Ch. 9 EPs

Question 1

The term LAND WITHOUT DELAY is defined as:

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

The term LAND AS SOON AS POSSIBLE is defined as:

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

The term AUTOROTATE is defined as:

Answer 3

adjusting the flight controls as necessary to establish an autorotational descent and landing.

Question 4

Emergency Shutdown:
1.
2.
3.
4.
(P.A.R.M.)

Answer 4

Emergency Shutdown:
1. POWER LEVERS – OFF
2. APU – OFF (if applicable)
3. ROTOR BRAKE switch – BRK
4. MSTR IGN – OFF once rotors have stopped

Question 5

EMERGENCY EXIT AND ENTRANCE – CANOPY JETTISON
1.
2.
3.
(H.A.C.)

Answer 5

EMERGENCY EXIT AND ENTRANCE – CANOPY JETTISON
1. Helmet visors – Down.
2. Area around helicopter – Clear of personnel.
3. 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

Dual Engine Failure- Low Altitude / Low Airspeed and Cruise
1. AUTOROTATE – Rapidly lower collective to maintain NR within limits
2. CHOP Button – Reset if an ENGINE CHOP warning message is present

Question 8

ABORT START PROCEDURES
1.
2.
(P.E.)

Answer 8

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

Question 9

Single Engine Failure- Low Altitude / Low Airspeed and Cruise
1.

Answer 9

Single Engine Failure- Low Altitude / Low Airspeed and Cruise
1. Achieve safe single engine flight conditions or land

Question 10

Engine 1 or 2 Overspeed – NP Failed High

Answer 10

Engine 1 or 2 Overspeed – NP Failed High
1. Collective – Adjust to maintain NR within limits
2. LAND AS SOON AS PRACTICABLE

Question 11

NP Failed Low – Low RPM Rotor
1.

Answer 11

NP Failed Low – Low RPM Rotor
1. Collective – Adjust to maintain NR within limits

Question 12

Engine Compressor Stall
1.

Answer 12

Engine Compressor Stall
1. Collective – Reduce

Question 13

MAIN TRANSMISSION TAIL ROTOR BEVEL-IDLER GEAR SET FAILURE
1.
2.
3.
4.
5.
(E.C.P.C.L.)

Answer 13

MAIN TRANSMISSION TAIL ROTOR BEVEL-IDLER GEAR SET FAILURE
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
5. LAND WITHOUT DELAY

Question 14

LOSS OF TAIL ROTOR THRUST IN CRUISE FLIGHT – CONTINUED FLIGHT POSSIBLE
1.

Answer 14

LOSS OF TAIL ROTOR THRUST IN CRUISE FLIGHT – CONTINUED FLIGHT POSSIBLE
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
1.
2.
3.
(C.P.C)

Answer 15

LOSS OF TAIL ROTOR THRUST IN CRUISE FLIGHT – CONTINUED FLIGHT NOT POSSIBLE
1. Collective – Reduce (compromise between rate of turn and rate or 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
1.
2.
3.
(C.C.B.)

Answer 16

TAIL ROTOR FIXED PITCH – LOW AIRSPEED OR HOVER
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
1.
2.
………
3.
(C.C.B)

Answer 17

TAIL ROTOR FIXED PITCH – FORWARD FLIGHT
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
1.

Answer 18

MAIN TRANSMISSION INPUT DRIVE CLUTCH FAILURE – IN FLIGHT
1. Achieve safe single engine flight conditions or land

Question 19

ENGINE 1 OR ENGINE 2 FIRE – IN FLIGHT
1.
2.
3.
(A.I.F)

Answer 19

ENGINE 1 OR ENGINE 2 FIRE – IN FLIGHT
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

APU FIRE – ON GROUND
1.
2.
3.
(A.I.F)

Answer 20

APU FIRE – ON GROUND
1. APU – OFF
2. Illuminated APU FIRE button – Press and RDY light illuminates
3. FIRE DISCH button(s) – Press

Question 21

APU FIRE – IN FLIGHT
1.
2.
(I.F.)

Answer 21

APU FIRE – IN FLIGHT
1. Illuminated APU FIRE button – Press and RDY light illuminates
2. FIRE DISCH button(s) – Press

Question 22

HYDRAULIC FAILURE – PRIMARY & UTILITY HYDRAULIC PSI LOW
1.
…..
2.
(E.L)

Answer 22

HYDRAULIC FAILURE – PRIMARY & UTILITY HYDRAULIC PSI LOW
1. EMERG HYD button – Press ON
…..Urgency to land….
2. LAND WITHOUT DELAY

Question 23

EMERGENCY LANDING IN WOODED AREA (POWER OFF)
1.

Answer 23

EMERGENCY LANDING IN WOODED AREA (POWER OFF)
1. AUTOROTATE – Apply full collective to decay rotor RPM as helicopter settles.

Question 24

DITCHING (POWER OFF)
1.
2.
3.
4.
(A.C.C.E)

Answer 24

DITCHING (POWER OFF)
1. AUTOROTATE (apply full collective to decay rotor RPM as helicopter settles)
2. Canopy – JETTISON prior to entering water.
3. Cyclic – Position in direction of roll
4. Exit when rotor has stopped.

Question 25

BUCS FAIL
1.

Answer 25

BUCS FAIL
1. Transfer flight controls to rear crew station

Question 26

FLIGHT CONTROL MALFUNCTION – STABILIZATION EQUPMENT/FORCE TRIM
1.

Answer 26

FLIGHT CONTROL MALFUNCTION – STABILIZATION EQUPMENT/FORCE TRIM
1. FMC release button – Press

Question 27

NVS Failure
1.
2.
(E.P.)

Answer 27

NVS Failure
1. Exit the NOE environment
2. Pilot on the controls, NVS Select Switch – Select alternate sensor (PNVS or TADS)

Question 28

IHADSS/HDU Failure or IHADSS STALE At night (NVS flight)
1.

Answer 28

IHADSS/HDU Failure or IHADSS STALE At night (NVS flight)
1. Exit the NOE environment

Question 29

Single MP Operation
1.
…….
2.

Answer 29

Single MP Operation
1. NVS SELECT Switch – Reselect (PNVS or TADS)
…..or…..
2. Crewmemeber (not on controls) – Assume control

Question 30

Dual MP Failure – MP1 AND MP2 FAIL at night (NVS flight)
1.

Answer 30

Dual MP Failure – MP1 AND MP2 FAIL at night (NVS flight)
1. Exit the NOE environment

Question 31

CAUTION: Both ENG 1 FUEL PSI LOW and ENG 2 FUEL PSI LOW
1.
2.
(F.L.)

Answer 31

CAUTION: Both ENG 1 FUEL PSI LOW and ENG 2 FUEL PSI LOW
1. FUEL page, BOOST button – Press ON
2. LAND AS SOON AS POSSIBLE