EP's Flashcards
Formatted for the written test, not oral knowledge - RFM version 27 deck created 27 OCT 2016
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**
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**
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
ENG FIRE IN FLIGHT
1. OEI flight condition – _________________
2. Airspeed – _____________
3. FIRE sw (affected engine) – _____________
4. BOT 1/BOT 2 pb – _______________
5. Clock stop watch – ________________
6. Affected engine – ________________
7. Single engine emergency shutdown – ______________
8. Passengers – Alert
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
1. Establish
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)
6. Identify
7. Perform
8. Passengers – Alert
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
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
ROTOR RPM
Procedure
NRO low/NRO high
1. Rotor RPM indicator – Check
2. Collective lever – ____________________
ROTOR RPM
2. Collective lever – Adjust as necessary to maintain
NRO within normal range
XMSN OIL T
1. XMSN oil temperature and oil pressure indication
– ___________________ If indications are within limits:
2. LAND AS SOON AS _________________
If indications are above limit:
2. Power – ____________________
If oil temperature indication remains above limit:
3. LAND AS SOON AS ____________________
XMSN OIL T
- *1. Check**
2. PRACTICABLE - *2. Reduce, as much as possible
3. POSSIBLE**
XMSN OIL PRESS
- *If one XMSN oil pressure indication is below 1.0 bar:
1. Power – _____________________**
2. LAND AS SOON AS PRACTICABLE - *If both indications are below 1.0 bar:
3. LAND ______________________**
XMSN OIL PRESS
1. Power – Reduce
3. IMMEDIATELY
ENG CHIP
- *IN FLIGHT
1. OEI flight condition – __________________
2. Affected engine – _________________**
1. Alternative: - *3. Single engine emergency shutdown – ___________**
2. Alternative: - *3. Twist grip (affected engine) – ______________**
ENG CHIP
- *IN FLIGHT
1. Establish
2. Identify**
1. Alternative: - *3. Perform**
2. Alternative: - *3. Rotate slowly to IDLE, check indications**
ENGINE OIL TEMP HIGH
1. OEI flight condition – __________________
2. Affected engine – __________________
3. Twist grip (affected engine) – __________________
4. Oil temperature indicator (affected engine) -__________________
If engine oil temperature decreases below limit:
5. LAND AS SOON AS __________________
If engine oil temperature still remains above limit:
6. Single engine emergency shutdown – __________________
7. LAND AS SOON AS__________________
ENGINE OIL TEMP HIGH
1. Establish
2. Identify
3. Adjust to 20–30% torque (TWIST GRIP caution indication comes on)
4. Monitor
If engine oil temperature decreases below limit:
5. PRACTICABLE
If engine oil temperature still remains above limit:
6. Perform
7. PRACTICABLE
ENG OIL P
- Engine oil pressure – Check
* *2. OEI flight condition – ____________ - Affected engine – ____________
- Single engine emergency shutdown –____________**
- LAND AS SOON AS ___________
ENG OIL P
- Check
* *2. Establish - Identify
- Perform**
- PRACTICABLE
FUEL FILT
One caution indication:
LAND AS SOON AS _____________
CAUTION BE PREPARED FOR SINGLE ENGINE FAILURE.
Both caution indications:
LAND AS SOON AS _____________
CAUTION BE PREPARED FOR DOUBLE ENGINE FAILURE.
FUEL FILT
POSSIBLE
GEN DISCON
1. DC VOLTS, GEN AMPS – ______________
Voltage < 28.2 V or > 28.8 V, Current < 0 A or > 200 A
2. Both BUSTIE sw’s – ____________________
If voltage > 30.5 V:
3. Both GEN sw’s – _______________
4. LAND AS SOON AS _________________
GEN DISCON
- *1. Check**
- *2. OFF both BUSTIE OPN cautions present**
- *3. OFF both GEN DISCON cautions present**
4. PRACTICABLE
GEN OVHT
- Affected GEN sw – OFF
CAUTION IF GEN OVHT CAUTION INDICATION REMAINS ON AND IF THERE ARE INDICATIONS OF A FIRE SUCH AS BURNING ODOR OR SMOKE, SHUT DOWN THE AFFECTED ENGINE.
