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35 Cards in this Set

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Definitions: Land Immediately
Land on the nearest clear area where a safe normal landing can be performed. Be prepared to enter autorotaion during the approach, if required.
POH 3-1
Definitions: Land as soon as practical
Land at the nearest airport or other facility where emergency maintenance may be performed.
POH 3-1
Power failure causes and indications
May be caused by either an engine or drive system failure and will usually be indicated by the low RPM horn.
POH 3-1
Engine Failure indications
May be indicated by a change in noise level, nose left yaw, oil pressure light, or decreasing engine RPM.
POH 3-1
Drive system failure indications
May be indicated by an unusual noise or vibration, nose right or left yaw, or decreasing rotor RPM wile engine RPM is increasing.
POH 3-1
Emergency Procedures:
Ditching - Power Off
1.
2.
3.
1 Follow same procedures as for power failure over land until contacting water.
2. Apply lateral cyclic when aircraft contacts water to stop blades from rotating.
3. Release seat belt and quickly clear aircraft when blades stop rotating.
POH 3-4
Emergency Procedures:
Ditching - Power On
1.
2.
3.
4.
5.
6.
7.
8.
9.
1. Descend to hover above water.
2. Unlatch doors.
3. Passenger exit aircraft.
4. Fly to safe distance from passenger to avoid possible injury by blades.
5. Switch off battery and alternator.
6. Roll throttle off unto overtravel spring.
7. Keep aircraft level and apply full collective as aircraft contacts water.
8. Apply left lateral cyclic to stop blades from rotating.
9. Release seat belt and quickly clear aircraft when blades stop rotating.
POH 3-4
Emergency Procedures:
Loss of tail rotor thrust during forward flight
1.
2.
3.
4.
1. Immediately enter autoration.
2. Maintain at least 70 KIAS airspeed if practical.
3. Select landing site,
4. Roll throttle off into overtravel spring and perform autorotation landing.
POH 3-5
Emergency Procedure:
Loss of tail rotor thrust during hover
1. Immediately roll throttle off into overtravel spring and allow aircraft to settle.
2. Raise collective just before touchdown to cushion landing.
POH 3-5
Emergency Procedure:
Engine fire during start on ground
1. Cranking - Continue and attempt to start which would suck flames and excess fuel through carburetor into engine.
2. If engine starts, run at 50-60% RPM for a short time, shut down, and inspect for damage.
3. If engine fails to start, shut off fuel and master battery switch.
4. Extinguish fire with fire extinguisher, wool blanket, or dirt.
5. Inspect for damage.
POH 3-6
Emergency Procedure:
Fire in flight - Non electrical
1.
2.
3.
4.
5.
6.
1. Enter Autorotation.
2. master battery switch - Off (if time permits)
3. Cabin heat - Off (if installed and time permits).
4. Cabin vent - On (if time permits).
5. If engine is running, perform normal landing and immediately shut off fuel valve.
6. If engine stops running, shut off fuel valve and execute autorotation landing.
POH 3-6
Emergency Procedure:
Electrical fire in flight
1.
2.
3.
4.
1. Master battery switch - Off
2. Alt switch - Off.
3. Land immediately.
4. Extinguish fire and inspect for damage.
POH 3-6
Caution: When is the low RPM warning system and governor inoperative?
When the master battery and alternator switches are both off.
POH 3-6
Tachometer failure
If rotor or engine tach malfunctions in flight, use remaining tach to monitor RPM.

If it is not clear which tach is malfunctioning or if both tachs malfunction, allow governor to control RPM and land as soon as practical.
POH 3-7
Governor failure
Grip throttle firmly to override the governor,
then switch governor off.
Complete flight using manual throttle control.
POH 3-7
Warning/Caution Lights:
Oil
Indicates 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. continued operation without oil pressure will cause serious engine damage and engine failure may occur.
POH 3-8
Warning/Caution Lights:
MR (Main Rotor) Temp
Indicates excessive temperature of main rotor gearbox.

Note: If light is accompanied by any indication of a problem such as noise, vibration, or temperature rise, land immediately. If there is no other indication of a problem, land as soon as practical.
POH 3-8
Warning/Caution Lights:
MR (Main Rotor) Chip
Indicates metallic particles in main rotor gearbox.

