ICS FAILURE

Indication
=> Loss of Audio tone and/or no response to voice commands

CORRECTIVE ACTION

1. Perform an ICS check, check hoist pendant ICS switch and visually inspect cord. If in position to safely do so, retrieve the device(FM).
2. Perform an ICS Check, check PTT and cord (P).
3. Slowly move the aircraft to establish visual reference with the hoisting area(P).
4. Payout slack - AS REQ'D(FM)
5. Troubleshoot ICS Malfunction.

If ICS malfunction is corrected, proceed with normal hoist procedures.

If ICS malfunction is not corrected:
6. Position aircraft to recover rescue device per Rescue Briefing
7. Signal pilot to reestablish visual reference with hoisting area by pointing to the left side of aircraft. Rescue device may or may not have been recovered(FM).
8. Observe signal, pass to pilot(CP)
9. Slowly move aircraft to establish visual reference with the hoisting area(P).

If device was recovered:
10. Complete hoist of rescue device (FM).

If the device was not recovered:
11. Make onscene repairs, abort the mission, or take other action as appropriate

LOST SWIMMER

Day:
1. Mark and note position
2. Transition and establish right-hand orbit
3. Search/Monitor for rescue swimmer signal

Night:
1. Mark and note position
2. Flash landing/Hover lights
3. Search/monitor for rescue swimmer signal

LEAVING RESCUE SWIMMER ONSCENE

1. Mark and note position

2. Deploy lighted raft

3. Deploy DMB

4. If time/situation permits, contact Rescue Swimmer via pre-briefed radio frequency and advise of situation/intentions.

5. Notify SAR Mission Coordinator

EMERGENCY RECOVERY OF THE RESCUE SWIMMER

If aircrew on the helicopter observe the IN TROUBLE NEED ASSISTANCE hand signal or see a potential hazard to the swimmer such as dangerous marine life, the helicopter shall move into position for an emergency pickup of the swimmer using one of the following devices:

1. Rescue Basket - if rigged and empty. The rescue basket is the primary device for recovery

2. Bare Hoist Hook - rescue basket is not readily available.

EMERGENCY FLYAWAY DURING HOISTING OPERATIONS

If the swimmer or device is attached to the hoist hook between the water and beneath cabin door:

1. "SHEAR, SHEAR, SHEAR" (P, CP, FM).

2. EMER REL - Press (P, CP).

3. HOIST SHEAR - Shear (FM).

If swimmer or device is attached to the hoist hook between cabin door and hoist drum:

1. Bring swimmer into cabin or maintain firm handhold

PILOT EMERGENCY LANDING PROCEDURE

During descent:

1. Alert Crew

2. Shoulder harness - Locked

3. Transmit Distress Call

4. IFF - EMER

5. FUEL BOOST PUMPS - Off

After Landing (water):

6. ENG POWER CONT levers - OFF

7. Copilot Collective - RETRACT

8. Egress helicopter when rotor stops

After Landing (Land):

1. EMER ENG Shutdown

2. Rotor brake - ON

3. BATT switch - OFF

4. Egress helicopter

EMERGENCY EGRESS PROCEDURE

1. Reference Point - Locate and remain calm

2. SEAS Bottle - Employ as required

3. Emergency Exits - Locate emergency release handles, push/pull, and jettison

4. ICS Cord - Disconnect

5. Reference Point - Relocate and hold

6. Seatbelt/Harness - RELEASE

7. Egress - Holding reference points, exit at right angles to the aircraft.

Lifevest - Inflate as required when clear of the aircraft

VORTEX RING STATE

Indications:

Aircraft in a vertical descent with max power applied and little or no cyclic authority. Nr remains at 100%. May be entered any time the Main rotor is in a state of high upflow and low longitudinal airspeed such as quick stop type manuevers or during autorotative recoveries. Power should be increase once airspeed is above approx 20KIAS

CORRECTIVE ACTION:

1. Decrease collective pitch

2. Increase forward airspeed or establish directional flight

3. Enter autorotation if altitude permits

BLADE STALL

CORRECTIVE ACTION:

1. Decrease collective pitch

2. Decrease severity of manuever

3. Gradually decrease airspeed

4. Increase rotor RPM

5. Decrease altitude

Brief Discussion:

The retreating blad will stall since it is traveling at the rotational velocity, minus the forward speed of the helicopter.

