EP’s

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 the 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

Emergency Shutdown:

Answer 4

Power Levers - OFF
APU - OFF (if applicable)
Rotor Brake switch - BRK
MSTR IGN - OFF once rotors have stopped

Question 5

Emergency Exit and Entrance - Canopy Jettison

Answer 5

Helmet Visors - DOWN
Area around Helicopter - Clear of personnel
CANOPY JETTISON handle - operate (see caution 2)

Question 6

If flares are ignited and lodged in the dispenser, jettison all flare munitions and ________________________

Answer 6

Land as soon as possible

Question 7

Dual Engine Failure - Low Altitude/Low Airspeed and Cruise

Answer 7

1. AUTOROTATE - Rapidly lower collective to maintain N_R within limits.
2. CHOP Button - Reset if an ENGINE CHOP warning message is present.

Question 8

ABORT START PROCEDURE

Answer 8

1. POWER lever - OFF
2. ENG START switch - IGN ORIDE for 30 seconds and TGT is below 540C

Question 9

Single Engine Failure - Low Altitude/ Airspeed and Cruise

Answer 9

1. Achieve Safe Single Engine Flight Conditions or Land

Urgency to Land - LAND AS SOON AS PRACTICABLE

Question 10

Engine 1 or 2 Overspeed - N_P Failed High

Answer 10

1. Collective - Adjust to maintain N_R within limits

LAND AS SOON AS PRACTICABLE

Question 11

N_P Failed Low -Low RPM Rotor

Answer 11

1. Collective - Adjust to maintain N _R within limits

Urgency to Land - LAND AS SOON AS PRACTICABLE

Question 12

Engine Compressor Stall

Answer 12

1. Collective - Reduce

LAND AS SOON AS PRACTICABLE — Perform after Subsequent Actions

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 touch-down)

LAND AS SOON AS PRACTICABLE — Perform after Subsequent Actions

Question 15

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

Answer 15

1. COLLECTIVE - Reduce (compensate between rate of turn and rate of descent)
2. POWER LEVERS - OFF (5-10 ft 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
   ———-If pedals are jammed———-
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
   ————-If pedals are jammed————
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

If NP drops below NR - LAND AS SOON AS PRACTICABLE
If NP does not drop below NR - LAND AS SOON AS POSSIBLE

Question 19

ENGINE 1 OR ENGINE 2 FIRE - IN FLIGHT

Answer 19

1. Achieve safe single engine flight condition or land
2. ILLUMINATED ENG FIRE BUTTON - Press and RDY light illuminates
3. FIRE DISCH BUTTON(s) - Press

Urgency to Land - LAND AS SOON AS POSSIBLE

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 BUTTONS - Press

Question 21

APU FIRE - ON GROUND

Answer 21

1. APU - Off
2. ILLUMINATED APU FIRE BUTTON - Press and RDY light illuminates
3. FIRE DISCH BUTTONS - Press

Question 22

APU FIRE - IN FLIGHT

Answer 22

1. ILLUMINATED APU FIRE BUTTON - Press and RDY light illuminates
2. FIRE DISCH BUTTONS - Press

Urgency to Land - LAND AS SOON AS POSSIBLE

Question 23

HYDRAULIC FAILURE - PRIMARY & UTILITY HYDRAULIC PSI LOW

Answer 23

1. EMERG HYD button - Press ON

Urgency of the landing: LAND WITHOUT DELAY

Question 24

EMERGENCY LANDING IN WOODED AREAS
(POWER OFF)

Answer 24

1. AUTOROTATE - Apply full collective to decay Nr as helicopter settles

Question 25

DITCHING in water (POWER OFF)

Answer 25

1. AUTOROTATE - apply full collective to decay Nr as helicopter settles 2. CANOPY - JETTISON prior to entering water 3. CYCLIC - Position in the direction of roll 4. Exit when rotor has stopped

Question 26

BUCS FAIL

Answer 26

1. Transfer flight controls to rear crew station Urgency to Land - LAND AS SOON AS PRACTICABLE

Question 27

FLIGHT CONTROL MALFUNCTION - STABILIZATION EQPMNT/FORCE TRIM

Answer 27

1. FMC RELEASE BUTTON - Press If Uncommanded Inputs clear - LAND AS SOON AS PRACTICABLE If Uncommanded Inputs remain - LAND AS SOON AS POSSIBLE

Question 28

NVS FAILURE

Answer 28

1. Exit the NOE environment 2. Pilot on the controls, NVS SELECT SWTCH - Select alternate sensor (PNVS or TADS)

Question 29

IHADSS/HDU Failure or IHADSS STALE

Answer 29

At night (nvs flight) 1. Exit the NOE environment

Question 30

SINGLE MP OPERATION

Answer 30

1. NVS SELECT SWITCH - Reselect (PNVS or TADS) Or 2. Crewmember (not on controls) - Assume control

Question 31

DUAL MP FAILURE - MP1 AND MP 2 FAIL

Answer 31

At night under NVS flight 1. Exit the NOE environment Urgency to Land - LAND AS SOON AS POSSIBLE

Question 32

CAUTION: Both ENG 1 FUEL PSI LOW and ENG 2 FUEL PSI LOW

Answer 32

1. FUEL page, BOOST button - Press ON urgency of the landing: LAND AS SOON AS POSSIBLE

Question 33

The term AUTOROTATE is defined as:

Answer 33

The term AUTOROTATE is defined as: adjusting the flight controls as necessary to establish an autorotational descent and landing.