EP’s

Question 1

EMIF

Answer 1

1. Control Nr
2. C-pwr Switch- on
3. Single Engine Conditions- Establish
4. Eng Ani Ice switches- as required
5. External Cargo, Stores, Fuel- Jettison, dump as required

Question 2

Engine High Side Failure in Flight
All of the following conditions exist:
1. Torque is 10% or greater of other Engine
2. Ng is 5% or greater of other engine
3. Np is matched within 5% of other engine
4. Nr is at or above 103%

Answer 2

1. EMIF- perform
2. PCL (malfunctioning Engine)- Retard to set:
   Torque 10% Below the good Engine
   Matched Ng
   Matched TGT

Question 3

Engine High Side Failure on Deck

Answer 3

PCL malfunctioning engine - Idle

Question 4

Engine Low Side Failure
	All of the following conditions exist:
		1. Torque is 10% below good engine
		2. Ng is 5% or less of good engine
		3. Np is at or below 98%
		4. Nr is at or below 97%

Answer 4

EMIF- Perform

Question 5

Engine Torque or TGT Spiking/Fluctuations

Answer 5

If an engine instrument is spiking/fluctuating and inducing secondary indications in Ng, Np, and/or Nr:

*1. Engine Malfunction in Flight emergency procedure—Perform.

If fuel contamination is suspected:

*2. Land as soon as possible.

Question 6

Compressor Stall

Answer 6

• 1. Engine Malfunction in Flight emergency procedure—Perform.
• 2. PCL (malfunctioning engine)—IDLE.

Question 7

Engine High Speed Shaft Failure

Indicates failure of the high-speed shaft. Np is greater than Nr by more than 3% and engine torque is below 10%.

Answer 7

• 1. Engine Malfunction in Flight emergency procedure—Perform.
• 2. PCL (malfunctioning engine)—OFF.

Question 8

Abort Start

Abort engine start if any of the following limits are exceeded:

1. Ng does not reach14% within 6 seconds after starter initiation.
2. No oil pressure within 30 seconds after starter initiation (do not motor engine). 3. No light-off within 30 seconds after moving PCL to IDLE.
3. ENG STARTER advisory disappears before reaching 52% Ng.
4. TGT is likely to exceed 851°C before idle speed is attained.

Answer 8

To abort start:

• 1.PCL—OFF.
• 2. ENGINE IGNITION switch—OFF

If engine oil pressure is indicated:

*3. Starter—Engage.

Question 9

Engine Malfunction During Hover/Takeoff

Answer 9

• 1. Control Nr.
• 2. CONTGCY PWR switch—ON.

If a suitable landing site exists or unable to transition to forward flight:

*3. Set level attitude, eliminate drift, cushion landing.

If able to transition to forward flight:

*4. Engine Malfunction in Flight emergency procedure—Perform.

Question 10

Dual Engine Failure

Answer 10

• 1. Autorotation— Establish.
• 2.Immediate Landing/Ditching emergency procedure—Perform.

If time and altitude permit:

*3. Engine Air Restart emergency procedure— Perform.

Question 11

Single Engine failure in flight

Warning light is activated by the vertical instrument when Ng decreases below 55%. In the event of an isolated Ng signal failure, the ENG OUT light will be illuminated with the engine operating normally. TORQUE SPLIT Difference between engine torques is greater than 10%.

Answer 11

*1. Engine Malfunction in Flight emergency procedure—Perform.

Question 12

Engine Air Restart

Answer 12

• 1. APU Emergency Start procedure—As required.
• 2. Engine ignition switch—NORM.
• 3. Fuel selector lever—DIR or XFD.
• 4. PCL—OFF.
• 5. Starter—Engage, motor engine.
• 6. PCL—IDLE (TGT 80°C or less, if time permits).
• 7. PCL—Advance to FLY after starter dropout.

Question 13

APU Emergency Start Procedure

Answer 13

• 1. ECS—OFF.
• 2. AIR SOURCE ECS/START switch—APU.
• 3. FUEL PUMP switch—APU BOOST.
• 4. APU CTRL switch—ON.
• 5. APU GENERATOR switch—ON.

Question 14

Hung Droop Stops

Answer 14

*1. Reengage rotor to greater than 75% Nr.

