Engine operating rpm, with zero to near zero torque must be maintained throughout the approach. Torque applied for landing should be used at low altitudes to aid in preventing seizure of the transmission.

The Nose of the helicopter will turn left when power is reduced

1. Fixed pedal - land
2. Loss of tail rotor thrust - Autorotate

1. Autorotate
2. EMER SHUTDOWN

1. BAT, STBY and MAIN GEN switches - OFF
2. Land as soon as Possible

1. Pedal input has no effect on helicopter trim
2. Nose of the helicopter turns to the right (left sideslip)
3. Roll of the fuselage along the longitudinal axis
4. Nose down tucking will also be present

Helicopter nose will turn to the right when power is applied

1. Enter autorotation (power off)
2. Maintain airspeed above min rate of descent
3. If running landing possible complete auto with touchdown speed 15-25 kts
4. If running landing NOT possible start to descel fro 75' so that forward ground speed is at a minimum when aircraft is 10-20; execute the touchdown with rapid collective pull prior to touchdown in a level attitude with minimum ground roll

1. Relax pressure on the collective control
2. Make a significant collective application either up or down
3. Increase collective friction

1. Circuit Breakers - Out. Check for indications of the source of the fire.
2. MAIN GEN switch - STBY GEN
3. BAT switch - ON
4. Circuit breakers - In one at a time in the priority required, GEN BUS RESET first. When malfunctioning circuit is identified pull the applicable circuit breaker out.

Airspeeds bellow 30-40 kts the sideslip may become uncontrollable and the helicopter will begin to revolve on the vertical axis.

1. If control can be maintained in powered flight the best solution is to maintain control with power and accomplish a running landing as soon as practicable.
2. If control cannot be maintained close the throttle immediately and accomplish an autorotational landing

Lower collective to regain control and allow the aircraft to touchdown with little if any forward movement

1. Start switch - Press. The switch must be held until EGT is in the normal range
2. Throttle - Off. Must be closed immediately after the starter switch is pressed.
3. FUEL switches - OFF

1. BAT switch - OFF
2. Land as soon as possible
3. EMER SHUTDOWN after landing

1. If no immediate safe landing area present continue flight to a suitable landing area at or above min rate of descent as. Degree of roll and sideslip may be varied by varying throttle and/or collective.
2. When landing area reached AUTOROTATE agove min rate of descent airspeed
3. If landing area suitable touchdown above ETL using throttle to maintain directional control
4. If running landing not possible start to descel at about 75' so forward airspeed is minimal when at 10-20 feet. Execute touchdown with rapid collective pull just prior to touchdown with min ground speed.

1. Maintain control with power and airspeed 40-70 kts
2. If needed reduce rpm (not bellow 91%) to control sideslip
3. Continue powered flight to a suitable landing area where a running landing can be done.
4. On final reduce rpm to 91% and accomplish running landing

1. Autorotate
2. EMER SHUTDOWN

EMER SHUTDOWN

Doors and windows and vents - Open

1. HYD CONT switch - select opposite position
2. Land as soon as practical in an area that permits a running landing. Maintain a/s at or above ETL at touchdown.

Heading cannot be controlled with pedals

1. Throttle - Full Open
2. Land as soon as Possible

With Power: 1. Land as soon as Possible 2. EMER SHUTDOWN after landing / Without Power: 1. Autorotate 2. EMER SHUTDOWN

1. Airspeed - adjust as necessary to attain the most comfortable level of control movements
2. HYD CONT circuit breaker - Out
If hydraulic power is not restored:
3. HYD CONT circuit breakers - In.
4. HYD CONT switch - OFF
Land as soon as practicable in an area that allows a running landing with power. Maintain a/s above ETL until touchdown.