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34 Cards in this Set
- Front
- Back
Emergency Shutdown |
Throttle - close FUEL VALVE switch - off BAT switch - off Rotor Brake - engage and allow rotors to stop Helicopter - open or jettison doors and egress |
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Engine hot start/abort start: TOT above 150 prior to opening throttle TOT >927, or above 810 for 10 seconds TOT rises rapidly/abnormally and pilot feels a limit exceedance might occur Engine fails to light within 3 seconds Starter released before 58% N1 Rotor does not turn by 25% N1 |
Starter switch - engage and hold until TOT < 810 Throttle - close Fuel valve switch - Off IGN ENG CB - out Shutdown - complete Bat switch - off GPU - off |
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External fire during start |
Starter switch - release GPU - off Helicopter - complete emergency shutdown |
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Engine fire during flight |
Helicopter - establish autorotation Throttle - close Fuel valve switch - off Helicopter - complete autorotative landing |
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Cabin fire during flight |
Helicopter - start descent Blower A/C switch - off Vents and windows - open Helicopter - land asap, complete emergency shutdown |
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Electrical fire |
Gen switch - off BAT switch - off If: fire, smoke/fumes persist: A. Vents and windows - open Helicopter - land as soon as possible, complete emergency shutdown |
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Engine failure at hover or taxi ENG OUT, ENGINE RELIGHT |
Pedals - maintain direction Cyclic - eliminate drift Collective - cushion landing |
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Engine failure in flight ENG OUT, ENGINE RELIGHT |
Helicopter - establish autorotation If engine fails to automatically relight: Throttle - close Helicopter - complete autorotative landing If time permits: Passengers/crew - alert Radio - transmit mayday Engine - attempt restart in flight procedure |
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High side failure |
Collective - increase to control Nr Throttle - reduce to maintain 97-100% N2 Helicopter - land asap If unable to maintain powered flight: Throttle - close Helicopter - establish autorotation and complete autorotative landing. |
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Low side failure/low rotor rpm ROTOR LOW RPM |
Collective - decrease to control Nr Throttle - full Gov rpm switch - increase to maximum Blower A/C switch - A/C off If unable to maintain powered flight: Helicopter - establish autorotation and complete autorotative landing Else if powered flight can be maintained: Helicopter - land asap |
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Main driveshaft failure |
Helicopter - establish autorotation Throttle - maintain 97-100% N2 Helicopter - complete autorotative landing |
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TAIL ROTOR LOSS OF THRUST/LOSS OF COMPONENTS IN FLIGHT |
1. Helicopter………………………….. Reduce collective to control yaw c. Helicopter……………………….. Complete autorotative landing b. Throttle Close for landing |
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PEDALS LOCKED AT HOVER (ROTATING LEFT) |
Cyclic……………………………….. Eliminate drift 2. Collective…………………………... Lower slowly, accepting rotation on touchdown |
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PEDALS LOCKED AT HOVER (ROTATING RIGHT) |
1. Throttle……………………………... Idle 2. Cyclic……………………………….. Eliminate drift 3. Collective…………………………... Cushion landing |
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PEDALS LOCKED IN-FLIGHT |
1. Helicopter………………………….. Maintain controllable airspeed above 60 KIAS 2. FOD check…………………………. Complete 3. Torque Reaction Check…………. Complete 4. Approach…………………………... Shallow to normal 5. Landing…………………………….. Use procedure for pedals locked at hover |
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HYDRAULIC SYSTEM HARDOVER |
1. HYDRAULIC SYSTEM switch… OFF 2. Helicopter………………………… Land as soon as possible |