Question 15

Low Rotor RPM

Answer 15

*1. Control Nr

Question 16

Main Transmission Malfunction

Answer 16

If failure is imminent:

*1. Land immediately.

If secondary indications are present
:
*2. Land as soon as possible.

Question 17

Tail/Intermediate Transmission Malfunction

Answer 17

If failure is imminent:

*1. Land immediately.

If failure is not imminent:

*2. Land as soon as possible.

Question 18

1/#2 Input Chip Caution

Answer 18

*1. Main Transmission Malfunction emergency procedure—Perform.

Question 19

Loss of Tail Rotor Drive Altitude and Airspeed Sufficient to Enter Autorotation

Answer 19

• 1. PAC call—“AUTO,AUTO,AUTO.”
• 2. Autorotation—Establish. Center tail rotor pedals.
• 3. Drive failure—Attempt to verify.
• 4. Immediate Landing/Ditching emergency procedure—Perform.
• 5. PCLs—OFF when directed (prior to the flare).

Question 20

Loss of Tail Rotor Drive Altitude and Airspeed not Sufficient to enter Autorotation

Answer 20

• 1. PAC call— “HOVER,HOVER,HOVER.”
• 2. Collective—Lower.
• 3. PNAC—Hands on PCLs.
• 4. PCLs—OFF when directed (approximately 20 to 30ft).

Question 21

Loss of Tail Rotor Control

Answer 21

*1. Collective/airspeed—Adjust as required to control yaw

Question 22

Tail Rotor Quadrant Caution

Answer 22

*1. Check for tail rotor control.

If tail rotor control is not available:

*2. Loss of Tail Rotor Control Emergency procedure —Perform.

Question 23

Hydraulic System Warning

Answer 23

*1. Land Immediately

Question 24

1 and #2 Hyd Pump Failure

Answer 24

• 1. Restrict flight control movement.

* 2. Land as soon as possible.

Question 25

#1 Primary Servo or #1 Transfer Mod Leak

Answer 25

* 1. SERVO switch—1ST OFF. * 2. Land as soon as practicable. If the BACKUP RSVR LOW caution also appears or the backup pump fails: *3. Land as soon as possible. Be prepared for loss of tail rotor control If the #2 PRI SERVO PRESS caution and/or HYD warning appears: *4. Land immediately.

Question 26

#2 Primary Servo or #2 Transfer Mod Leak

Answer 26

* 1. SERVO switch—2ND OFF. * 2. Land as soon as practicable. If the BACKUP RSVR LOW caution also appears or backup pump fails: *3. Land as soon as possible. Be prepared for loss of the pilot-assist servos If the #1 PRI SERVO PRESS caution and/or HYD warning appears: *4. Land immediately.

Question 27

Boost Servo Hardover

Answer 27

* 1. PAC call—“BOOST,BOOST,BOOST”. | * 2. SAS/BOOST pushbutton—Off.

Question 28

Utility Hyd Pump Caution

Answer 28

*1. Stop dome.

Question 29

AFCS Degraded Cautioln

Answer 29

*1. Safe altitude and airspeed—Establish (waveoff/Instrument Takeoff [ITO], as required).

Question 30

Stabilator Auto Mode Failure

Answer 30

* 1. PAC call—“STAB,STAB,STAB”. * 2. Cyclic—Arrest pitch rate. * 3. Collective—Do not reduce. * 4. STABILATOR MAN SLEW switch—Adjust to 0°.

Question 31

Unusual Attitude Recovery Procedure

Answer 31

* 1. Level wings. * 2. Nose on horizon. * 3. Center ball. * 4. Stop rate of climb/descent. * 5. Control airspeed.

Question 32

Electrical Power failure/Dual Generator Failure

Answer 32

* 1. Safe altitude and airspeed—Establish. * 2. Stabilator—Check position visually, slew as required. * 3. APU Emergency Start procedure—Perform. * 4. CMPTR PWR/RESET, SAS 1, SAS 2, TRIM, AUTOPLT, STABILATOR AUTO CONTROL push buttons—On.

Question 33

(#1/#2) FUEL FLTR BYPASS OR (#1/#2) FUEL PRESS CAUTION

Answer 33

*1. Fuel selector lever (affected engine)—XFD (DIR if currently in XFD).

