________\_
  3. Refer to single-engine failure emergency procedure.
A
  1. EPCL (HIGH TRQ/TGT TEMP ENGINE) - RETARD.
  2. 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:

  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. __________________

If condition persists:

  1. __________________
  2. ENG POWER CONT lever (affected engine) - FLY.

If stall condition recurs:

  1. __________________
  2. __________________
  3. Refer to single-engine failure emergency procedure
A
  1. COLLECTIVE - REDUCE

If condition persists:

  1. EPCL (AFFECTED ENGINE) - RETARD
  2. ENG POWER CONT lever (affected engine) - FLY.

If stall condition recurs:

  1. ESTABLISH SINGLE-ENG AIRSPEED
  2. EMERGENCY ENG SHUTDOWN (AFFECTED ENGINE)
  3. Refer to single-engine failure emergency procedure
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12
Q

CHIP #1 ENG OR CHIP #2 ENG, #1 ENG OIL PRESS OR #2 ENG OIL PRESS, #1 ENG OIL TEMP OR #2 ENG OIL TEMP CAUTION APPEARS.

  1. __________________
  2. __________________ lever (affected engine) – Retard (to reduce torque)

If oil pressure is below minimum limits or if oil temp remains above maximum limits:

  1. ___________________
  2. Refer to single-engine failure emergency procedure.
A
  1. ESTABLISH SINGLE ENGINE AIRSPEED
  2. ♦​EPCL (AFFECTED ENGINE) - RETARD (to reduce torque)

If oil pressure is below minimum limits or if oil temp remains above maximum limits:

  1. EMER ENG SHUTDOWN (AFFECTED ENGINE)
  2. Refer to single-engine failure emergency procedure.
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13
Q

ENGINE HIGH-SPEED SHAFT FAILURE

  1. ___________________
  2. ___________________
  3. ___________________
  4. Refer to single-engine failure emergency procedure.
A
  1. COLLECTIVE - ADJUST
  2. ESTABLISH SINGLE ENGINE AIRSPEED
  3. EMER ENG SHUTDOWN (AFFECTED ENGINE)
  4. Refer to single-engine failure emergency procedure.
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14
Q

LIGHTNING STRIKE

  1. ___________________________
  2. ___________________________
A
  1. EPCLS - ADJUST AS REQUIRED TO CONTROL % RPM
  2. LAND AS SOON AS POSSIBLE
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15
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. EPCLS - OFF (DURING DECELERATION WHEN INTENDED POINT OF LANDING IS ASSURED
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16
Q

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

  1. _____________________
  2. _____________________
A
  1. COLLECTIVE - REDUCE
  2. EPCLS - OFF ( 5 - 10 FEET ABOVE TOUCHDOWN)
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17
Q

TAIL ROTOR QUADRANT 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.
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18
Q

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

  1. ___________________
  2. ___________________
  3. ___________________
  4. ___________________
A
  1. EPCL(S) - RETARD TO DECREASE % RPM R BELOW 100% & BEGIN A PARTIAL POWER DESCENT
  2. COLLECTIVE - ADJUST TO PRESERVE % RPM R
  3. ​EPCLS - OFF ( 5 - 10 FEET ABOVE TOUCHDOWN)
  4. COLLECTIVE ADJUST FOR LANDING
19
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:

  1. TAIL SERVO switch - NORMAL
  2. BOOST switch - OFF
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:

  1. TAIL SERVO switch - NORMAL
  2. BOOST switch - OFF
20
Q

1 TAIL RTR SERVO Caution Appears and BACK-UP PUMP ON Advisory Does not Appear or #2 TAIL RTR SERVO ON Advisory Does Not Appear.

