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37 Cards in this Set
- Front
- Back
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BAT TEMP |
1. BAT MSTR switch - OFF 2. Land as soon as possible |
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ENG 1/2 FAIL |
1. OEI flight condition - Establish 2. Affected engine - Identify 3. Single engine emergency shutdown - Perform |
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FIRE on ground |
1. FIRE switch (affected engine) - Raise guard, press 2. Both FUEL PRIME PUMPS - Check OFF 3. BOT 1/BOT 2 push button - Press; bottle 1 activated; EXT indicator light comes on (EMER OFF SW panel) 4. Clock stop watch - Start (after BOT 1 legend and EXT indicator light go off) 5. Double engine emergency shutdown - perform If situation permits and FIRE warning is still on after 1 minute: 7. BOT 1/BOT 2 push button - Press; bottle 2 activated; EXT indicator light comes on (EMER OFF SW panel) |
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FIRE in flight |
1. OEI flight condition - Establish 2. Airspeed - Max 100 KIAS 3. FIRE switch (affected engine) - raise guard; press 4. BOT 1/BOT 2 push button - Press; bottle 1 activated; EXT indicator light comes on (EMER OFF SW panel) 5. Clock stop watch - Start (after BOT 1 legend and EXT indicator light go off) 6. Affected engine - Identify 7. Single engine emergency shutdown - perform 9. Land as soon as possible If FIRE warning is still on after 1 minute 10. BOT 1/BOT 2 push button - Press; bottle 2 activated; EXT indicator light comes on (EMER OFF SW panel) If FIRE warning remains on 11. Land Immediately |
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ROTOR RPM |
1. Collective lever - adjust as necessary to maintain Nro within normal range. |
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XSM OIL PRESS |
If one XMSN oil pressure indication is below 1.0 bar: 1. Power - reduce 2. Land as soon as practicable If both XSM oil pressure indications are below 1.0 bar: 3. Land Immediately |
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ENG OIL P (system 1 or 2) |
2. OEI flight condition - Establish 3. Affected engine - Identify 4. Single engine emergency shutdown - Perform |
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GEN DISCON (System 1 or 2) |
1. DC VOLTS, GEN AMPS - Check If voltage <28.2 V or >28.8V, Current < 0 A or >200 A: 2. Both BUSTIE switches - OFF (both BUSTIE OPN cautions present) If voltage > 30.5 V: 3. Both GEN switches - OFF (both GEN DISCON cautions present) |
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GEN DISCON (System 1 and 2) |
1. GEN AMPS - Check If GEN AMPS < 0A: 2. Both BUSTIE switches - OFF (both BUSTIE OPN cautions present) |
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GEN OVHT (system 1 or 2) |
If GEN OVHT caution remains on for more than 1 min: 2. OEI Flight condition - establish 3. Affected engine - Identify 4. Single engine emergency shutdown - Perform |
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Single engine failure - HIGE |
1. Collective level - Adjust to OEI limits or below 2. Landing Attitude - Establish 3. Collective lever - Raise as necessary to stop descent and cushion landing After Landing: 4. Affected engine - Identify 5. Single engine emergency shutdown - perform |
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Single engine failure - HOGE |
1. Collective lever - Adjust to maintain rotor RPM 2. Airspeed - Increase if possible Forced Landing: 3. Landing attitude - Establish 4. Collective lever - Raise as necessary to stop descent and cushion landing After Landing: 5. Affected Engine - Identify 6. Single engine emergency shutdown - perform Transition to OEI Flight: 3. Collective lever - Adjust to OEI limits or below 4. Rotor Speed - Trim to maximum 5. Airspeed - Gain, 65 KIAS (Vy) After reaching safe altitude: 6. Collective lever - Reduce to OEI MCP or below 7. Affected engine - Identify 8. Single engine emergency shutdown - Perform |
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Single engine failure - Takeoff |
1. Collective lever - Adjust to maintain rotor RPM Rejected Takeoff: 2. Landing attitude - Establish 3. Collective lever - Raise as necessary to stop descent and cushion landing After landing: 4. Affected engine - Identify 5. Single engine emergency shutdown - perform Transition to OEI Flight: 2. Collective lever - Adjust to OEI limits or below 3. Rotor speed - Trim to maximum 4. Airspeed - Gain, 65 KIAS (Vy) After reaching safe altitude: 5. Collective lever - reduce to OEI MCP or below 6. Affected engine - Identify 7. Single engine emergency shutdown - Perform |
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Single engine failure - Flight |
1. OEI flight condition - establish 2. Rotor Speed - trim to maximum 3. Affected engine - Identify 4. Single engine emergency shutdown - Perform |
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Single engine failure - Approach |
1. Rotor speed - Trim to maximum 2. Single engine landing procedure - Perform After landing: 3. Affected engine - Identify 4. Singl engine emergency shutdown - Perform |
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Single engine emergency shutdown |
1. Twist grip (affected engine) - Rotate slowly to IDLE, check indications, then to OFF 2. Rotor Speed - Trim to maximum |
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Engine Overspeed (Driveshaft failure) |
1. OEI flight condition - Establish 2. Affected engine - Identify 3. Single engine emergency shutdown - Perform |
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Engine Overspeed (Governor Failure) |
