Use LEFT and RIGHT arrow keys to navigate between flashcards;
Use UP and DOWN arrow keys to flip the card;
H to show hint;
A reads text to speech;
23 Cards in this Set
- Front
- Back
- 3rd side (hint)
SINGLE ENGINE FAILURE |
- ENG FAIL warning light and gong
- ENG SPLIT caution - ENG OIL P caution - FUEL PESS caution - GEN DISCON caution - OVSP FAIL caution - VAR NR caution - NORM/MAN pb to MAN - Instruments indicate power loss |
<b><color red>1. Collective lever - Adjust to OEI limits or below
2. Landing attitude - Establish 3. Collective lever - Raise as necessary to stop descent and cushion landing</b></color> <i>after landing <b><color red>4. Affected Engine - Identify 5. single engine emergency shutdown - Perform |
|
SINGLE ENGINE FAILURE
<b>HOGE</b> |
- ENG FAIL warning light and gong
- ENG SPLIT caution - ENG OIL P caution - FUEL PESS caution - GEN DISCON caution - OVSP FAIL caution - VAR NR caution - NORM/MAN pb to MAN - Instruments indicate power loss |
<b><color red>
1. Collective lever - Adjust too maintain Rotor RPM 2. Airspeed - Increase if possible</color> Forced Landing: <color red>3. Landing attitude - Establish 4. Collective lever - Raise as necessary to stop descent and cushion landing</b></color> <i>after landing:</i> <b><color red>5. affected Engine - Identify 6. Single engine emergency shutdown - Perform</color> Transition to OEI-flight: <color red>3. Collective lever - Adjust to OEI-limits or below 4. Rotor speed - Trim to maximum 5. Airspeed - Gain, 65 KIAS (Vy)</b></color> <i>after reaching safe altitude</i> <b><color red>6. Collective lever Reduce to OEI MCP or below 7. Affected engine - Identify 8. single engine emergency shutdown - Perform</b></color> 9. Land ASAPracticable |
|
SINGLE ENGINE FAILURE
<b>TAKEOFF</b> |
- ENG FAIL warning light and gong
- ENG SPLIT caution - ENG OIL P caution - FUEL PESS caution - GEN DISCON caution - OVSP FAIL caution - VAR NR caution - NORM/MAN pb to MAN - Instruments indicate power loss |
<b><color red>
1. Collective lever - Adjust too maintain Rotor RPM</color> Rejected Takeoff:<color red> 2. Landing attitude - Establish 3. Collective lever - Raise as necessary to stop descent and cushion landing</b></color> <i>after landing:</i> <b><color red>4. affected Engine - Identify 5. Single engine emergency shutdown - Perform</color> Transition to OEI-flight:<color red> 2. Collective lever - Adjust to OEI-limits or below 3. Rotor speed - Trim to maximum 4. Airspeed - Gain, 65 KIAS (Vy)</b></color> <i>after reaching safe altitude:</i> <b><color red>5. Collective lever - reduce to OEI-MCP or below 6. Affected engione - Identify 7. Single engine emergency shutdown - Perform</b></color> 8. Land ASAPracticable |
|
SINGLE ENGINE FAILURE
<b>FLIGHT</b> |
- ENG FAIL warning light and gong
- ENG SPLIT caution - ENG OIL P caution - FUEL PESS caution - GEN DISCON caution - OVSP FAIL caution - VAR NR caution - NORM/MAN pb to MAN - Instruments indicate power loss |
<b><color red>1. OEI flight condition - Establish
2. Rotor speed - Trim to maximum 3. Affected engine - Identify 4. Single engine emergency shutdown - Perform</b></color> 5. Land ASAPracticable |
|
SINGLE ENGINE FAILURE
<b>APPROACH</b> |
- ENG FAIL warning light and gong
- ENG SPLIT caution - ENG OIL P caution - FUEL PESS caution - GEN DISCON caution - OVSP FAIL caution - VAR NR caution - NORM/MAN pb to MAN - Instruments indicate power loss |
<b><color red>1. Rotor speed - Trim to maximum
2. Affected engine - Identify 3. Single engine emergency shutdown - Perform 4. Singke engine landing procedure - Perform</b></color> |
|
SINGLE ENGINE LANDING
|
OEI
|
<b>Landing Approach:</b>
1. Rotor speed - Check maximum 2. Bleed air heating - Check off 3. Airspeed - 65 KIAS (Vy) 4. Shallow approach - Establish <b>On Final, at 50ft AGL:</b> 5. Airspeed - 40 KIAS 6. Rate of descent - max 500ft/min <b>Touchdown:</b> 7. airspeed - Reduce to minimum 8. Landing attitude - Establish 9. Collective lever - Raise as necessary to stop descent and cushion landing <b>After landing:</b> 10. Collective lever - Lower slowly 11. Cyclic stick - maintain neutral position |
|
SINGLE ENGINE EMRGENCY SHUTDOWN
|
- VAR NR to manual mode automatically