Most likely to occur when operating at high values of speed gross weight, density altitude, power and aggrevated by low Nr.

Manuevers, acceleration, or turbulent air, all of which increase g-load factors, reduce the airspeed at which blade stall will occur.

In a blade stall, each main rotor blade will stall as it passes through the stall region and create vibrations per revolution equal to the number of blades.

Fully developed blade stall will induce a pitch up and left. Forward cyclic is ineffective at this point and may aggrevate the condition because it increase the angle of attack of the retreating blade.

CAAS FAILURES: Which CAAS Failures result in LAND AS SOON AS POSSIBLE?

1. Loss of DCU 1 and 2

2. Loss of 4 MFD's

3. Loss of CDU 1 and 2

4. Loss of GPPU 1 and 2

Dual EGI failure

Indications:

- Loss of navigation info including heading and attitude display on the PFD. If coupled, Roll Couple will kick off.

- AFCS Degraded Caution flashing

- EGI source indicator is replaced with a Red Failure flag if invalid

- NAV FAIL Advisory

- Degraded aircraft stability

Corrective Action:

1) Transfer scan to the ESIS

CAAS Failures: Which CAAS failures result in Land as soon as Practicable?

1. Loss of DCU 1 or 2

2. Loss of CDU 1 or 2

3. Loss of GPPU 1 or 2

4. Loss of 2 or 3 MFDs

5. loss of MFD 1and MFD 4

6. Loss of ADC 1 and ADC 2

7. Loss of EGI 1 and EGI 2

Smoke and fume elimination procedure

Corrective action:

1) Airspeed - 70KIAS or less

2) Cabin Door - Open

3) Windows and vents - open to blow air into cockpit

4) Yaw aircraft to vent smoke and fumes

Electrical Fire

Indications:

- Acrid smell of burning eletrical insulation

- Smoke, flames, and/or sparks visible in the cabin or cockpit

Corrective Action:

1) Alert the crew

2) Designate a crew member to fight the fire

3) Affected equipment and associated circuit breakers - OFF/PULL

4) Windows and vents - CLOSED

5) Doors - CLOSED

6) ECS - OFF

If the fire appears out

7) Land as soon as practicable

If the fire persists

8) Generators, convertors, and other logical equipment - OFF

9) Land Immediately

Perform smoke and fume elimination procedure as necessary

Cockpit Cabin Fire

Symptoms:

- Smoke or flames visible in the cockpit

Corrective Action:

1) Alert the crew

2) Designate a crew member to fight the fire

3) Windows and vents - CLOSED

4) Doors - CLOSED

5) ECS - OFF

If the fire appears out

6) Land as soon as practicable

If the fire persists

7) Land Immediately

Post shutdown fire

Symptoms:

- TGT remains or climbs above 540C after engine shutdown

Corrective action:

1) Engine Ignition Switch - OFF

2) Engage starter, motor engine until TGT below 300C; disengage starter

Engine Compartment Fire

Symptoms:

- FIRE Warning Lights on

- Engine fire warning T-handle lights on

Corrective Action:

1) Alert Crew

2) Confirm Presence of fire
 If fire is confirmed
3. Engine Malfunction Procedure
4. ENG PCL on Affected Engine - OFF
5. ENG FIRE T-Handle - PULL

 6. FUEL BOOST PUMP - OFF(Associated Engine
7. FIRE EXT Switch - MAIN (Reserve if required)
If the fire Continues

8. LAND IMMEDIATELY

If fire appears out:
9. LAND AS SOON AS POSSIBLE

APU Compartment fire

Symptoms:

- FIRE warning lights on

- APU fire warning T-handle on

Corrective Action:

1) Alert Crew

2) Confirm presence of fire

a. If unable to confirm, LAND AS SOON AS POSSIBLE

3) APU FIRE EXT T-handle pull

4) FIRE EXT Switch Reserve(Main if required and available

If fire persists:
6) Land Immediately

Total Loss of AC Electrical Power

Symptoms:

- Loss of all AC powered equipment

- Loss of all equipment powered by No. 1 and No. 2 DC PRI BUSES

- Loss AFCS

- Loss of MFD's 1 and 5

- Loss of Copilot and Cabin CDU

Corrective action:
1) Transfer Scan to ESIS - AS REQUIRED

2) Generators No. 1 and No. 2 - OFF/RESET then ON
3) EMER APU START
4) APU Generator switch - Verify ON

