UH-60M - Emer. Proc. (ch. 9) - changes

Question 1

SINGLE ENGINE FAILURE

1. _______________________
2. _______________________
3. _______________________

If continued flight is not possible:
4. _______________________

If continued flight is possible:
​5. LAND AS SOON AS PRACTICABLE

Answer 1

1. Collective - Adjust to maintain NR
   (2. ) External cargo/stores - Jettison (if required).
2. Establish single-engine airspeed.

If continued flight is not possible:
4. LAND ASAP.

If continued flight is possible:
5. LAND AS SOON AS PRACTICABLE

Question 2

DECREASING % RPM R.

1. ______________________
2. 1. ______________________

If single engine flight cannot be achieved or maintained:

(2) . ______________________
3. LAND AS SOON AS PRACTICABLE

Answer 2

1. Collective - Adjust to control NR.
2. 1. Establish single-engine airspeed.

If single engine flight cannot be achieved or maintained:

(2.) EPCL (low Q/TGT TEMP engine) - LOCKOUT.
Maintain Q approximately 10% below other engine.
3. LAND AS SOON AS PRACTICABLE

Question 3

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:
3. Establish single engine airspeed.
(4). Perform _________________________\_
(5). Refer to single-engine failure emergency procedure.

Answer 3

(1). EPCL (high Q/TGT TEMP engine) - Retard.
Maintain Q approximately 10% below other engine.

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:

3. Establish single engine airspeed.
   (4) . Perform EMER ENG SHUTDOWN (affected engine).
   (5) . Refer to single-engine failure emergency procedure.

Question 4

ENGINE COMPRESSOR STALL

1. _________________________\_
2. _________________________\_
   If condition persists:
   (3). _________________________\_
   (4). ENG POWER CONT lever (affected engine) - FLY.
   If stall condition recurs:
   (5). _________________________\_
   ​(6). Refer to single-engine failure emergency procedure.

Answer 4

1. Establish single engine airspeed.
2. Collective - Reduce.
   If condition persists:
   (3). EPCL​ (affected engine) - Retard (TGT TEMP 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.

Question 5

ENGINE HIGH-SPEED SHAFT FAILURE

1. _____________________\_
   ​2. _____________________\_
2. _____________________\_
3. Refer to single-engine failure emergency procedure.

Answer 5

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.

Question 6

Loss of Tail Rotor Thrust in Cruise Flight

1. ____________________\_
2. ____________________\_
   (3) . ____________________\_

Answer 6

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).

Question 7

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

1. _________________\_
2. ​_________________\_

Answer 7

1. Collective - Reduce.
   (2. ) EPCLs - OFF (5 to 10 feet above touchdown).

Question 8

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

(1) . ______________\_
2. ______________\_
(3) . ______________\_
4. ______________\_

Answer 8

(1. ) EPCL(s) - Retard to decrease NR below 100% and begin a partial power descent.
2. Collective - Adjust to preserve NR.
(3. ) EPCLs - OFF (5 to 10 feet above touchdown).
4. Collective - Adjust for landing.

Question 9

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 - NORMAL.
(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.

Answer 9

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 - NORMAL.
(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.

Question 10

• *CHIP L INPUT MDL or CHIP R INPUT MDL** Caution Appears
  1. ______________
  2. ______________
  3. ______________

Answer 10

1. Establish single engine airspeed.
   (2. ) EPCL (affected engine) - IDLE.
2. LAND ASAP.

Question 11

ENGINE/FUSELAGE FIRE ON GROUND

1. ___________________
2. ___________________
3. ___________________
4. ___________________

Answer 11

(1. ) EPCLs - OFF.
(2. ) ENG EMER OFF T-handle - Pull if applicable.
(3. ) FIRE EXTGH switch - MAIN/RESERVE as required.
(4. ) Rotor Brake - As required.

Question 12

FLIGHT CONTROL / MAIN ROTOR SYSTEM MALFUNCTIONS

If the main rotor system malfunctions:

1. ________________
2. ________________
3. ________________

Answer 12

If the main rotor system malfunctions:

1. LAND ASAP.
   (2. ) EMER ENG(S) SHUTDOWN after landing.
   (3. ) Rotor Brake - As required.

WARNING - Danger exists that the main rotor system could collapse or separate from the aircraft after landing. Exit when main rotor has stopped.

Question 13

COLLECTIVE BOOST SERVO HARDOVER / POWER PISTON FAILURE

1. ________________
2. FPS switch - Off.
3. LAND AS SOON AS PRACTICABLE.

Answer 13

(1. ) SAS/BOOST switch - Off.
(2. ) FPS switch - Off.
3. LAND AS SOON AS PRACTICABLE.

Question 15

BOOST SERVO OFF Caution Appears

(1. ) _________________\_
(2) . FPS switch - Off.
3. LAND AS SOON AS PRACTICABLE.

Answer 15

(1. ) SAS/BOOST switch - Off.
(2) . FPS switch - Off.
3. LAND AS SOON AS PRACTICABLE.

Question 16

STAB UNLOCKED Caution Appears.

In flight -

Answer 16

In flight - LAND ASAP.

Question 17

INTEGRATED AVIONICS SYSTEM MALFUNCTIONS

The following component failures will result in — ___________________

a. Loss of two data concentrator units (DCU).
b. Loss of four MFDs.

Answer 17

INTEGRATED AVIONICS SYSTEM MALFUNCTIONS

The following component failures will result in — LAND AS SOON AS POSSIBLE

a. Loss of two data concentrator units (DCU).
b. Loss of four MFDs.

Question 18

DUAL EGI FAILURE

1. __________________\_
   (2. ) EGI switches — OFF, then ON. If successful, an EGI inflight alignment will automatically be done.
2. LAND AS SOON AS PRACTICABLE.

Answer 18

DUAL EGI FAILURE

1. Transition to ESIS display.
   (2. ) EGI switches — OFF, then ON. If successful, an EGI inflight alignment will automatically be done.
2. LAND AS SOON AS PRACTICABLE.

Question 19

FLT DIR FAIL, FD COUPLE FAIL Cautions Appear.

1. ______________________________________\_
   (2. ) FAILURE RESET CPTR 1 and/or CPTR 2 – Press to clear flight director cautions.
   (3. ) Check AFCS and FCC status page if necessary. Clear BITE codes if necessary.
   (4. ) Reengage affected mode when able.
2. Fly affected axis manually if not restored.

Answer 19

FLT DIR FAIL, FD COUPLE FAIL Cautions Appear.

1. Check FD/DCP to verify which flight director modes are functioning.
   (2. ) FAILURE RESET CPTR 1 and/or CPTR 2 – Press to clear flight director cautions.
   (3. ) Check AFCS and FCC status page if necessary. Clear BITE codes if necessary.
   (4. ) Reengage affected mode when able.
2. Fly affected axis manually if not restored.

Question 20

ENG 1 OIL BYPASS OR ENG 2 OIL BYPASS Caution

1. _______________________\_
   (2. ) ENG POWER CONT lever — Retard.
2. LAND AS SOON AS PRACTICABLE.

Answer 20

1. Establish single engine airspeed.
   (2. ) ENG POWER CONT lever — Retard.
2. LAND AS SOON AS PRACTICABLE.