R22 EP'S EXAM QUESTIONS AND
ANSWERS 100% PASS
A power failure may be caused by - ANS Engine or drive system failure
An engine failure may be indicated by - ANS change in noise level, nose left yaw, oil pressure
light, decreasing engine RPM
Drive system failure may be indicated by - ANS Unusual noise or vibration, noise right or left
yaw, or decreasing rotor RPM while engine RPM is increasing
A power failure will usually be indicated by - ANS the low RPM horn
In case of power failure - ANS Immediately lower collective to enter autorotation
Caution
Aft cyclic is required when - ANS collective is lowered at high speed
Caution
Do not apply aft cyclic during - ANS touchdown or ground slide to prevent possible blade
strike to tailcone
Power failure above 500' AGL - ANS 1.Lower collective to maintain RPM
2.65 knots
1 @COPYRIGHT 2025/2026 ALLRIGHTS RESERVED.
, 3. rpm 97-110 or collective full down if unable
4. Select landing spot, if alt permits manuever into wind
5. Air restart if time permits
6. unnecessary switches and fuel valve off
7. 40 feet begin flare
8. 8 feet level-cushion
Power failure between 8' and 500' AGL - ANS 1. Lower collective to maitain RPM
2. RPM 97-110 or collective full down if unable
3. Maintain AS until ground is approached
4. Cyclic flare to reduce AS and ROD
5. 8' level-cushion
Power failure below 8' AGL - ANS pedal/settle/pull
Max glide - ANS 1.75 Knots/90% RPM
2. 1 NM per 1500' AGL-4:1 glide ratio
Caution
below 500' AGL RPM 97% min
Air restart - ANS 1. Mixture full rich
2. Primer (if installed)-down and locked
3. Throttle-closed then cracked
4. Starter with left hand
Caution
Do not attempt restart if engine malfunction is suspected or before safe auto is established
Emergency water landing power off - ANS 1. same as auto
2 @COPYRIGHT 2025/2026 ALLRIGHTS RESERVED.
ANSWERS 100% PASS
A power failure may be caused by - ANS Engine or drive system failure
An engine failure may be indicated by - ANS change in noise level, nose left yaw, oil pressure
light, decreasing engine RPM
Drive system failure may be indicated by - ANS Unusual noise or vibration, noise right or left
yaw, or decreasing rotor RPM while engine RPM is increasing
A power failure will usually be indicated by - ANS the low RPM horn
In case of power failure - ANS Immediately lower collective to enter autorotation
Caution
Aft cyclic is required when - ANS collective is lowered at high speed
Caution
Do not apply aft cyclic during - ANS touchdown or ground slide to prevent possible blade
strike to tailcone
Power failure above 500' AGL - ANS 1.Lower collective to maintain RPM
2.65 knots
1 @COPYRIGHT 2025/2026 ALLRIGHTS RESERVED.
, 3. rpm 97-110 or collective full down if unable
4. Select landing spot, if alt permits manuever into wind
5. Air restart if time permits
6. unnecessary switches and fuel valve off
7. 40 feet begin flare
8. 8 feet level-cushion
Power failure between 8' and 500' AGL - ANS 1. Lower collective to maitain RPM
2. RPM 97-110 or collective full down if unable
3. Maintain AS until ground is approached
4. Cyclic flare to reduce AS and ROD
5. 8' level-cushion
Power failure below 8' AGL - ANS pedal/settle/pull
Max glide - ANS 1.75 Knots/90% RPM
2. 1 NM per 1500' AGL-4:1 glide ratio
Caution
below 500' AGL RPM 97% min
Air restart - ANS 1. Mixture full rich
2. Primer (if installed)-down and locked
3. Throttle-closed then cracked
4. Starter with left hand
Caution
Do not attempt restart if engine malfunction is suspected or before safe auto is established
Emergency water landing power off - ANS 1. same as auto
2 @COPYRIGHT 2025/2026 ALLRIGHTS RESERVED.