1. Collective lever - Raise to maintain N2 and Nro within limits 2. VAR NR system NORM/MAN switch - Check MAN 3. N2 TRIM switch - Try to trim Nro to 101% with matched torque If step 3 is not possible: 4. Affected engine - Identify 5. Twist grip (affected engine) - Rotate towards IDLE until N2 and Nro stabilize in normal range and FLI needles match |
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Engine Underspeed (Governor Failure) |
1. OEI Flight Condition - Establish 2. Bleed air consumers - Off 3. VAR Nr system NORM/MAN switch - Check MAN 4. Affected engine - Identify 5. N2 TRIM switch - Compensate N2/Nro droop and try to match torque If torque match is not possible: 6. Twist grip (affected engine) - Release stop and rotate towards FLIGHT until N2 and Nro stabilize in normal range and FLI needles match If no residual torque (affected engine) is available: 8. Single engine emergency shutdown - Perform |
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Compressor Stall |
1. Collective lever - Lower 2. Engine instruments - Monitor 3. Collective lever - Raise slowly If compressor stall returns: 4. Affected engine - Identify (TOT) 5. Single engine emergency shutdown - Perform |
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Droop Compensation Failure |
1. Collective lever - Maintain Nro within limits |
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Engine Oil Temp High |
1. OEI flight condition - Establish 2. Affected engine - Identify 3. Twist grip (affected engine) - Adjust to 20-30% torque 4. Oil temperature indicator (affected engine) - Monitor If oil temp remains above limit: 6. Single engine emergency shutdown - Perform |
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Double Engine Failure (HIGE) |
1. Right pedal - Apply as necessary to stop yaw 2. Landing attitude - Establish 3. Collective lever - Raise as necessary to cushion landing |
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Double engine failure (Flight) |
1. Autorotation - Perform |
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Double engine emergency shutdown |
On Ground: 1. Both twist grips - OFF 2. Both fuel prime pumps - OFF 3. BAT MSTR switch - OFF In Flight: 1. Both twist grips - OFF If there is an indication that the engines are still running: 2. Both EMER OFF switches - Press |
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Autorotation |
1. Collective lever - Reduce to maintain Nro within limits 2. Airspeed - 75 KIAS recommended (60 min RoD; 90 max range) 3. Double engine emergency shutdown - perform .... 8. BAT MSTR switch - OFF |
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Cabin Fire |
On Ground: 1. Double engine emergency shutdown - Perform 2. Passengers - Alert/evacuate 3. Fire - Extinguish if possible In flight: 1. Airspeed - 65 KIAS recommended 2. Passengers - Alert 3. Heating/air conditioning - OFF 4. Fire - Extinguish if possible 5. Fumes, smoke, fire extinguishing fumes/gas - Eliminate, open doors, windows, and vents (fresh air) 6. Land as soon as possible After Landing: 7. Double engine emergency shutdown - Perform |
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Electrical Fire/Short Circuit (On Ground) |
1. Double engine emergency shutdown - perform 2. Passengers - Alert/Evacuate 3. EPU, if connected - Disconnect 4. Fire - Extinguish if possible |
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Electrical Fire/Short Circuit (In Flight) |
1. Both BUSTIE switches - OFF (both BUSTIE OPN cautions present) 2. GEN 1 and 2 switches - OFF (both GEN DISCON cautions and BAT DISCH cautions present) 3. Electrical Consumers - Reduce as much as possible 4. Passengers - ALERT |
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Tail Rotor Drive Failure (Hover) |
In Ground Effect: 1. Both twist grips - Rotate to IDLE and simultaneously 2. Landing attitude - Establish 3. Collective lever - Apply as necessary After landing: 4. Double engine emergency shutdown - Perform Out of Ground Effect: 1. Collective lever - Reduce as required to stop rotation If height permits: 2. Airspeed - Gain, the proceed with fwd flight EP If height does not permit: 2. Both twist grips - Rotate to IDLE 3. Collective lever - Raise to stop descent and cushion landing After landing: 4. Double engine emergency shutdown - Perform |
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Tail Rotor Drive Failure (Forward Flight) |
1. Collective lever - Reduce to obtain minimum sideslip angle 2. Airspeed - Maintain 70 KIAS or higher 4. Shallow approach with nose left - Perform If airspeed can be reduced below 40 kts with nose still pointing left: 5. Airspeed - Reduce close to ground until nose is aligned with flight direction 6. Landing - Perform If nose direction changes from left to right at airspeeds higher than 40 kts: 5. Airspeed - Increase 6. Approach - Abort, climb to sufficient height for autorotation 7. Autorotation - Perform |
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AP (remains on for 10 seconds) |
1. Flight controls - Hands on |
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AP1 + AP2 |
1. Flight controls - Hands on |
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Second AHRS failure |
1. Flight controls - Hands on 2. Land as soon as possible |
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Single AHRS Failure |
1. Artificial horizon on PFDs and standby AI - Compare 2. Flight controls - Hands on 3. RCU - Reconfigure to valid AHRS |
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Localized discrepancy between both AHRS and FOG |
1. Artificial horizon on PFDs and standby AI - Compare 2. Flight controls - Hands on 3. RCU - reconfigure to valid AHRS |
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Cyclic and yaw trim failure |
1. Flight controls - Hands on |