- make sure that the correct engine is selected - the collective lever is adjusted to OEI limits for normal engine |
<b><color red>1. Twist grip 8affected engine) - Rotate slowly to IDLE, check indications, then to OFF</b></color>
<i>bleed heating will be shut down automatically, if needed....</i> 2. BLD HTG EMER/NORM sw - EMER 3. BLD HTG rheostat - ON |
|
INFLIGHT RESTART
|
- if OVSP FAIL caution indication of the affected engine is <b>not</b> on an restart is not possible due to Overspeed protection shutdown
|
1. Collective lever - Adjust to OEI MCP or below
2. Collective lever friction - Adjust to maintain position of lever 3. Electriocal consumption - Reduce 4. FUEL PRIME PUMP sw (aff. engine) - ON <i>after 10 seconds</i> 5. Twist grip - preselect 20° (hot engine 18°) 6. Normal engine starting procedure - Perform 7. Twist grip 8aff. engine) - Increase to FLIGHT position 8. Electrical consumers - As required 9. FUEL PRIME PUMP sw - OFF <i>if restart ot successfull</i> 10. Land ASAPracticable |
|
ENGINE OVERSPEED
<b>DRIVESHAFT FAILURE</b> |
- VAR NR caution
- NRO decrease <i>affected engine:</i> - ENG SPLIT caution - Torque decreases to zero - N1 decreases - N2 increases above NRO and either: - drops back to 100% or below, or - increases to 123,1% causing overspeed protection to shutdown engine <i>normal engine:</i> - Torque, N1 , TOT increase - N2 decreases |
<b><color red>1. OEI flight condition - Establish
2. Affected engine - Identify 3. Single engine emergency shutdown - Perform</b></color> 4. Land ASAPracticable |
|
ENGINE OVERSPEED
<b>GOVERNOR FAILURE</b> |
- ROTOR RPM warning
- VAR NR caution - ENG SPLIT caution - NRO and both N2 increase <i<affected engine:</i> - Torque, TOT, N1 increase <i>normal engine:</i> - Torque and TOT may decrease |
<b><color red>1. Collective lever - Raise as necessary to maintain Rotor RPM and N2 within limits
2. VAR NR system NORM/MAN sw - Check MAN 3. N2 trim sw - Try to trim NRO to 101% with matched torque</b></color> <i>if step 3. ist not possible:</i> 4. affected engine - Identify 5. Twist grip (aff engine) - Rotate slowly to IDLE until N2 and NRO stabilize in normal range an FLI needles match</b></color> 6. Land ASAPracticable |
|
ENGINE UNDERSPEED
<b>GOVERNOR FAILURE</b> |
- ROTOR RPM warning
- VAR NR caution - ENG SPLIT caution <i>affected engine:</i> - Torque, N1, N2TOT may decrease <i>normal engine:</i> - NRO and N2 may decrease |
<b></color red>1. OEI flight condition - Establish
2. Bleed air consumers - Off 3. VAR NR NORM/MAN pb - check MAN 4. Affected engine - Identify 5. N2 trim sw - Compensate N2/NRO drop and try to match torque</b></color> <i>if torque match not possible:</i> <b><color red>6. Twist grip (affected engine) - Release stop plate and rotate towards FLIGHT until N2 and NRO stabilize in normal range and FLI needles match</b></color> 7. Land ASAPracticable <i>if no residual torque is available</i> <b><color red>8. Single engine emergency shutdown - Perform</b></color> <i>after landing rotate to IDLE prior lowering collective</i> |
|
COMPRESSOR STALL
|
- popping sounds
- Torque and N1 may decrease - TOT may increase - Slight yaw jerk |
<b><color red>1. Collective lever - Lower
2. Engine instruments - Monitor 3. Collective leverv - Raise slowly</b></color> <i>if compressor stall returns</i> <b><color red>4. Affected engine - Identify 5. Single engine emergency shutdown - Perform</b></color> 6. Land ASAPracticable |
|
DROOP COMPENSATION FAILURE
|
- NRO and both N2 decrease when collective is raised
- NRO and both N2 increase when collective lever is lowered |
<b><color red>1. Collective lever - Maintain NRO within limits</b></color>
2. Land ASAPracticable |
|
ENGINE OIL TEMPERATURE HIGH
|
oil temperature above limits
|
<b><color red>1. OEI flight conditions - Establish
2. Affected engine - Identify 3. Twist grip (aff. engine) - Adjust to 20-30% torque (TWIST GRIP caution comes on) 4. Oil temperature indicator - Monitor</b></color> <i>if engine oil temperature decreases below limit:</i> 5. Land ASAPracticable <i>if eng oil temp remains above limit:</i> <b><color red>6. Single engine emergency shutdown - Perform</b></color> 7. Land ASAPracticable |
|
DOUBLE ENGINE FAILURE
<b>HIGE</b> |
- yawing nose left