  1. ___________________
  2. BACKUP HYD PUMP switch – ON.
  3. LAND AS SOON AS PRACTICABLE.
A
  1. TAIL SERVO SWITCH - BACKUP
  2. BACKUP HYD PUMP switch – ON.
  3. LAND AS SOON AS PRACTICABLE.
21
Q

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

  1. __________________

If time permits:

  1. Slow to _____ KIAS.
  2. __________________
  3. GENERATORS NO.1 and NO. 2 switches - OFF.
A
  1. LAND AS SOON AS POSSIBLE

If time permits:

  1. Slow to 80 KIAS.
  2. EMERGENCY APU START
  3. GENERATORS NO.1 and NO. 2 switches - OFF.
22
Q

CHIP INPUT MDL LH OR RH CAUTION APPEARS

  1. ____________________________
  2. ____________________________
  3. ____________________________
A
  1. ESTABLISH SINGLE ENGINE AIRSPEED
  2. EPCL (AFFECTED ENGINE) - IDLE
  3. LAND AS SOON AS POSSIBLE
23
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 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 THROUGHOUT THE DESCENT AND LANDING
  2. LAND AS SOON AS POSSIBLE
25
Q

ENGINE/FUSELAGE FIRE ON GROUND

  1. _______________________
  2. _______________________
  3. _______________________
  4. _______________________
A
  1. EPCLS - OFF
  2. ENG EMER OFF HANDLE - PULL IF APPLICABLE
  3. FIRE EXTGH SWITCH - MAIN / RESERVE AS REQUIRED
  4. EMER ENG SHUTDOWN - PERFORM (OTHER ENG)
26
Q

APU COMPARTMENT FIRE

  1. ________________________
  2. ________________________
A
  1. APU FIRE T - HANDLE - PULL
  2. FIRE EXTGH SWITCH - MAIN / RESERVE AS REQUIRED
27
Q

ENGINE FIRE IN FLIGHT

  1. ______________________
  2. ______________________
  3. ______________________
  4. ______________________
  5. ______________________
A
  1. ESTABLISH SINGLE ENGINE AIRSPEED
  2. EPCL (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

1 AND #2 FUEL FLTR BYPASS CAUTIONS APPEAR

_____________________________

A

LAND AS SOON AS POSSIBLE

30
Q

1 OR #2 FUEL PRESS CAUTIONS APPEAR

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 CONTROL SWITCHES - NO. 1 PUMP OR NO. 2 PUMP - ON (AS APPLICABLE)
  3. LAND AS SOON AS POSSIBLE
  4. EMER ENG SHUTDOWN AFTER LANDING
31
Q

1 AND #2 FUEL PRESS CAUTIONS APPEAR

  1. ____________________
  2. ____________________
A
  1. LAND AS SOON AS POSSIBLE
  2. EMER ENG SHUTDOWN AFTER LANDING
32
Q

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

  1. SAS 1 switch - Press off
  2. Airspeed - Adjust (80 KIAS or less)
  3. GENERATORS NO. 1 and NO. 2 switches - RESET; then ON

If cautions still appear:

  1. GENERATORS NO. 1 and NO. 2 switches - OFF
  2. If MCUs are in use: BCA MCU control knobs (pilot, copilot, and crewmembers) - OFF
  3. ___________________
  4. SAS 1 switch – ON
  5. LAND AS SOON AS PRACTICABLE
A
  1. SAS 1 switch - Press off
  2. Airspeed - Adjust (80 KIAS or less)
  3. GENERATORS NO. 1 and NO. 2 switches - RESET; then ON

If cautions still appear:

  1. GENERATORS NO. 1 and NO. 2 switches - OFF
  2. If MCUs are in use: BCA MCU control knobs (pilot, copilot, and crewmembers) - OFF

6. EMER APU START

  1. SAS 1 switch – ON
  2. LAND AS SOON AS PRACTICABLE
33
Q

1 AND #2 HYD PUMP CAUTIONS APPEAR

____________\_ Restrict control movement to moderate rates.

A

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

34
Q

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

  1. ___________________
  2. ___________________

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

  1. ___________________
  2. ___________________
A
  1. AIRSPEED - ADJUST
  2. BACKUP HYD PUMP SWITCH - ON

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

  1. FPS AND BOOST SWITCHES - OFF ( FOR #2 HYD PUMP CAUTION )
  2. LAND AS SOON AS POSSIBLE
35
Q

1 OR #2 PRI SERVO PRESS CAUTIONS APPEAR

  1. ______________
  2. ______________
  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
36
Q

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

  1. LAND AS SOON AS PRACTICABLE.

If the BACK-UP RSVR LOW caution also appears:

  1. ______________\_
  2. _______________
A
  1. LAND AS SOON AS PRACTICABLE.

