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Engine Hot Start
- Starter....................Engage and hold until TOT <810C
- Throttle...................Close
- Fuel Valve Switch.....Off
- IGN ENG C/B...........Out
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Exterior Engine Fire
- Starter swit.......Release
- GPU..................Off
- Helo.................Complete emergency shutdown
- Note
- At pilot's discretion, fight fire with the on-board fire ext
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Engine Fire
- Helo........................Est. Auto
- Throttle...................Close
- Fuel Valve Switch......Off
- Helicopter................Complete auto landing
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Cabin Fire
- Helo.........................Start descent
- Blower A/C Swit.........Off
- Vents/windows..........Open
- Helo.........................Land as soon as possible, do an emerg shutdown.
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Electrical Fire
- Gen Switch.....................Off
- Bat Switch......................Off
- If: Fire, smoke/fumes persists
- Vents/windows................Open
- Helo..............................Land ASAP, do an emerg shutdown
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Engine Failure at hover or taxi
- Pedals...................Align Skids, maintain direction
- Cyclic....................Control direction, attitude and drift
- Collective...............Cushion landing
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Engine failure in-flight
- Helo...........................Est. Auto
- If Engine fails to automatically relight
- Throttle......................Closed
- Helo..........................Complete Auto Ldg
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Governor/ FCU - High Side Failure
- Collective..................Increase to maintain Nr
- Throttle....................Reduce to Maintain 97% to 100%N2
- Helo........................Land as soon as possible
- If unable to maintain powered flight;
- Throttle....................Close
- Helo.........................Est Auto
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Governor/FCU - Low Side Failure
- Collective................Decrease to control Nr
- Throttle..................Full
- GOV RPM Swit.........Increase to max
- Blower A/C swit.......Off
- If unable to maintain powered flight
- Helo......................Est Auto
- Else if:Powered flight can be maintained
- Helo......................Land ASAP
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Main Drive Shaft Failure
- Helo........................Est Auto
- Throttle...................Maintain 97%-100%N2
- Helo.......................Complete Auto Ldg
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Rotor Low RPM (RPM below 90+/-3%Nr)
- Collective.....................Reduce
- Throttle.......................Full
- GOV RPM(beep)switch...To Max
- Blower AC switch...........Off
- If rotor RPM still decreasing
- Helo...........................Treat as Eng Fail
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Tail Rotor loss of Thrust/Components
Warning:
Aggressive application of aft cyclic can cause the main rotor to contact the tailboom. When pitched nose-down, do not aggressively apply aft cyclic. Catastrophic damage can result from main rotor contact with the tailboom.
- Helo.............................Reduce Collective to control yaw
- If adverse yaw is encountered
- Helo.............................Est Auto
- Throttle.......................Close for landing
- Helo............................complete autorotative landing
- Else if: yaw is controllable
- Helo...........................Resume restricted powered flight, position to suitable landing area. Enter and complete auto
- Throttle.........Close for landing
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Pedals locked at hover (left YAW)
Warning:
Application of power below 30 KIAS can start a rapid rotation to the right. Consider the helicopter committed to land below 30 KIAS. Rapid rotation with the pedals locked can result in loss of control.
- Cyclic.....................Eliminate drift
- Collective...............Lower,
- Accept left rotation
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Pedals locked at hover (Right YAW)
- Throttle.......................Idle
- Cyclic..........................Eliminate Drift
- Collective....................Cushion Ldg
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Hydraulic System hardover
- Hydraulic System Swit............Off
- Helo.....................................Land ASAP
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Hydraulic System Failure
- Helo.......................Gradually reduce speed (61-69KIAS)
- Hyd system.............Confirm On
- Hyd Boost C/B.........Out
- If: Hyd press is not regained:
- Hyd Boost C/B.........In
- Hyd System.............Off
- Helo....................Land as soon as practical
- Approach..............Shallow to normal terminate in a run-on landing
- Landing................A run-on landing at 10KIAS to 15KIAS is recommend.
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Emergency Shutdown
Warning:
Caution:
- Warning: Rapid engagement of rotor brake on ice or slippery surfaces can cause the rotorcraft to rotate. Avoid rapid rotor brake engagement on slippery surfaces. Sudden rotorcraft rotation can cause loss of control.
- Caution: Low rotor rpm and wind can cause excessive rotor flapping and/or coning. Do not use collective and/or pedal inputs to slow the main rotor blades. Excessive flapping or coning can cause equipment damage.
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Emergency shutdown
- Throttle...............Close
- Fuel Valve Swit....Off
- Bat Swit.............Off
- Rotor Brake........Engage, allow rotors to stop
- Helo...................Open or jettison doors and egress.
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Engine restart (in-flight)
Caution:
TOT rises rapidly in engine restart at high altitude. Do not do an engine restart above 12000'. Engine restart above 12000' will cause TOT to rise too fast to control.
- Altimeter..............Check for sufficient Altitude
- Collective.............Maintain 90%-107% Nr
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Free Wheel Unit failure
- Helo...............Est Auto
- Throttle..........Idle
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Engine Compressor stall
- Collective..................Reduce
- Eng Anti-Ice Swit.......reposition
- Heat Vent Swit..........reposition
- Blower A/C Swit........AC off
- If problem continues
- Helo........................Land ASAP be prepared for an engine failure at any time
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Engine Oil Press
- Engine oil Press and Temp gauge....Monitor gauge
- Power....................................Reduce
- Helo...........................................Land ASAP
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Transmission Oil Temp @ or above 110
- Collective.............Reduce power, monitor gage
- Trans oil temp caution light remains on
- Helo....................Land ASAP
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Transmission oil pressure (below 30PSI)
Helo....................LAND ASAP, monitor gage
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Fuel boost pump failure
Warning:
Bank/Pitch inputs combined with a low fuel condition can cause air ingestion in the fuel lines. Do not exceed 10 deg bank or pitch with less than 15 gal. Air ingestion can cause loss of power or engine flameout.
- Fuel Press..................Check
- Helo..........................Land ASAP a dual pump failure can cause the loss of head pressure to the eng-driven fuel pump and result in power loss
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Engine Fuel Filter
Helo.................Land as soon as possible
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Metallic Particles
- Chip FAULT caution light switch....Press then release
- Helo.........................................Land ASAP
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Icing Conditions
Warning:
- Turning the ENG ANTI-ICE ON after encountering icing can cause ice to break off the inlet guide vanes and enter into the compressor. Unless absolutely necessary the helo is to be landed and shutdown prior to continuing flight with the ENG ANTI -ICE ON. Ice ingestion into the compressor can cause engine damages and loss of power.
- Helo............Fly clear of icing conditions
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