If GEN OVHT caution indication remains on for more than 1 minute:
**2. OEI flight condition – ____________ - Affected engine – _______________
- Single engine emergency shutdown – __________________**
- LAND AS SOON AS ________________
ENG 1 FAIL or ENG 2 FAIL
- *2. Establish
3. Identify
4. Perform
5. PRACTICABLE**
SEF HOVER/TAKEOFF IGE
1. Collective lever –
2. Landing attitude –
3. Collective lever –
After landing:
4. Affected engine –
5. Single engine emergency shutdown –
SEF HOVER/TAKE OFF IGE
1. Adjust to OEI limits or below
2. Establish
3. Raise as necessary to stop
descent and cushion landing
After landing:
4. Identify
5. Perform
SEF HOVER OGE FORCED LAND
1. Collective lever –
2. Airspeed –
3. Landing attitude –
4. Collective lever –
After landing:
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
After 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 – _____________
7. Affected engine – _____________
8. Single engine emergency shutdown – _____________
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
7. Identify
8. Perform
9. PRACTICABLE
SEF TAKE OFF FLIGHT
- *1. Collective lever – __________________
2. Collective lever –**__________________
3. Rotor speed – __________________
4. Airspeed – __________________
After reaching safe altitude:
5. Collective lever – __________________
6. Affected engine – __________________
7. Single engine emergency shutdown – __________________
8. LAND AS SOON AS __________________
SEF TAKE OFF FLIGHT
- *1. Adjust to maintain rotor RPM
2. Adjust to OEI-limits or below**
3. Trim to maximum
4. Gain, 65 KIAS (VY)
After reaching safe altitude:
5. Reduce to OEI MCP or below
6. Identify
7. Perform
8. 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 ______________
SEF APPROACH
1. Rotor speed – ______________
2. Single engine landing procedure – ______________
After landing:
3. Affected engine – ______________
4. Single engine emergency shutdown – ______________
SEF APPROACH
1. Trim to maximum
2. Perform
After landing:
3.Identify
4. Perform
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 DRIVESHAFT
- *1. OEI flight condition – _____________
2. Affected engine – _____________
3. Single engine emergency shutdown – _______________**
4. LAND AS SOON AS ________________
ENG OVERSPEED DRIVESHAFT
- *1. Establish
2. Identify
3. Perform**
4. PRACTICABLE
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
Compressor Stall
1. Collective lever – ________________
2. Engine instruments – ________________
3. Collective lever – ________________
If compressor stall returns:
4. Affected engine – ________________
5. Single engine emergency shutdown – ________________
6. LAND AS SOON AS ________________
Compressor Stall
1. Lower
2. Monitor
3. Raise slowly
If compressor stall returns:
4. Identify (TOT)
5. Perform
6. PRACTICABLE
Droop Compensation failure
- *1. Collective lever – ______________**
2. LAND AS SOON AS______________
Droop Compensation failure
- *1. Maintain NRO within limits**
2. PRACTICABLE
Double Engine Fail - Hover IGE
- *1. Right pedal – _______________
2. Landing attitude – ________________
3. Collective lever – ______________**
Double Engine Fail - Hover IGE
- *1. Apply as necessary to stop yaw
2. Establish
3. Raise as necessary to cushion landing**
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 – 75 KIAS recommended
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
Cabin Fire
ON GROUND
1. Double engine emergency shutdown –__________
2. Passengers – __________
3. Fire – __________
IN FLIGHT
1. Airspeed – __________
2. Passengers – __________
3. Heating/air conditioning (if installed) – __________
4. Fire – __________
5. Fumes, smoke – __________
6. LAND AS SOON AS__________
After landing:
7. Double engine emergency shutdown –__________
Cabin Fire
ON GROUND
1. Perform
2. Alert/Evacuate
3. Extinguish if possible
IN FLIGHT
1. 65 KIAS recommended
2. Alert
3. OFF
4. Extinguish if possible
5. Eliminate, open sliding doors, windows and vents (fresh air)
6. POSSIBLE
After landing:
7. Perform
Electrical Fire
ON GROUND
- *1. Double engine emergency shutdown – ______________
2. Passengers – ______________
3. EPU, if connected –______________
4. Fire –______________**
IN FLIGHT
- *1. Both BUS TIE sw’s – ______________
2. GEN 1 and GEN 2 sw’s – ______________
3. Electrical consumers – ______________
4. Passengers –**______________
Electrical Fire
- *1. Perform
2. Alert/evacuate
3. Disconnect
4. Extinguish if possible**
IN FLIGHT
- *1. OFF (both BUSTIE OPN cautions present)
2. OFF (both GEN DISCON cautions and BAT DISCH caution present)
3. Reduce as much as possible
4. Alert**
TAIL ROTOR FAILURE HOVER
HOVER IN GROUND EFFECT
1. Both Twist grips – ______________
and simultaneously:
2. Landing attitude – ______________
3. Collective lever – ______________
After landing:
4. Double engine emergency shutdown – ______________
HOVER OUT OF GROUND EFFECT
1. Collective lever – ______________
If height permits:
2. Airspeed – ______________
If height does not permits:
2. Both Twist grips – ______________
3. Collective lever – ______________
After landing:
4. Double engine emergency shutdown –______________
TAIL ROTOR FAILURE HOVER
HOVER IN GROUND EFFECT
1. Rotate to IDLE
and simultaneously:
2. Establish
3. Apply as necessary
After landing:
4. Perform
HOVER OUT OF GROUND EFFECT
1. Reduce as required to stop rotation
If height permits:
2. Gain, then proceed according to para 3.6.2 (Tail Rotor Drive Failure/
Fixed-pitch Tail Rotor Control Failure - Forward Flight)
If height does not permits:
2.Rotate to IDLE
3. Raise to stop descent and cushion landing
After landing:
4. Perform
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