5) Stabilator - CHECK POSITION - SLEW AS REQUIRED
 If AC power not restored:
6) LAND AS SOON AS POSSIBLE

AC Essential Bus Failure

Symptoms:
1) AC ESS BUS OFF Caution on
2) AFCS DEGRADED Caution flashing
3) Degraded Aircraft stability
4) #2 PITOT HEAT Caution on
5) Loss of No.1 and No.4 MFDs
6) Loss of Mission Senser Manager(TCAS, RADAR, MFD ESS functionality lost, HUD)
7) Loss of System Manager (BIT, Zeroization, Data load/transfer, Avionics monitoring
8) Loss of Flight Director

CORRECTIVE ACTION:
1) Stabilator - Check position - Slew as required

DUAL CONVERTER FAILURE

Indications:

1. #1 CONV Caution on

2. #2 CONV Caution

3. NAV FAIL Advisory

4. EGI 1 and GPS 1 NAV FAIL Advisories

5. EGI 2 and GPS 2 NAV FAIL Advisories

6. Loss of power to all items on the NO.1 and NO.2 DC PRI BUSES

7. Loss of all Flight Instrumentation with MFDs still powered

8. Stabilator Caution on

9. AFCS Degraded Caution

10. CHECK LRU STATUS Advisory

Corrective Action:

1. Transfer Scan to ESIS - AS REQUIRED

DUAL FUEL FILTER BYPASS

Symptoms:

1. #1 and #2 FUEL FLTR BP Cautions on.

CORRECTIVE ACTION:

1. LAND AS SOON AS POSSIBLE. Fly at a safe alttude and airspeed for entry into autorotation if both engines fail.

ENGINE-DRIVEN BOOST PUMP OR FUEL LINE FAILURE

Symptoms:

1. #1 or #2 FUEL PRESS Caution

CORRECTIVE ACTION:

1. FUEL BOOST PUMP - OFF

2. FUEL SELECTOR LEVER ON AFFECTED ENGINE - XFD

DUAL ENGINE-DRIVEN FUEL BOOST PUMP OR FUEL LINE FAILURE

Symptoms:

1. #1 and #2 FUEL PRESS Cautions on

CORRECTIVE ACTION:

1. FUEL BOOST PUMP switches - OFF

2. LAND AS SOON AS POSSIBLE. Fly at a safe altitude and airspeed for entyr into autorotation if both engines fail

What are your symptoms for a No.1 Hydraulic Pump failure?

Symptoms:

1. #1 HYD PUMP Caution on

2. BACKUP PUMP ON Advisory

3. #1 T/R SRVO OFF Caution on

4. #1 T/R SRVO Advisory on

Symptoms:

1. #2 HYD PUMP Caution

2. BACKUP PUMP ON Advisory

Symptoms:

1. #2 HYD PUMP Caution on

2. #2 PRI SRVO PRES Caution on

3. BACKUP PUMP ON Advisory off

4. BOOST SERVO OFF Caution on

5. SAS Caution on

6. AFCS DEGRADED Caution flashing

Failure of No.1 and No.2 Hydraulic pumps

Symptoms:

1. #1 and #2 HYD PUMP Cautions on

2. BACKUP PUMP ON Advisory

3. #1 T/R SRVO Off Caution on

4. #2 T/R SRVO ON Advisory on

Corrective Action:

1. LAND AS SOON AS POSSIBLE - Restrict control movements to moderate rates.

Complete Loss of No.1 Hydraulic Fluid

Symptoms:

- #1 HYD PUMP Caution on
- #1 RSVR LOW Caution on
- BACKUP PUMP ON Advisory

Corrective Action:

1) SERVO Switch - 1st OFF
2) LAND AS SOON AS PRACTICABLE

If the B/U RSVR LOW or any #2 Hydraulic System Cautions are displayed:

3) LAND AS SOON AS POSSIBLE

If the B/U RSVR LOW and any #2 Hydraulic System Cautions are displayed:

4) LAND IMMEDIATELY

What are the symptoms for Partial loss of No.2 Hydraulic Fluid?

Symptoms:

- #2 RSVR LOW Caution

- BOOST SERVO CAUTION ON

- SAS CAUTION ON

- AFCS DEGRADED CAUTION FLASHING

Complete loss of #2 Hydraulic Fluid

Symptoms:

- #2 HYD PUMP Caution on.