- NRO and N2 decrease - ROTOR RPM warning - ENG FAIL warning - ENG OIL P caution - FUEL PRESS caution - GEN DISCON caution - engine instuments indicate power loss |
<b><color red>1. Right pedal - Apply as necessary to stop yaw
2.Landing attitude - Establish 3. Collective lever - Raise as necessary to stop descent and cushion landing </b></color> |
|
DOUBLE ENGINE FAILURE
<b>FLIGHT</b> |
- yawing nose left
- NRO and N2 decrease - ROTOR RPM warning - ENG FAIL warning - ENG OIL P caution - FUEL PRESS caution - GEN DISCON caution - engine instuments indicate power loss |
<b><color red>Autorotation - Perform
</b></color> |
|
DOUBLE ENGINE EMERGENCY SHUTDOWN
|
blank
|
<b>On ground:<color red>
1. Both twist grips - Off 2. Both FUEL PRIME PUMP sw - Off 3. BAT MSTR sw - Off</color> In flight:<color red> 1. Both twist grips - Off</b></color> <i>if there is an indication that engines are still running:</i> <b><color red>2. Both EMER OFF sw - Press </b></color> |
|
AUTOROTATION
|
Max range airspeed - 90 KIAS
Minimum rate of descent airspeed - 60 KIAS |
<b><color red>1. Collective lever - Reduce to maintain NRO within limits
2. Airspeed - 75 KIAS recommended 3. Double engine emergency shutdown - Perform</b></color> <i>at approx. 100ft AGL:</i> 4. Flare attitude - Establish (approx. 15° to 20°) to reduce forward speed and rate of descent <i>at approx. 8-12 ft AGL:</i> 5. Flare attitude - Reduce to approx. 7° 6. Heading - Maintain 7. Collective lever - Raise to stop descent and cushion landing <b><color red>8. BAT MSTR sw - Off </b></color> |
|
CABIN FIRE
|
smoke, flames, burning odor
|
<b>On ground:<color red>
1. Double engine emergency shutdown - Perform 2. Passengers - Alert/Evacuate 3. Fire - Extinguish if possible</color> In flight:<color red> 1. Airspeed - 65 KIAS recommended 2. Passengers - Alert 3. Heating/air conditioning - Off 4. Fire - Extinguish if possible 5. Fumes, smoke - Eliminate, open sliding doors and vents 6. Land ASAP</b></color> <i>after landing:</i> <b><color red>7. Double engine emergency shutdown - Perform</b></color> |
|
ELECTRICAL FIRE / SHORT CIRCUIT
|
odor of burning isolation and / or acrid smoke
|
<b>On ground:<color red>
1. Double engine emergency shutdown - Perform 2. Passengers - Alert/evacuate 3. EPU, if connected - Disconnect 4. Fire - Extinguish if possible</color> In flight:<color red> 1. GEN 1sw and GEN 2 sw - Off 2. Heating / Ventilation - Off 3. Passengers - Alert</b></color> |
|
TAIL ROTOR DRIVE FAILURE
<b>HOVER</b> |
- complete loss of tail rotor thrust
- yawing motion to the right depending on actual power setting |
<b>Hover IGE:<color red>
1. Both twist grips - Rotate to idle</b></color> <i>and simultaneously:</i><color red> 2. Landing attitude - Establish 3. Collective lever - Apply as necessary</color></b> <i>After landing:</i> <b><color red>4. Double engine emergency shutdown - Perform</color> Hover OGE:<color red> 1. Collective lever - Reduce as required to stop rotation</color></b> If height permits:<b><color red> 2. Airspeed - Gain</color></b> If height does not permit:<b><color red> 2. Both twist grips - Rotate to IDLE 3. Collective lever - raise to stop descent and cushion landing </color></b> After landing:<b><color red> 4. Double engine emergency shutdown |
|
TAIL ROTOR DRIVE FAILURE
FIXED PITCH TAIL ROTOR CONTROL FAILURE <b>FORWARD FLIGHT</b> |
- no directional repsonse
- complete loss of tail rotor thrust - locked pedals |
<b><color red>1. Collective lever - Reduce to obtain minimum sideslip angle
2. Airspeed - Maintain 70 KIAS or higher</b></color> 3. Suitable landing area - Select <i>-left crosswind is advantegeous-</i> <b><color red>4. Shallow approach with nose left - Perform</b></color> <i>if the airspeed can be reduced below 40 kts with the nose pointing left:</i> <b><color red>5. Airspeed - Reduce close to the ground until nose is alligned with flight direction 6. Landing - Perform</b></color> <i>if the nose direction changes from left to right at airspeeds higher 40kts:</i> <b><color red>5. Airspeed - Increase 6. Approach - Abort, climb to sufficient height for autorotation 7. Autorotation - Perform </b></color> |
|
PEDAL VIBRATIONS
|
unusual pedal v ibrations
|
<b><color red>Land ASAP
</b></color> |