Chp9

Question 1

LAND WITHOUT DELAY

Answer 1

A landing in which the primary consideration is continued control of the aircraft and survival of the occupants. It is meant to be more urgent than Land As Soon As Possible. The situation may not permit the aircrew to continue to maneuver the aircraft to a suitable landing area (e.g. open field).

Question 2

LAND AS SOON AS POSSIBLE

Answer 2

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

Question 3

LAND AS SOON AS PRACTICABLE

Answer 3

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

Question 4

AUTOROTATE

Answer 4

Adjusting the flight controls a necessary to establish an autorotational descent and landing.

Question 5

EMERGENCY SHUTDOWN

Answer 5

1. POWER LEVERS - OFF
2. APU - OFF (if applicable)
3. ROTOR BRAKE SWITCH - BRK
4. MSTR IGN - OFF once rotors have stopped

Question 6

EMERGENCY EXIT AND ENTRANCE - CANOPY JETTISON

Answer 6

1. HELMET VISORS - DOWN
2. AREA AROUND HELICOPTER - CLEAR OF PERSONNEL
3. CANOPY JETTISON HANDLE - OPERATE (see caution 2)

If Flares are ignited and lodged in the dispenser, jettison all flare munitions and LAND AS SOON AS POSSIBLE

Question 7

DUAL ENGINE FAILURE - LOW ALTITUDE / LOW AIRSPEED AND CRUISE

Answer 7

1. AUTOROTATE
2. CHOP BUTTON - RESET

Question 8

ABORT START PROCEDURES

Answer 8

1. POWER LEVER - OFF
2. ENG START SWITCH - IGN ORIDE

Question 9

SINGLE ENGINE FAILURE - LOW ALTITUDE / LOW AIRSPEED AND CRUISE

Answer 9

1. ACHIEVE SAFE SINGLE ENGINE FLIGHT CONDITIONS OR LAND

Question 10

ENGINE 1 or 2 OVERSPEED - Np FAILED HIGH

Answer 10

1. COLLECTIVE - ADJUST

Question 11

Np FAILED LOW - LOW ROTOR RPM

Answer 11

1. COLLECTIVE - ADJUST

Question 12

ENGINE COMPRESSOR STALL

Answer 12

1. COLLECTIVE - REDUCE

Question 13

MAIN TRANSMISSION TAIL ROTOR BEVEL-IDLER GEAR SET FAILURE

Answer 13

1. EMERG HYD BUTTON - PRESS ON
2. COLLECTIVE REDUCE - COMPROMISE BETWEEN RATE OF TURN AND RATE OF DESCENT
3. POWER LEVERS - OFF (10-20 FEET ABOVE TOUCHDOWN)
4. COLLECTIVE - INCREASE TO CUSHION TOUCHDOWN

LAND WITHOUT DELAY

Question 14

LOSS OF TAIL ROTOR THRUST IN CRUISE FLIGHT - CONTINUED FLIGHT POSSIBLE

Answer 14

1. AIRSPEED - 100 KTAS MINIMUM (UNTIL 10-20 FEET ABOVE TOUCHDOWN)

Question 15

LOSS OF TAIL ROTOR THRUST IN CRUISE FLIGHT - CONTINUED FLIGHT NOT POSSIBLE

Answer 15

1. COLLECTIVE - REDUCE (COMPROMISE BETWEEN RATE OF TURN AND RATE OF DESCENT)
2. POWER LEVERS - OFF (5-10 FEET ABOVE TOUCHDOWN)
3. COLLECTIVE - INCREASE TO CUSHION TOUCHDOWN

Question 16

TAIL ROTOR FIXED PITCH - LOW AIRSPEED OR HOVER

Answer 16

1. COLLECTIVE - ADJUST TO MINIMIZE YAW RATE
2. CYCLIC - MINIMIZE DRIFT
3. BREAK INTO BUCS

Question 17

TAIL ROTOR FIXED PITCH - FORWARD FLIGHT

Answer 17

1. COLLECTIVE - ADJUST TO MINIMIZE YAW RATE
2. CYCLIC - OPPOSE YAW
3. BREAK INTO BUCS

Question 18

MAIN TRANSMISSION INPUT DRIVE CLUTCH FAILURE - IN FLIGHT

Answer 18

1. ACHIEVE SAFE SINGLE ENGINE FLIGHT CONDITIONS OR LAND

Question 19

ENGINE 1 OR ENGINE 2 FIRE - IN FLIGHT

Answer 19

1. ACHIEVE SAFE SINGLE ENGINE FLIGHT CONDITIONS OR LAND
2. ILLUMINATED ENG FIRE BUTTON - PRESS AND RDY LIGHT ILLUMINATES
3. FIRE DISCH BUTTON(S) - PRESS

Question 20

ENGINE 1 OR ENGINE 2 FIRE - ON GROUND

Answer 20

1. POWER LEVERS - OFF
2. ILLUMINATED ENG FIRE BUTTON - PRESS AND RDY LIGHT ILLUMINATES
3. FIRE DISCH BUTTON(S) - PRESS

Question 21

APU FIRE - ON GROUND

Answer 21

1. APU - OFF
2. ILLUMINATED APU FIRE BUTTON - PRESS
3. FIRE DISCH BUTTON(S) - PRESS

Question 22

APU FIRE - IN FLIGHT

Answer 22

1. ILLUMINATED APU FIRE BUTTON - PRESS
2. FIRE DISCH BUTTON(S) - PRESS

Question 23

HYDRAULIC FAILURE - PRIMARY & UTILITY HYDRAULIC PSI LOW

Answer 23

1. EMERG HYD BUTTON - PRESS ON
LAND WITHOUT DELAY

Question 24

EMERGENCY LANDING IN WOODED AREA (POWER OFF)

Answer 24

1. AUTOROTATE

Question 25

DITCHING (POWER OFF)

Answer 25

1. AUTOROTATE
2. CANOPY - JETTISON PRIOR TO ENTERING WATER
3. CYCLIC - POSITION IN DIRECTION OF ROLL
4. EXIT WHEN ROTOR HAS STOPPED

Question 26

BUCS FAIL

Answer 26

1. TRANSFER FLIGHT CONTROLS TO REAR CREW STATION

Question 27

FLIGHT CONTROL MALFUNCTION - STABILIZATION EQUIPMENT/FORCE TRIM

Answer 27

1. FMC RELEASE BUTTON - PRESS

Question 28

NVS FAILURE

Answer 28

1. EXIT THE NOE ENVIRONMENT
2. PILOT ON THE CONTROLS, NVS SELECT SWITCH - SELECT ALTERNATE SENSOR (PNVS OR TADS)

Question 29

IHADSS/HDU FAILURE OR IHADSS STALE

Answer 29

1. EXIT THE NOE ENVIRONMENT

Question 30

SINGLE MP OPERATION

Answer 30

1. NVS SELECT SWITCH - RESELECT (PNVS OR TADS)
2. CREWMEMBER (NOT ON CONTROLS) - ASSUME CONTROL

Question 31

DUAL MP FAILURE - MP1 AND MP2 FAIL

Answer 31

1. EXIT THE NOE ENVIRONMENT

Question 32

CAUTION: BOTH ENG 1 FUEL PSI LOW AND ENG 2 FUEL PSI LOW

Answer 32

1. FUEL PAGE, BOOST BUTTON - PRESS ON
LAND AS SOON AS POSSIBLE