Short version of EP's for exam Flashcards
ENG 1 FAIL or ENG 2 FAIL
- *1. OEI flight condition – ___________
2. Affected engine – __________
3. Single engine emergency shutdown – ________
4. LAND AS SOON AS ________**
ENG 1 FAIL or ENG 2 FAIL
- *1. Establish
2. Identify
3. Perform
4. PRACTICABLE**
ENG FIRE IN FLIGHT
2. Airspeed – _____________
3. FIRE sw (affected engine) – _____________
4. BOT 1/BOT 2 pb – _______________
5. Clock stop watch – ________________
9. LAND AS SOON AS - _____________
If FIRE warning is still on after 1 minute:
10. BOT 1/BOT 2 pb – ______________
If FIRE warning remains on:
11. LAND - ____________
ENG FIRE IN FLIGHT
2. Reduce if IAS is exceeding 100 kts
3.Raise guard, press
4.Press; bottle 1 activated; – EXT indicator light comes on (EMER OFF SW pnl)
5. Start (after BOT 1 legend and EXT indicator light go off (EMER OFF SW pnl)
9.POSSIBLE
If FIRE warning is still on after 1 minute:
10.Press; bottle 2 activated; – EXT indicator light comes on (EMER OFF SW pnl)
If FIRE warning remains on:
11. LAND IMMEDIATELY
XMSN OIL PRESS
- *1. Power – _____________________**
- *3. LAND ______________________**
XMSN OIL PRESS
- *1. Power – Reduce**
- *3. IMMEDIATELY**
SEF HOVER OGE FORCED LAND
- *1. Collective lever –
2. Airspeed –
3. Landing attitude –
4. Collective lever –** - *5. Affected engine –
6. Single engine emergency shutdown –**
SEF HOVER OGE FORCED LAND
- *1. Adjust to maintain rotor RPM
2. Increase if possible
3. Establish
4. Raise as necessary to stop descent and cushion landing** - *5. Identify
6. Perform**
SEF HOVER OGE TRAN FLIGHT
- *1. Collective lever – _____________
2. Airspeed – _____________**
3. Collective lever – _____________
4. Rotor speed – _____________
5. Airspeed –_____________
After reaching safe altitude:
6. Collective lever – _____________
9. LAND AS SOON AS_____________
SEF HOVER OGE TRAN FLIGHT
- *1. Adjust to maintain rotor RPM
2. Increase if possible**
3. Adjust to OEI-limits or below
4. Trim to maximum
5. Gain, 65 KIAS (VY)
After reaching safe altitude:
6. Reduce to OEI MCP or below
9. PRACTICABLE
SEF FLIGHT
- *1. OEI flight condition – ______________
2. Rotor speed – ______________
3. Affected engine – ______________
4. Single engine emergency shutdown – ______________**
5. LAND AS SOON AS ______________
SEF FLIGHT
- *1. Establish
2. Trim to maximum
3. Identify
4. Perform**
5. PRACTICABLE
SINGLE ENGINE EMERG SHUTDOWN
1. Twist grip (affected engine) – _________________
Bleed air heating (if installed) will be shut down automatically, however, depending on power margin of the remaining engine, may be re–engaged as follows:
2. BLD HTG EMER/NORM sw – _________________
3. BLD HTG rheostat – ________________________
SINGLE ENGINE EMERG SHUTDOWN
1. Rotate slowly to IDLE, check indications, then to OFF
Bleed air heating (if installed) will be shut down automatically, however, depending on power margin of the remaining engine, may be re–engaged as follows:
2. EMER
3. ON
ENG OVERSPEED GOV FAIL
1. Collective lever – ________________
2. VAR NR system NORM/MAN sw – ________________
3. N2 TRIM sw – ________________
If step 3. is not possible:
4. Affected engine – ________________
5. Twist grip (affected engine) – ________________
6. LAND AS SOON AS ________________
ENG OVERSPEED GOV FAIL
1. Raise as necessary to maintain
N2 and NRO within limits
2. Check MAN
3. Try to trim NRO to 101% with matched torque
If step 3. is not possible:
4. Identify
5. Rotate towards IDLE until N2 and NRO stabilize in normal
range and FLI needles match
- PRACTICABLE
ENG UNDERSPEED
1. OEI flight condition – _____________
2. Bleed air consumers – _____________
3. VAR NR system NORM/MAN pb –_____________
4. Affected engine – _____________
5. N2 TRIM sw –_____________
If torque match is not possible:
6. Twist grip (affected engine) –_____________
7. LAND AS SOON AS _____________
If no residual torque (affected engine) is available:
8. Single engine emergency shutdown – _____________
ENG UNDERSPEED
1. Establish
2.Off
3.Check MAN
4. Identify
5.Compensate N2/NRO drop and try to match torque
If torque match is not possible:
6. Release stop plate and rotate towards FLIGHT until N2 and
NRO stabilize in normal range and FLI needles match
7. PRACTICABLE