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HYDRAULIC SYSTEM FAILURE |
1. Helicopter………………………….. Gradually reduce airspeed (61 to69 KIAS) 2. HYDRAULIC SYSTEM switch…... Confirm ON 3. HYD BOOST circuit breaker……. OUT 4. If: Hydraulic pressure is not regained: a. HYD BOOST circuit breaker….. IN b. HYDRAULIC SYSTEM switch… OFF c. Helicopter………………………... Land as soon as practical Minimize flight control movements d. Approach………………………… Shallow to normal e. Landing…………………………... A run-on landing at 10 KIAS to 15KIAS is recommended
Note: With the skis installed, maximum run-on ground speed is 10 knots. |
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DITCHING (POWER-OFF) |
1. Helicopter…………………………… Establish autorotation 2. Doors………………………………... Open and locked 3. Cyclic………………………………... Reduce groundspeed to 0 beforetouchdown Maintain level attitude 4. Collective……………………………. Minimize rate of decent as rotorcraftsettles into the water 5. Helicopter…………………………… Allow rotors to stop and egress |
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DITCHING (POWER-ON) (not memory) |
1. Crew and passengers……………... Alert/Brief 2. Helicopter…………………………… Establish low hover and jettisondoors Crew and passengers egress Taxi downwind well clear of crew andpassengers 3. Throttle……………………………… Close 4. Cyclic………………...……………… Maintain level attitude 5. Collective……………………………. Minimize rate of decent as rotorcraftsettles into the water 6. Helicopter…………………………… Allow rotors to stop and egress |
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ENGINE RESTART (IN-FLIGHT) |
1. Altimeter..… Check for sufficient altitude 2. Collective…………. Maintain 90% to 107% NR 3. Helicopter………………… Reduce airspeed to 52 KIAS to 69KIAS for existing conditions 4. Throttle……………………………… Close 5. ENG ANTI-ICE switch…………….. OFF 6. HEATER switch……………………. OFF 7. GEN switch…………………………. OFF 8. Engine………………. Proceed with normal start 9. If: Engine idles normally: a. Throttle………………. Open slowly to FULL b. TOT……………………………….. Monitor c. Helicopter…………. Land as soon as possible Else if: No relight, completeshutdown: a. FUEL VALVE switch…………….. OFF b. BAT switch……………………….. OFF c. Helicopter… Complete autorotative landing |
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FREE-WHEEL UNIT FAILURE |
1. Helicopter……….. Establish autorotation 2. Throttle…………………………….. Idle 3. If: Time and altitude permit: a. Throttle……………………………. Open If: NR and N2 rise together: (1) Limited powered flight may bepossible (2) Helicopter………... Land as soon as possible Else if: Unable to maintain poweredflight: a. Helicopter…………. Establish autorotation Follow engine failure in flightprocedure |
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ENGINE COMPRESSOR STALL |
1. Collective…………………………... Reduce 2. ENG ANTI-ICE switch……………. Reposition 3. HEAT VENT switch………………. Reposition 4. BLOWER A/C switch…………….. A/C OFF 5. If: Problem continues: a. Helicopter…….. Land as soon as possible Be prepared for an engine failure at any time Else if: Problem stops: a. Helicopter………. Land as soon as practical Be prepared for possible reoccurrence |
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ENGINE OIL TEMPERATURE |
1. Engine oil pressure and temperature……. Check gauge If: Engine oil temperature exceeds 107°C: 2. Power……………………….. Reduce If: Engine oil temperature remains out of limits: 3. Helicopter……... Land as soon as possible Else if: Engine oil temperature within limits oris fluctuating: a. Helicopter…………. Land as soon as practical |
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ENGINE OIL PRESSURE |
1. Engine oil pressure and temperature…….Check gauge If: Engine oil pressure below 50 psi or above130 psi: 2. Power…………………………….. Reduce If: Engine oil pressure remains out of limits: 3. Helicopter……... Land as soon as possible Else if: Engine oil pressure within limits or isfluctuating: a. Helicopter……………. Land as soon as practical |
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TRANSMISSION OIL TEMPERATURE TRANS OIL TEMP Caution Transmission oil temperature is at or above 110°C. |
