EPs

Question 1

Hydraulic pump 1 fail & hydraulic pump 2 fail

Answer 1

Land as soon as possible

Question 2

Flight control/rotor system vibrations or malfunctions on ground

Answer 2

Engine power control levers - OFF
Engine fuel system selectors - OFF
Fuel boost pump switches - OFF

Question 3

Single engine failure:
Eng1 or Eng2 out

Answer 3

• Achieve safe single engine airspeed
• External cargo/stores - jettison

Question 4

Tail rotor servo 1 fail with no backup pump on advisory or tail rotor servo 2 on advisory does not appear

Answer 4

Tail rotor servo switch - back up

Question 5

Hydraulic pump 1 fail without back up pump on advisory

Answer 5

Back up hydraulic pump switch - ON

Question 6

Flight control/rotor system vibrations or malfunctions in flight

Answer 6

Land as soon as possible

AFTER LANDING:
- ENG POWER CONT levers — OFF
- ENG FUEL SYS selectors — OFF
- FUEL BOOST PUMP switches — OFF

Question 7

Engine control malfunction DEC/EDECU low side failure

Answer 7

Engine power control lever (low torque, low TGT) - Lockout

Question 8

Dual engine failure
ENG1 & ENG2 OUT

Answer 8

Autorotate

Question 9

Main transmission failure

Answer 9

LAND AS SOON AS POSSIBLE: (KEEP POWER APPLIED TO THE MAIN TRANSMISSION DURING DESCENT AND LANDING)

Question 10

STABILATOR UNCOMMANDED NOSE DOWN PITCH ATTITUDE CHANGE

Answer 10

Cyclic mounted stabilator slew-up switch — Adjust

Question 11

Lightning strike

Answer 11

Engine power control levers - ADJUST
Land as soon as possible

Question 12

Loss of tail rotor control
If at low airspeed or hover a right yaw becomes uncontrollable:

Answer 12

• Collective — Reduce
• ENG POWER CONT levers — OFF (5 to 10 feet above touchdown)

Question 13

Loss of tail rotor control
If during cruise flight a right yaw becomes uncontrollable:)

Answer 13

• AUTOROTATE — Maintain airspeed at or above 80 KIAS
• ENG POWER CONT LEVERS — OFF (during deceleration when intended point of landing is assured)

Question 14

Loss of tail rotor control
If an uncontrolled left yaw develops during low airspeed or hover:

Answer 14

• ENG POWER CONT levers — Retard
• Collective — Increase (NR will decrease)
• ENG POWER CONT levers — OFF (5 to 10 feet above touchdown)
• Collective — Adjust for landing

Question 15

Fuel 1 pressure and fuel 2 pressure low

Answer 15

Land as soon as possible

Question 16

Fires: APU/electrical/or engine

Answer 16

• Airspeed adjust to 80 KIAS or less
• ENG POWER CONT lever — OFF
• ENG EMER OFF handle/APU fire T-handle — Pull (as appropriate)
• FIRE EXTGH switch — MAIN/RESERVE as required

If an electrical fire is present:
- BATT and GENERATORS switches — OFF

Question 17

COUPLED FLIGHT DIRECTOR MALFUNCTION

Answer 17

• RMT SBY switch — Press to disengage FD modes
  If coupled FD does not disengage:
• CPLD switch — Press the uncouple FD
  If coupled FD does not disengage:
• FPS and TRIM switches — OFF
  After FD is uncoupled:
• FPS and TRIM switches — ON

Question 18

Land as soon as possible

Answer 18

A landing at the nearest suitable landing area (e.g. open field). The primary consideration is to ensure the survival of occupants.

Question 19

Land as soon as practicable

Answer 19

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

Question 20

The term AUTOROTATE is defined as

Answer 20

adjusting the flight controls as necessary to establish an autoro-tational descent and landing.

Question 21

The term EMER ENG SHUTDOWN is defined as

Answer 21

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

Question 22

The term LOCKOUT is defined as

Answer 22

manual con-trol of engine RPM while bypassing DEC/EDECU func-tions. Bypass of the engine control will be required when NP1 or 2 decreases below normal demand speed due to a malfunction of the DEC/EDECU.

Question 23

Lockout EP

Answer 23

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