R44 Emergency Procedures Flashcards
Definition Land Immediately
Land on the nearest clear area where a safe normal landing can be performed. Be prepared to enter autorotation during approach, if required
Definition Land as soon as Practical
Landing site is at Pilot’s discretion based on nature of the problem and available landing areas. Flight beyond nearest airport is not recommended
Power Failure Above 500ft
- Lower collective immediately to maintain RPM
- 70kts or maximum glide/maximum endurance
- Keep RPM between 97% and 108%
- Select landing spot and, if altitude permits, maneuver to land into wind
- Air restart if possible
- Switches and fuel valve off
- Land
Power Failure Between 8ft and 500ft
- Lower collective immediately to maintain RRPM
- Keep RPM between 97% and 108%
- Maintain airspeed until ground is approached then flare
- Touchdown
Power Failure Below 8ft
- Apply Pedal to stop the yaw
- Allow heli to settle
- Raise collective to cushion the landing
Maximum Glide Distance Configuration
90 kts / 90% RRPM
4.7:1 = 1nm per 1300ft
Minimum Rate of Descent Configuration
55 kts / 90%
4:1 - 1nm per 1500ft
Air Restart Procedure
- Mixture Full Rich
- Throttle - Closed then crack
- Actuate Starter
Emergency Water Landing
Autorotate - unlatch doors prior to water contact
Loss of Tail Rotor Thrust in Forward Flight
Failure indicated by nose yaw right that cannot be stopped by left pedal
- Immediately roll throttle off into overtravel spring
- 70kts
- Raise collective just before touchdown to cushion landing (making sure throttle is in overtravel)
Engine Fire During Start on Ground
- Cranking - Continue and attempt to start
- If engine starts run at 60-70%
- Fuel Mixture - OFF
- Fuel Valve - OFF
- Battery Switch - OFF
- Stop Rotors
- Exit Aircraft
Engine Fire in Flight
- Enter Autorotation!
- Cabin Heat - OFF
- Cabin Vent - ON
- Engine Running - Land
- Engine Stops - Fuel Valve off and complete Autorotation
- Battery Switch - OFF
- Stop Rotors
- Exit Aircraft
Electrical Fire in Flight
- Battery and alternator - OFF
- Open Cabin Vents
- Land Immediately
- Fuel mixture and fuel valve OFF
- Stop Rotors
- Exit Airrcraft
Tachometer Failure
Use remaining Tacho to monitor RPM
If not clear which is malfunctioning , allow governor to control RPM and land as soon as practical
Hydraulic System Failure
- HYD Switch - Confirm ON
- If Hydraulics not restored. HYD Switch - OFF
- Adjust speed and flight condition for control
- Land as soon as practical
Governor Failure
If engine RPM governor malfunctions, grip throttle firmly to override the governor, then switch off governor. Complete rest of flight with manual throttle control
OIL Light
- Loss of engine power or oil pressure
- Check engine tach for power loss
- Check oil pressure gauge and, if pressure loss is confirmed LAND IMMEDIATELY
ENG FIRE Light
- Indicated Possible Fire in Engine Compartment
- Enter Autorotation!