If no residual torque (affected engine) is available:
8. Perform
Double Engine Emergency Shutdown
ON GROUND
1. Both Twist grips – ______________
2. Both FUEL PRIME PUMP sw – ______________
3. BAT MSTR sw – ______________
IN FLIGHT
1. Both Twist grips – ______________
If there is an indication that the engines are still running:
2. Both EMER OFF sw – ______________
Double Engine Emergency Shutdown
ON GROUND
1. OFF
2. OFF
3. OFF
IN FLIGHT
1.OFF
If there is an indication that the engines are still running:
2.Press
Autorotation
1. Collective lever – ________________
2. Airspeed –_____________________
NOTE Maximum range airspeed 90 KIAS
Minimum rate-of-descent airspeed 60 KIAS
3. Double engine emergency shutdown – _____________
AT APPROXIMATELY 100 FT AGL:
4. Flare attitude – Establish (approx. 15_ to 20_) to reduce
forward speed and rate of descent; control NRO
AT APPROXIMATELY 8 – 12 FT AGL:
5. Flare attitude – Reduce to approx 7 degrees
6. Heading – Maintain
7. Collective lever – Raise to stop descent and cushion landing
8. BAT MSTR sw – _______________
Autorotation
1. Reduce to maintain NRO within limits
2. Airspeed – 75 KIAS recommended
NOTE Maximum range airspeed 90 KIAS
Minimum rate-of-descent airspeed 60 KIAS
3. Perform
AT APPROXIMATELY 100 FT AGL:
4. Flare attitude – Establish (approx. 15_ to 20_) to reduce
forward speed and rateof descent; control NRO
AT APPROXIMATELY 8 – 12 FT AGL:
5. Flare attitude – Reduce to approx 7_
6. Heading – Maintain
7. Collective lever – Raise to stop descent and cushion landing
8. OFF
TAIL ROTOR FAIL FLIGHT
1. Collective lever – ____________________
2. Airspeed – ____________________
3. Suitable landing area – ____________________
NOTE D Landing surface should be hard (e.g. concrete, asphalt) and flat.
D Left crosswind is advantageous
4. Shallow approach with nose left – ____________________
<u>If the airspeed can be reduced below 40 kts with the nose still pointing to the left:</u>
5. Airspeed –____________________
6. Landing – ____________________
<u>If the nose direction changes from left to right at airspeeds higher than 40 kts:</u>
5. Airspeed – ____________________
6. Approach – ____________________
7. Autorotation – ____________________
TAIL ROTOR FAIL FLIGHT
1. Reduce to obtain minimum sideslip angle
2. Maintain 70 KIAS or higher
3. Select
<u>NOTE D Landing surface should be hard (e.g. concrete, asphalt) and flat. Left crosswind is advantageous</u>
4. Perform
<u>If the airspeed can be reduced below 40 kts with the nose still pointing to the left:</u>
5. Reduce close to the ground until nose is aligned with the flight direction
6. Perform
<u>If the nose direction changes from left to right at airspeeds higher than 40 kts:</u>
5. Increase
6. Abort, climb to sufficient height for autorotation
7. Perform
BAT
TEMP
ON GROUND
1. BAT MSTR sw – _ _ _
IN FLIGHT
– Single pilot operation:
1. BAT MSTR sw – _ _ _
2. LAND AS SOON AS ______
– Dual pilot operation:
1. BAT MSTR sw – _ _ _
2. LAND AS SOON AS ________
BAT
TEMP
ON GROUND
1. OFF
IN FLIGHT
– Single pilot operation:
1. OFF
2. POSSIBLE
– Dual pilot operation:
- *1. OFF
2. POSSIBLE**
FIRE - ON GROUND
- *ON GROUND
1. FIRE sw (affected engine) – _____________
2. Both FUEL PRIME PUMPS – ____________
3. BOT 1/BOT 2 pb – _________________** - *__________________________________**
- *4. Clock stop watch –____________
5. Double engine emergency shutdown –**
6. Passengers – Alert/Evacuate
7. BOT 1/BOT 2 pb – _________________
- *__________________________________**
8. BAT MSTR sw – OFF
FIRE - ON GROUND
1. Raise guard, press
2. Check OFF
3.Press; bottle 1 activated;
EXT indicator light comes on
(EMER OFF SW pnl)
4. Start (after BOT 1 legend and
EXT indicator light go off
(EMER OFF SW pnl)
5. Perform
6. Passengers – Alert/Evacuate
7. Press; bottle 2 activated;
EXT indicator light comes on
(EMER OFF SW pnl)
- BAT MSTR sw – OFF
LOW FUEL
- Fuel quantity indication – Check
If positive fuel indication in the main tank: - Both fuel pump XFER sw (Fwd + Aft) – Check ON
- Both fuel pump XFER circuit breakers
(Fwd + Aft)
– Check in
If both FUEL LOW warning lights remain on:
4. ______________________
If one FUEL LOW warning light remains on:
4. ______________________
LOW FUEL
4. LAND WITHIN 10 MINUTES
4. Expect single engine failure