Question 34

#1 AND #2 FUEL FLTR BYPASS OR #1 AND #2 FUEL PRESS CAUTIONS

Answer 34

* 1. Land as soon as possible. Be prepared for dual engine failure * 2. APU Emergency Start procedure--perform

Question 35

External Engine Fire

Answer 35

* 1. Confirm fire. * 2. Engine Malfunction in Flight emergency procedure—Perform. * 3. PCL (affected engine)—OFF. * 4. Engine T-handle (affected engine)—Pull. * 5. FIRE EXTGH switch—MAIN (RESERVE if required or ac power is off). If airborne and fire continues: *6. Land immediately. If fire appears extinguished: *7. Land as soon as possible.

Question 36

Internal Engine Fire An internal engine fire is indicated by a rise in TGT above 540°C after engine shutdown.

Answer 36

*1. Starter—Engage. Motor engine.

Question 37

APU Fire

Answer 37

* 1. APU T-handle—Pull. * 2. Confirm fire. * 3. FIRE EXTGH switch—RESERVE (MAIN if required and available). If airborne and fire continues: *4. Land immediately. If fire appears extinguished: *5. Land as soon as possible. If on ground: *6. Fire extinguisher—As required.

Question 38

COCKPIT/CABIN FIRE

Answer 38

If source is known: * 1. Affected power switches and circuit breakers— OFF/Pull. * 2. Portable fire extinguisher—As required. If fire continues or source is unknown: * 3. Cabin/doors/vents/ECS—Close/OFF, as required. * 4. Unnecessary electrical equipment and circuit breakers—OFF/Pull. If fire continues: *5. Land as soon as possible.

Question 39

SMOKE AND FUMES ELIMINATION

Answer 39

* 1. Airspeed—Adjust, as required. * 2. Doors/windows/vents—Open. * 3. Aircraft—Yaw, as required.

Question 40

IMMEDIATE LANDING/DITCHING

Answer 40

* 1. Crew and passengers—Alert. * 2. Harness—Locked. * 3. APU Emergency Start procedure--Perform as required * 4. External cargo/stores/fuel—Jettison/dump,as required. * 5. Searchlight—As required. * 6. Mayday/IFF—TRANSMIT/EMER. In the flare: *7. Windows—Jettison, reset handle as required. After landing: * 8. PCLs—OFF. * 9. Rotor brake—On. * 10. Copilot collective—Stow. * 11. Pilot HCU—Stow. After all violent motion stops: *12. Egress.

Question 41

UNDERWATER EGRESS

Answer 41

* 1. Emergency Breathing Device—As required. * 2. Cords—Disconnect. * 3. Door/window—Open/jettison. * 4. Place hand on known reference point. * 5. Harness—Release. * 6. Exit helicopter. After egress: *7. Swim clear of helicopter and inflate LPU.

Question 42

DUAL EGI FAILURE

Answer 42

* 1. Backup instruments—Scan, as required. | * 2. #1 and #2 EGI PWR switches—OFF, then ON.

Question 43

MTS UNCOMMANDED LASING

Answer 43

* 1. ACI MASTER ARM—SAFE. * 2. LASER SELECT switch—SAFE. If lasing continues: *3. FLIR bezel key> +FLIR OFF—Select.

Question 44

HELLFIRE MISSILE HANGFIRE

Answer 44

If rocket motor ignites and aircraft yaws: *1. Adjust controls as required to maintain straight-and-level flight.

Question 45

ROCKET HANGFIRE

Answer 45

* 1. Point weapon in a safe direction. * 2. Safe weapon. a. +1760 OFF—Select. b. ACI MASTER ARM—SAFE.

Question 46

Ground Resonance/Unusual Vibrations on Deck

Answer 46

If ground resonance is encountered and a safe takeoff is possible: *1. Takeoff immediately *2. Unusual Vibrations in Flight emergency procedure--Perform If ground resonance is not encountered or a safe takeoff is not possible: *3. Collective--Lower *4. PCLs--Off *5. Rotor Brake-- Apply as required

Question 47

Sonar Cable Angle Malfunction

Answer 47

*1. PAC call "CABLE, CABLE, CABLE" *2. Cable Angle Pushbutton--Off *3. Cable angle display--Center *4. SO--Fold array