EPs

Question 1

FLIGHT CONTROL/ROTOR SYSTEM VIBRATIONS OR MALFUNCTIONS (FLIGHT)

Urgency to land:
1. ____

AFTER LANDING:
1. ____
2. ____
3. ____

Answer 1

Urgency to land:
1. Land as soon as possible

AFTER LANDING:
1. ENGINE POWER CONTROL LEVERS – OFF
2. ENGINE FUEL SYSTEM SELECTORS - OFF
3. FUEL BOOST PUMP SWITCHES - OFF

Question 2

FLIGHT CONTROL/ROTOR SYSTEM VIBRATIONS OR MALFUNCTIONS (GROUND)

Immediate actions:
1. ____
2. ____
3. ____

Answer 2

1. ENGINE POWER CONTROL LEVERS – OFF
2. ENGINE FUEL SYSTEM SELECTORS - OFF
3. FUEL BOOST PUMP SWITCHES - OFF

Question 3

Stabilator uncommanded nose down pitch attitude change

Immediate actions
1.____

Answer 3

1. Cyclic mounted stabilator slew-up switch – adjust (as required to arrest nose down pitch rate)

Question 4

Loss of tail rotor control

Immediate actions

If during Cruise flight a right yaw becomes uncontrollable:
1.___
2.____

If at low airspeed or hover a right yaw becomes uncontrollable:
3.___
4.____

If an uncontrolled left yaw develops during low airspeed or hover:
5.___
6.____
7.____
8.____

Answer 4

1. Auto rotate - maintain airspeed at or above 80kias
2. Engine power control levers – off (during deceleration when intended point of landing is assured)
3. Collective- reduce
4. Engine power control levers – off (5 to 10 ft above touchdown)
5. Engine power control levers - retard
6. Collective – increase ( NR Will decrease)
7. Engine power control levers – off (5 to 10 ft above touchdown)
8. Collective - adjust for landing

Question 5

DEC/EDECU low side failure

If an engine control unit fails to the low side and the other engine is unable to provide sufficient torque NR will decrease.

Immediate actions:

If NR continues to decrease and single engine flight is not possible:
1._____

Urgency to land
1._____

Answer 5

1. Engine power cont lever (low Q/TGT engine) – LOCKOUT (maintain Q approximately 10% below other engine)

Urgency to land
1. Land as soon as practicable

Question 6

STABILATOR MALFUNCTION – AUTO MODE FAILURE

Immediate actions:
1.____

Answer 6

1. Cyclic mounted stabilator slew-up switch – adjust

Question 7

Land as soon as possible

Answer 7

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

Question 8

Lightning strike

Immediate actions
1._____

Urgency to land
1.____

Answer 8

1. Eng power control levers - adjust (as required to control NP/NR)

Urgency to land
1. Land as soon as possible

Question 9

HYD PUMP 1 FAIL WITHOUT BACK-UP PUMP ON ADVISORY

Immediate actions:
1.____

Answer 9

1. Backup hydraulic pump switch – ON

Question 10

Emergency engine shutdown

Answer 10

Engine shutdown without delay. Engine shutdown in flight is usually not an immediate action item unless a fire exists

Question 11

Auto rotate

Answer 11

Adjusting the flight controls as necessary to establish an auto rotational descent and landing

Question 12

T/R SERVO 1 FAIL with no BACK UP PUMP ON advisory or T/R SERVO 2 ON advisory does not appear

Immediate actions
1. ___

Answer 12

T/R servo switch – backup

Question 13

Fires: APU/electrical/engine

Engine fire in flight

Immediate actions (if ENG EMER OFF handle/APU fire T-handle illuminates in flight):
1. ___
2. ___
3. ___
4. ___

If an electrical fire is present:
1. ___

Urgency to land
1. ____

Answer 13

1. Establish airspeed 80 KIAS or below
2. Engine power cont lever - OFF
3. ENG EMER OFF handle /APU fire T-handle - PULL (AS APPROPRIATE)
4. Fire extinguisher switch - main/reserve (as required)

If an electrical fire is present:
1. Battery and generator switches – off

Urgency to land
1. Land as soon as possible

Question 14

Dual engine failure

Immediate actions
1. ___

Answer 14

1. Autorotate

Question 15

The term Lockout Is defined as ____

Answer 15

Manual control of engine RPM while bypassing DEC/EDECU functions

Question 16

Land as soon as practical

Answer 16

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

Question 17

LOCKOUT EP:

1. _____

Answer 17

1. ENG POWER CONT lever - pull down and advance full forward while maintaining downward pressure, then adjust to set NR as required

Question 18

Single engine failure

Immediate actions:
1.___
2.___

Answer 18

1. Achieve safe single engine emergency AirSpeed (if possible)
2. External cargo/stores - jettison (if required)

Question 19

COUPLED FLIGHT DIRECTOR MALFUNCTION

Any uncommanded changes in pitch roll and yaw other than those observed in normal flight conditions while coupled to the flight director

Immediate actions
1. ____

If coupled FD does not disengage
2.____

If coupled FD does not disengage
3.____

After FD is uncoupled
4.____

Answer 19

Immediate actions
1. Remote standby switch - press to disengage FD modes

If coupled FD does not disengage:
2. Coupled switch- press to uncouple FD

If coupled FD does not disengage:
3. FPS and trim switches – off

After FD is uncoupled:
4. FPS and trim switches - on

Question 20

Hydraulic pump 1 fail and hydraulic pump 2 fail

Answer 20

Land as soon as possible (restrict control movements to moderate rate)

Question 21

Fuel 1 Press Low and Fuel 2 Press Low

Urgency to Land:
____

AFTER LANDING:
1. ENGINE POWER CONTROL LEVERS – OFF
2. ENGINE FUEL SYSTEM SELECTORS - OFF
3. FUEL BOOST PUMP SWITCHES - OFF

Answer 21

Urgency to Land:
Land as soon as possible