- #2 RSVR LOW Caution on.

- BACKUP PUMP ON Advisory

CORRECTIVE ACTION:

1) SERVO SWITCH - 2ND OFF

Loss of fluid in backup Hydraulic System

Symptoms:

- B/U RSVR LOW Caution on

- All other hydraulic system indications normal

CORRECTIVE ACTION:

1) BACKUP HYD PUMP switch - OFF

BOOST SERVO MALFUNCTION

Symptoms:

- Increased control forces in collective, pitch, or yaw

- Uncommanded flight control movement in collective, pitch, or yaw (hardover)

CORRECTIVE ACTION:

1) SAS/BOOST pushbutton - OFF

BOOST SERVO CAUTION ON

Symptoms:

- BOOST SERVO OFF Caution on

- Control forces similar to flight with SAS/BOOST off in the affected axis or axes

CORRECTIVE ACTION:

1) SAS/BOOST pushbutton - RESET

MAIN ROTOR DAMPER MALFUNCTION

Symptoms:

- Low frequency (1, 2, or 2/3 per revolution) lateral or vertical vibration

CORRECTIVE ACTION:

1) Nr - MAINTAIN

2) Airspeed - ADJUST to minimize vibrations

3) Make small smooth control inputs and shallow turns as required

ROTOR BRAKE ADVISORY ON

Symptoms:

- ROTOR BARAKE Advisory on

CORRECTIVE ACTION:

1) Rotor Brake Handle - CHECK IN THE DETENT. PRESSURE GAUGE AT ZERO

2) Check for evidence of Puck dragging

If secondary indications present:
3) LAND AS SOON AS POSSIBLE

Rotor Blade Damage or abnormal vibrations

If main or tail rotor blade damage is known or suspected.

On Deck:

1. Do not takeoff

In-Flight: If vibrations are severe and/or flight characteristics are abnormal:

1) LAND IMMEDIATELY

If vibrations are moderate with no other change in flight characteristics:
2) LAND AS SOON AS POSSIBLE

If there are no secondary indications or vibrations:

3) LAND AS SOON AS PRACTICABLE

TAIL ROTOR GEARBOX MALFUNCTIONS

Symptoms: Any one or more of the following Cautions on.

a. TGB CHIP

b. IGB CHIP

c. TGB OIL TEMP

d. IGB OIL TEMP

CORRECTIVE ACTION:

1) LAND AS SOON AS POSSIBLE.- Use minimum power required to fly at a safe altitude and airspeed for entry into autorotation if tail rotor drive failure occurs.

When do I LAND AS SOON AS PRACTICABLE for a MAIN TRANSMISSION MALFUNCTION

Symptoms:

1) Any one or more of the following symptoms exist:

a) XMSN PRESS in the upper yellow or red range
b) MXMSN CHIP Caution
c) #1 ACCESS CHIP Caution
d) #2 ACCESS CHIP Caution

2) In combination with any of the following

a) Strong medium frequency vibrations

b) Hot metal fumes in the pylon or aft station area

c) Yaw kicks

d) Any other dynamic indication of impending tail rotor drive failure

CORRECTIVE ACTION:

1) LAND IMMEDIATELY - Use minimum power required to fly at a safe altitude and airspeed for entry into autorotation if tail rotor drive failure occurs.

TAIL ROTOR DRIVE FAILURE WHILE HOVERING

Symptoms:

1) Helicopter yaw sharply to the right

2) Tail rotor pedals movable but with no apparent effect

3) Possibly other indications of tail gearbox malfunction and/or failures

Corrective Action:

1) Collective Reduce

2) PCL's - Off (10-20 feet AGL)

3) Maintain a level attitude. Eliminate yaw and drift.

4) Cushion landing with collective

Tail Rotor Drive Failure While in Forward Flight

Symptoms:

- Helicopter yaw accelerates uncontrollably to the right and rolls left

- Tail rotor pedals movable but with no apparent effect

- Possible other indications of tail gearbox malfunction and/or failures

- Airspeed rapidly decreases

CORRECTIVE ACTION:

1) AUTOROTATE - ENG POWER CONTROL levers OFF prior to the flare

When do I LAND AS SOON AS POSSIBLE for a Main Transmission Malfunction?