If the BACK-UP RSVR LOW caution also appears:

  1. SVO OFF SWITCH - 1ST STAGE
  2. LAND AS SOON AS POSSIBLE
37
Q

2 RSVR LOW AND #2 HYD PUMP CAUTIONS APPEAR WITH BACK-UP PUMP ON ADVISORY APPEARING

  1. POWER ON RESET switches-Simultaneously press; then release.
  2. LAND AS SOON AS PRACTICABLE.

If the BACK-UP RSVR LOW caution also appears:

  1. ___________________
  2. ___________________
A
  1. POWER ON RESET switches-Simultaneously press; then release.
  2. LAND AS SOON AS PRACTICABLE.

If the BACK-UP RSVR LOW caution also appears:

  1. SVO OFF SWITCH - 2ND STG
  2. LAND AS SOON AS POSSIBLE
38
Q

COLLECTIVE BOOST SERVO HARDOVER / POWER PISTON FAILURE

  1. ______________________
  2. LAND AS SOON AS PRACTICABLE.
A
  1. BOOST SWITCH - OFF
  2. LAND AS SOON AS PRACTICABLE.
39
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
40
Q

DITCHING (POWER OFF)

  1. _______________________
  2. Cockpit doors jettison and cabin doors open prior to entering water.
  3. Cyclic-Position in direction of roll.
  4. Exit when main rotor has stopped
A
  1. AUTOROTATE
  2. Cockpit doors jettison and cabin doors open prior to entering water.
  3. Cyclic-Position in direction of roll.
  4. Exit when main rotor has stopped
41
Q

FIGHT CONTROL / MAIN ROTOR SYSTEM MALFUNCTIONS

If the main rotor system malfunctions:

  1. ____________________
  2. ____________________
A
  1. LAND AS SOON AS POSSIBLE
  2. EMER ENG(S) SHUTDOWN AFTER LANDING
42
Q

STABILATOR MALFUNCTION – AUTO MODE FAILURE
If an AUTO Mode Failure occurs:

  1. ___________________
  2. ___________________

If automatic control in 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.
  2. LAND AS SOON AS PRACTICABLE.

If manual control is not possible:

  1. STAB POS indicator-Check and fly at or below KIAS LIMITS shown on placard.
  2. LAND AS SOON AS PRACTICABLE.
A

1. CYCLIC MOUNTED STABILATOR SLEW-UP SWITCH - ADJUST IF NECESSARY

2. AUTO CONTROL SWITCH - PRESS ON ONCE AFTER ESTABLISHING A COMFORTABLE AIRSPEED

If automatic control in 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.
  2. LAND AS SOON AS PRACTICABLE.

If manual control is not possible:

  1. STAB POS indicator-Check and fly at or below KIAS LIMITS shown on placard.
  2. LAND AS SOON AS PRACTICABLE.
43
Q

UNCOMMANDED NOSE DOWN / UP PITCH ATTITUDE CHANGE

If an un-commanded nose down pitch attitude occurs:

  1. ___________________
  2. ___________________
  3. ___________________
  4. MAN SLEW switch-Adjust to 0° at airspeeds above 40 KIAS and full down at airspeeds below 40 KIAS.
  5. LAND AS SOON AS PRACTICABLE.

If an un-commanded nose up pitch attitude occurs:

  1. ___________________
  2. ___________________
  3. MAN SLEW switch-Adjust to 0° at airspeeds above 40 KIAS and full down at airspeeds below 40 KIAS.
A

If an un-commanded 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
  4. MAN SLEW switch-Adjust to 0° at airspeeds above 40 KIAS and full down at airspeeds below 40 KIAS.
  5. LAND AS SOON AS PRACTICABLE.

If an un-commanded nose up pitch attitude occurs:

  1. CYCLIC - ADJUST AS REQUIRED
  2. COLLECTIVE - REDUCE AS REQUIRED
  3. MAN SLEW switch-Adjust to 0° at airspeeds above 40 KIAS and full down at airspeeds below 40 KIAS.

UH-60 A/L 5/9 with guidance for test (2 decks)

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