- Cabin Heat - OFF
- Cabin Vent - ON
- Engine Running - Land
- Engine Stops - Fuel Valve off and complete Autorotation
- Battery Switch - OFF
- Stop Rotors
- Exit Aircraft
MR TEMP Light
Indicated Excessive Temp of MR Gearbox
If light is accompanied by any indication of problem such as noise , vibration, or temperature rise - land immediately
If there is no other indication of a problem - land as soon as practical 55kts
MR CHIP Light
Indicates metallic partials in MR Gearbox
If light is accompanied by any indication of problem such as noise , vibration, or temperature rise - land immediately
If there is no other indication of a problem - land as soon as practical 55kts
TR CHIP Light
Indicates metallic partials in TR Gearbox
If light is accompanied by any indication of problem such as noise , vibration, or temperature rise - land immediately
If there is no other indication of a problem - land as soon as practical 55kts
LOW FUEL Light
Indicates 11L of usable fuel remaining
Engine will run out after 10 minutes at cruise
CLUTCH Light
Indicates clutch actuator circuit is on
Light stays on until belts are tensioned
10 seconds or greater - Pull CLUTCH CB and land as soon as practical
Reduce power and land immediately
ALT Light
Indicates low voltage and possible alternator failure
Turn off nonessential electronics then recycle ALT switch
If light stays on, land as soon as practical
Continues flight without alternator can result in tachometer failure
STARTER ON Light
Indicates starter motor is engaged
If light does not go out after button released - PULL MIXTURE OFF and TURN BATTERY OFF
LOW RPM Light
Rotor Speed below 97% RPM
To restore RPM:
- Immediately Lower Collective
- Roll Throttle On
- Apply Aft Cyclic
Light is disabled when collective is fully down
GOV OFF Light
Indicates engine RPM governor is switched off
CARBON MONOXIDE Light
Indicates CO in cabin
Shut off Heater and open nose and door vents
If hovering - Land or transition into forward flight
BRAKE Light
Indicates rotor brake engaged
Release in flight or before starting
FULL THROTTLE Light
Indicates engine near full throttle
The governor will be ineffective because it cannot increase throttle to maintain RPM
Lower collective to extinguish light
HYD Light
Indicates Hydraulic system is switched off
LOW RPM HORN
Horn is provided by speakers in side of instrument console in earlier aircraft and through audio system in later aircraft
Horn activates with the light at 97% RPM
To restore RPM Lower collective, roll throttle on, and apply aft cyclic
Horn and light are disabled when collective is fully down
HIGH RPM WARBLE
On later aircraft a warble (high/low tone) indicates rotor speed approaching 108% RPM Limit. Raise collective to control RPM
Airspeed - Take off and climb
60 kts
Airspeed - Max Rate of Climb (Vy)
55 kts
Airspeed - Max range
100 kts
Airspeed - Max cruise
110 kts (Do not exceed except in smooth air)
Airspeed - Turbulence
60 - 70 kts
Airspeed - Landing Approach
60 kts
Powerplant
Lycoming O-540-F1B5
Normal Rating: 260 BHP @ 2800 RPM
MCP: 205 BHP @ 2718 RPM (102%)
5 Min Take Off: 225 BHP at 2718 RPM
Vne
998kg and below - 130kts over 998 kg - 120 kts Floats armed - 115 kts Autorotation - 100 kts Above MCP - 100 kts Doors off - 100 kts Floats Deployed - 80 kts
Rotor Speed Limits
Power on - 102% - 101%
Power off - 108% - 90%
Powerplant Limits
Engine Speed Max Continuous - 102%
Engine Speed Max Transient - 105%
Max CHT
500 F or 260 C
Max Oil Temp
245 F or 118 C
Oil Pressure Limits
Min Idle - 25 PSI
Min flight - 55 PSI
Max Flight - 95 PSI
Max startup - 115 PSI
Oil Quantity for Take off
7QT minimum
MTOW
1089 kg
Min TOW
703 kg
Max weight per seat (including baggage)
136kg
Max weight baggage compartment
23kg
Minimum Pilot Weight
68kg
Max Density Altitude
14,000ft
Max AGL Altitude
9,000ft (to allow landing in 5 min due fire)
Fuel Capacity
180L Total
176L Usable
Correlator
Prior to autorotation to the ground, ensure to roll throttle into overtravel spring and hold against hard stop until autorotation is complete. This prevents throttle correlator from adding power when collective is raised
Flat Pitch
Checking the manifold pressure before taking off- a higher than normal MAP can indicate a problem ie mag failure or only one mag on
Do hydraulics still work during an engine failure?
Yes - The hydraulic pump is driven by the main rotor gearbox so the actual hydraulic system is independent of the engine.
What do you do if the engine is kicking?
Switch off the governor and head for land / home at 55kts. If it is still kicking after governor is turned off then it could be mags or a stuck valve