If any one or more of the following symptoms exists without indications of an imminent failure:
1) XMSN TEMP in the yellow or red range
2) XMSN PRESS in the lower yellow or red range
3) MXMSN OIL TEMP Caution
4) MXMSN OIL PRESS Caution

 When do I LAND IMMEDIATELY for a MAIN TRANSMISSION MALFUNCTION 

Symptoms:
a. XMSN temp in the yellow or red range.
b. XMSN press in the lower yellow or red range.
c. XMSN press in the upper yellow or red range
d. MXMSN OIL TEMP CAUTION
e. MXMSN OIL PRESS CAUTION
f.  MXMSN CHIP
g. #1 ACCESS CHIP
h. #2 ACCESS CHIP

In combination with any of the following:

a. Yaw attitude excursion with no control input

b. Increase in power required for a fixed collective setting

c. Failure of main generator or hydraulic pump

d. Increased noise

e. Increased vibration levels

f. Abnormal fumes in the cabin

CORRECTIVE ACTION:

1) LAND IMMEDIATELY

What are the symptoms for ENGINE OIL SYSTEM

Symptoms:
Any one of these conditions 
1) #1 or #2 ENG CHIP Caution on

2) #1 or #2 ENG OIL PRESS  and/or associated ENG OIL PRESS in ower yellow or red range.
3) No. 1 or No. 2 ENG OIL PRESS in upper red range
4) #1 or #2 ENGINE OIL TEMP Caution and/or associated ENG OIL TEMP in red range
5) #1 or #2 OIL FLTR BP
6) Visible signs of oil leak
7) Abnormal Engine noise 

what is the corrective action for ENGINE OIL SYSTEM

CORRECTIVE ACTION:

1) Engine Malfunction Procedure 
If more than one symptom exists, or engine oil pressure is in the lower red range:
2) EMER ENG SHUTDOWN PROCURED 
3) LAND AS SOON AS PRACTICABLE

If only one symptom exists:
4) Affected ENG PCL - IDLE
5) LAND AS SOON AS PRACTICABLE.
If #1 OIL FLTR BP or #2 OIL FLTR BP is the only symptom:
6) Return ENG PCL to FLY in an attempt to clear the caution
7) Land as soon as Practicable 

ENGINE OSCILLATIONS

Symptoms:

- TQ, Ng, Np, and TGT of both engines, if indicated, oscillate out-of-phase.
- Nr oscillates in phase with malfunctioning engine. 

CORRECTIVE ACTION:

1) Engine Malfunction Procedure

ENGINE LOW-SIDE FAILURE

Symptoms:

- Nr at 100% in low to normal power situations and decays below 100% as high power is demanded

- Np malfunction engine at or below 100%

- Ng, TGT and torque, if functioning properly, differ significantly between engines, with malfunction engine indicating low

CORRECTIVE ACTION:

1) Engine Malfunction Procedure

ENGINE HIGH SIDE FAILURE

Symptoms:

- Nr/Np above normally selected speed and rise rapidly as collective is lowered to reduce power demand below that provided by the malfunction engine

- NG, TGT, torque, if functioning properly, differ significantly between engine, with malfunction engine indicating high

- Ng, TGT, and/or torque of the malfunctioning engine may be erroneous or absent

CORRECTIVE ACTION:

1) Engine Malfunction Procedure

Impending Engine High Speed Shaft Failure

Symptoms:

- Medium frequency vibrations

- Howling noise

- Transmission oil leak

- Increasing transmission oil temperature

- Decreasing transmission oil pressure

CORRECTIVE ACTION
1. Engine Malfunction Procedure 
2. Land as Soon As Practicable 

HIGH- SPEED SHAFT FAILURE

Symptoms:

- Np above Nr

- Torque indicating at or near zero

- Engine flameout when Np reaches 120%. Engine may or may not restart and continue to operate

- #1 or #2 ENG HSS FAIL Caution on

CORRECTIVE ACTION:

1) Engine Malfunction Procedure 
2) EMER ENG Shutdown on Affected Engine 

ENGINE COMPRESSOR STALL

Symptoms:

- Rapid increase in TGT

- Hung-up or decreasing Ng

- Decrease in torque

- Possible audible popping or rumbling noises or changes in engine noise

- Possible oscillation of torque and Np on both engines

CORRECTIVE ACTION:

1) Engine Malfunction Procedure 

2) ENG POWER CONT lever (malfunctioning engine) - IDLE

Single Engine Failure While Hovering at Low Altitude

CORRECTIVE ACTION:

1) Maintain level attitude. Eliminate yaw and drift

2) CONTGCY PWR - ON

3) Cushion landing with Collective

HOT START

Symptoms:

- TGT reaches 851C before idle speed (63%Ng) is reached

CORRECTIVE ACTION:

1) ENG POWER CONT lever - OFF

2) Engine Ignition switch - OFF

3) Engage starter and motor the engine until TGT is below 300C. Disengage the starter

ABORT START PROCEDURE

Symptoms: If any of the following occur

- Ng does not reach 14% within 6 seconds of engine starter activation

- No indication of TGT within 30 seconds of engine starter activation

- No indication of oil pressure within 30 seconds of engine starter activation

- ENG STARTER advisory goes out before 52% Ng

CORRECTIVE ACTION:

1) ENG POWER CONT lever - OFF

2) Check ENG STARTER Advisory out

3) Monitor TGT for post shutdown fire

EMER Engine Shutdown

CORRECTIVE ACTION:

1) ENG POWER CONT lever(s) - OFF

2) FUEL SELECTOR lever(s) - OFF

3) FUEL BOOST PUMP switch(es) - OFF

4) Monitor TGT for post shutdown fire

EMER APU START

CORRECTIVE ACTION:

1) ECS - OFF

2) FUEL PUMP switch - APU BOOST

3) APU CONT switch - ON

4) Backup Pump - Cycle ON/AUTO (AS REQUIRED)

EMERGENCY ENGINE RESTART

May be attempted anytime after shutdown if there are no indications of mechanical malfunction or engine fire

CORRECTIVE ACTION:

1) EMER APU START

2) FUEL SELECTOR LEVER - DIR or XFD

3) Air Source ECS/Start switch - AS REQUIRED

4) ENGINE IGNITION switch - NORM

5) ENG POWER CONT lever - OFF

6) Starter - ENGAGE

7) PCL - IDLE

8) PCL(after Ng stablizes) - FLY

AUTOROTATE

1) Collective - down to enter autorotation

2) Airspeed - Adjust to 75 - 95 KIAS

3) If altitude permits:

a) Turn into the wind

b) Analyze the malfunction

c) Perform Emergency Landing Procedure

4) At approximately 200 feet AGL, initiate a flare to decrease airspeed and rate of descent

5) At 35-60 feet assume the landing attitude. Eliminate yaw and drift

6) Cushion landing with collective

AFCS VOLTAGE SENSOR RELAY

Symptoms:

- MASTER Caution Illuminated

- AFCS DEGRADED Caution flashing

- AFCS control panel FAIL ADVISORY Mode Reset Capsules - ON: CPLR, CORD, AUG, ATT, A/S, HDG, ALT and BIAS.

- Degraded aircraft stability

CORRECTIVE ACTION:

1) Establish safe altitude and airspeed

2) Check BARALT/RADALT Hold status - AS REQUIRED

SAS MALFUNCTION

Symptoms:
1) SAS CAUTION on
2) Erratic flight (loss of dampening)
3) Hardover

CORRECTIVE ACTION:
1) Establish safe altitude and airspeed
2) Check BARALT/RADALT Hold status - AS REQUIRED

AFCS COMPUTER POWER LOSS

INDICATIONS:
1) AFCS DEGRADED Caution - ON (steady)
2) One or more AFCS Control Panel FAIL ADVISORY Mode reset Capsules on
3) SAS 2, TRIM, AUTO PLT - OFF (cannot be selected

Corrective Action:
1) Establish safe altitude and airspeed
2) Check BARALT/RADALT Hold status - AS REQUIRED

AFCS DEGRADED AND MASTER CAUTIONS ILLUMINATED DURING AUTO APPROACH OR DEPARTURE

INDICATIONS:
1) AFCS DEGRADED Caution - ON(flashing)
2) One or more AFCS Control Panel FAIL ADVISORY Mode Reset Capsules on.

CORRECTIVE ACTION:
1) Abort Approach or Departure using maual ITO
2) Establish safe altitude and airspeed

3) Check BARALT/RADALT Hold status - AS REQUIRED

AFCS DEGRADED AND MASTER CAUTIONS ILLUMINATED DURING COUPLED HOVER

INDICATIONS:
1) AFCS DEGRADED Caution - ON(flashing)
2) One or more AFCS Control Panel FAIL advisory Mode Reset Capsules on.