Note: If light is accompanied by any indication of a problem such as noise, vibration, or temperature rise, land immediately. If there is no other indication of a problem, land as soon as practical.
POH 3-81
Warning/Caution Lights:
TR (Tail Rotor) Chip
Indicates metallic particles in tail rotor gearbox.

Note: If light is accompanied by any indication of a problem such as noise, vibration, or temperature rise, land immediately. If there is no other indication of a problem, land as soon as practical.
POH 3-8
Warning/Caution Lights:
Low Fuel
Indicates approximately one gallon of usable fuel remaining. The engine will run out of fuel after five minutes at cruise power.
POH 3-9
Caution: T/F you can use Low Fuel light as a working indication of fuel quantity?
False - DO NOT use Low Fuel warning light as a working indication of fuel quantity.
POH 3-9
Warning/Caution Lights:
Clutch
Indicates that clutch actuator circuit is on, either engaging or disengaging the clutch.

When the switch is in the engage position, the light stays on until the belts are properly tensioned.

Never take off before the light goes out.
POH 3-9
If clutch light flickers or comes on in flight and doesn't go out within 10 seconds what do you do?
Pull the clutch circuit breaker, land as soon as practical. Reduce power and land immediately if there are any other indications of drive system failure. (Be prepared to enter autorotation.) Inspect drive system for a possible malfunction.
POH 3-9
Warning/Caution Lights:
ALT
Indicates low voltage and possible alternator failure. Turn off nonessential electrical equipment and switch ALT off and back on after one second to reset over voltage relay. If light stays on, land as soon as practical. continued flight without functioning alternator can result in loss of electronic tachometer, producing a hazardous flight condition.
POH 3-9
Warning/Caution Lights:
Brake
Indicates rotor brake is engaged. Release immediately in flight or before starting engine.
POH 3-10
Warning/Caution Lights:
Starter-On
Indicates starter motor is engaged. If light does not go out when ignition switch is released from start position, immediately pull mixture to idle cut-off and turn master switch off. have starter motor serviced.
POH 3-10
Warning/Caution Lights:
Carbon Monoxide (if Installed)
Indicates elevated levels of carbon monoxide (CO) in cabin. Open nose and door vents and shut off heater. If hovering, land or transition to forward flight.

If symptoms of CO poisoning (headache, drowsiness, dizziness) accompany light, land immediately.
POH 3-10
Warning/Caution Lights:
Low RPM Horn & Light
A horn and an illuminated caution light indicate that rotor RPM may be below safe limits. To restore RPM, immediately roll throttle on, lower collective and, in forward flight, apply aft cyclic. Horn and caution light are disabled when collective is full down.
POH 3-10
Emergency Procedure:
Right roll in low "G" condition
Gradually apply aft cyclic to restore positive "G" forces and main rotor thrust.
Do not apply lateral cyclic until positive "G" forces have been established.
POH 3-11
Emergency Procedure:
Uncommanded pitch, roll, or yaw resulting from flight in turbulence.
-Gradually apply controls to maintain rotor RPM, positive "G" forces, and to eliminate side-slip.
-Minimize cyclic positive inputs in turbulence: do not over-control.
POH 3-11
Emergency Procedure:
Inadvertent encounter with moderate, severe, or extreme turbulence.
If the area of turbulence is isolated, depart the area; otherwise, land the helicopter as soon as practical. Adjust forward airspeed to 60 KIAS and .7 Vne but no slower than 57 KIAS.
POH 3-11
BII:

0-360-J.2A

Powerplant of an R22
O - opposed 4 cylinders

360 - cubic inches

J.2A - type
SHUT DOWN checklist
Collective - Full down
Cyclic, pedals - Neutral
Governor - Off
Idle at 75% - Note time
Frictions - On
Cylinder head temperature - Plateau in drop, 2 minute min.
Throttle - Closed
Clutch switch - Disengaged
Wait 30 seconds - Pull idle cut-off
Mixture guard - Back on mixture
Wait 30 seconds - Apply rotor brake
Clutch light - All switches, mags off
Post flight - Walk around inspection
Which electrical equipment would you consider "non-essential"?
GPS, etc. Keep radio, and nav lights on.
With the master battery and alternator off, which avionics become inoperative?
GOVERNOR and LOW RPM WARNING SYSTEM - be careful of RPM!