1. Power………………….. Reduce 2. If: TRANS OIL TEMP caution light remains on: a. Helicopter…….. Land as soon as possible Else if: TRANS OIL TEMP cautionlight goes out: a. Helicopter…............. Land as soon as practical |
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TRANSMISSION OIL PRESSURE TRANS OIL PRESS Caution Transmission oil pressure is below 30 psi. |
1. Power……………………………….. Reduce Monitor gauge 2. Helicopter……….. Land as soon as possible |
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FUEL BOOST PUMP FAILURE FUEL PUMP caution One or both fuel boost pumps inoperative. |
1. Fuel pressure………………… Check 2. If: No indication of fuel pressure (dual pump failure): a. Helicopter…. Land as soon as possible A dual pump failure can cause the loss of head pressure to the engine-driven fuel pump and result in power loss Else if: With indication of fuel pressure (single pump failure): a. Altitude………Descend below 6,000 feet HP b. Helicopter…………Land as soon as practical |
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ENGINE FUEL FILTER (5 Micron) FUEL FILTER caution |
1. Helicopter………………. Land as soon as possible Be prepared for an engine failure at any time |
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AIRFRAME FUEL FILTER (10 Micron) AF FUEL FILTER |
1. Helicopter...... land as soon as practical |
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GENERATOR FAILURE GEN FAIL caution (Not memory) |
1. Loadmeter…………………………... Check 2. GEN FIELD and GEN RESET… cbsCheck IN 3. GEN switch…………………………. RESET then ON 4. If: GEN FAIL caution light remainsON: a. GEN switch……………………….. OFF b. Load shed……………All unnecessary electrics Required systems ON c. Altitude………. Reduce to below 6000 feet HP d. Helicopter……… Land as soon as practical Consider remaining battery power |
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Metallic Particles CHIP FAULT, ENGINE CHIP, T/R CHIP, TRANS CHIP Grinding noises, vibrations, high oil temp, low px |
1. CHIP FAULT caution light switch.. Press then release 2. If: CHIP and CHIP FAULT caution lights do not extinguish: a. Helicopter………… Land as soon as possible Else if: CHIP and CHIP FAULT cautions lights extinguish: a. Helicopter…………….. Flight can be continued b. Clock……………………………….. Start T/R CHIP or TRANS CHIP (1) Helicopter…………. Land as soon as possible d. If: Third CHIP caution light on the same component illuminates: (1) Helicopter…………………………. Land as soon as possible ENGINE CHIP e. If: Second ENGINE CHIP caution light illuminates within 50 aircraft hoursof the first ENGINE CHIP illumination: (1) CHIP FAULT caution light switch. Press then release If: ENGINE CHIP and CHIP FAULT lights do not extinguish: (2) Helicopter…………. Land as soon as possible Else if: ENGINE CHIP and CHIP FAULT caution lights extinguish: (1) Helicopter…………. Land as soon as practical If: Third or fourth ENGINE CHIP caution light illuminates within 50 aircrafthours of the first ENGINE CHIP illumination: (2) Helicopter…………. Land as soon as possible |
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ICING CONDITIONS |
1. Helicopter………………………….. Fly clear of icing conditions 2. ENG ANTI-ICE switch…………….. ON 3. PITOT HEAT switch………………. ON 4. TOT………………………. Maintain within limits 5. If: Icing condition persists: a. Helicopter…………… Land as soon as possible |
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Transponder Failure (Indication: "TRANSPONDER FAILED") When the GTX345 annunciates TRANSPONDER FAILED, the GTX345 transponder has detected an internal failure and no transponder data is transmitted. (not memory) |
1. Loss of Transponder Function ..... Considered |
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ADS-B Failure (Indication: "NO 1090ES TX")When the GTX345 annunciates NO 1090ES TX, the GTX345 transponder continues to transmit ATC and Flight ID codes and mode settings. (not memory) |
1. Function (FUNC)… ............................... SYS 2. GPS Status (8 or 9 keys)……….30 DIFF or 30 POS 3. Loss of ADS-B Function .......... Considered Note:The NO 1090ES TX annunciation may illuminate as the unit powers on and begins to receive input from external systems, including acquiring the SBAS position |