CORRECTIVE ACTION:
If aircraft remains in a stable hover:
1) Maintain stable hover
2) Attempt to reset malfunction using AFCS Degraded Caution On (steady or flashing) procedure, as required.

If hover becomes unstable or disorientation occurs:
3) Depart hover using manual ITO

4) Establish safe altitude and airspeed
5) Check BARALT/RADALT Hold status - AS REQUIRED

Tail Rotor Quadrant Caution with no loss of T/R control

Symptoms:

1) Loss of one tail rotor cable will be indicated by appearance of the T/R QUADRANT Caution. No change in handling characteristics should occur

Corrective action:

1) LAND AS SOON AS PRACTICABLE

Tail Rotor Quadrant Light with loss of T/R control

SYMPTOMS:

1) T/R QUADRANT Caution on
2) Uncommanded right or left yaw
3) No response in the yaw axis when either pedal is displaced

CORRECTIVE ACTION(non-memory):

1) External cargo, stores, and fuel - JETTISON AS REQUIRED
2) LAND AS SOON AS PRACTICABLE

NOTE:
Balanced flight may be achieved at about 45 and 120KIAS depending on aircraft gross weight.

What are the first 2 steps of T/R PEDAL BIND/RESTRICTION OR DRIVE WITH NO ACCOMPANYING CAUTION

CORRECTIVE ACTION:

1) Apply pedal force to oppose the drive
2) AUTO PLT and TRIM switches - OFF

ENGINE MALFUNCTION PROCEDURE

1. Nr - Maintain

2. CONTGCY PWR switch - AS REQUIRED
3. Altitude/Airspeed - AS REQUIRED
4. Fuel/Stores - JETTISON AS REQUIRED
5. ENG Anti-Ice - AS REQUIRED
6. Analyze 

#1 OIL FLTR BP AND #2 OIL FLTR BP

INPUT Chip

Symptoms:
1. #1 INPUT CHIP or #2 INPUT CHIP

CORRECTIVE ACTION
If secondary indications exist:
a. XMSN PRESS in yellow or red range.
b. XMSN TEMP in yellow or red range
c. MXMSN OIL TEMP
d. MXMSN OIL PRESS
e. Abnormal noises or vibrations from the main transmission area

1. ENGINE MALFUNCTION PROCEDURE 
2. Associated ENG POWER CONT lever - IDLE. Consideration may be given to bringing the ENG POWER CONT lever to FLY if required for safe landing.
3. LAND AS SOON AS POSSIBLE - Use minimum power required to fly at a safe altitude and airspeed for immediate landing in hte event of input module or main module failure.

FOULED CABLE

SYMPTOMS:
1. The hoist cable, hook or rescue device becomes fouled or secured ondeck.
CORRECTIVE ACTION
1. Immediately pay out cable
2. Advise the pilot

If injury or damage is imminent:
3. "SHEAR, SHEAR, SHEAR" FM
4. EMER REL button - PRESS (P, CP)
5. HOIST SHEAR switch - SHEAR (FM)

If injury or damage is not imminent:
6. Maintain position
7. Attempt to have flight mechanic and boat personnel free cable or rescue device.

If unable to free device from deck:
8. Cut cable with cable cutter
9. Abort mission or rig quick splice and continue hoist 

INADVERTENT IMC

SYMPTOMS
1. Unplanned entry into Instrument Meteorological Conditions (IMC) from Visual Meteorological Conditions (VMC).

CORRECTIVE ACTION
1. Announce "Inadvertent IMC."
2. Establish an instrument scan
3. Establish safe altitude, airspeed and heading.
4. External Communication - AS REQUIRED 

UNUSUAL ATTITUDE RECOVERY

UNUSUAL ATTITUDE RECOVERY
Unusual attitudes are considered to be attitudes beyond what is needed for normal flight within the confines of the aircraft's limitations. There are three general unusual attitudes: nose low, nose high, and high bank angles.

CORRECTIVE ACTION:
1. Level the wings
2. Smoothly place the nose on the horizon
3. Center ball
4. Adjust power to establish level flight

APU FAILURE

SYMPTOMS
1. APU FAIL Caution and APU FAIL(Overhead Console).

CORECTIVE ACTION
If APU continues to run:
1. APU CONTROL switch - OFF
2. Fuel Pump switch - OFF