Keystone Helicopter S-92A
Service difficulty reports · 324
Newest first. General aviation reporting is voluntary.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = 'S92A' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = 'S92A' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR HEEA20261526001Sensor · unserviceable#1 ENG OIL BYPASS ILLUMINATED APPROX. 75 MINUTES INTO FLIGHT.SDR AC2A202603069201Bearing · unbondedPITCH CONTROL LINK UPPER ROD END ELASTOMER SEPARATED FROM CENTER BUSHING AFTER PICKING UP INTO A HOVER. COMPONENT REMAINED CAPTURED BUT PRODUCED A VIBRATION IN THE MAIN ROTOR SYSTEM. HELICOPTER LANDED AND TAXIED BACK TO THE RAMP FOR INSPECTION.SDR U0GA2025120418345Unknown · odorAFTER LEVELING OFF FROM TAKEOFF WE STARTED NOTICING THE SMELL OF FUEL WHICH SEEMED TO BE COMING FROM THE CABIN AREA OF THE AIRCRAFT. INITIALLY WE TURNED OFF THE HEAT AND SELECTED OUTSIDE AIR FOR THE CABIN AND COCKPIT. WE TRIED DIFFERENT COMBINATIONS OF BLEED ASDR HEEA202511100001Sensor · dirtyFADEC1 FAULT ILLUMINATED FOLLOWED BY FADEC 2 FAULT SEVERAL MINUTES LATER DURING CRUISE FLIGHT. RTB. DURING RTB BOTH CAS EXTINGUISHED PRIOR TO LANDING.SDR HEEA202510240001Adc · inoperativeNR 2 ADC FAIL IN CRUISE FLIGHT. PERFORMED APPROPRIATE CHECKLIST AND RETURNED TO HMAN.SDR HEEA202508180001Apu · inoperativeDURING THE EXECUTION OF BEFORE LANDING CHECKS, THE AUXILIARY POWER UNIT (APU) FAILED TO START, AND THE APU FAIL CAUTION LIGHT ILLUMINATED. THE CREW FOLLOWED THE APPROPRIATE PROCEDURES CHECKLIST AND RETURNED THE AIRCRAFT TO THE HOUMA HELIPORT.SDR HEEA202508080001Warning Light · illuminatedDURING CRUISE FLIGHT, IGB CHIP LIGHT ILLUMINATED. LANDED BACK AT DESTINATION PLATFORM.SDR HEEA202506200001Adc · inoperative#2 ADC FAILED IN FLIGHT.SDR HEEA202505270001Sensor · inoperativeAPU FAIL CAUTION LIGHT ILLUMINATED DURING BEFORE LANDING CHECKS.SDR HEEA202403190001Actuator · inoperativeON INITIAL CLIMB OUT, LANDING GEAR FAILED TO RETRACT. EMERGENCY PROCEDURE PERFORMED AND GEAR HANDLE PLACED DOWN. DOWN LOCKED 3 GREEN INDICATION AND AIRCRAFT RETURNED TO BASE.SDR HEEA202503100001Apu · failedBEFORE LANDING OFFSHORE, APU FAIL LIGHT ILLUMINATED. EMERGENCY PROCEDURE PERFORMED. RETURNED TO HOUMA.SDR AC2A202502289202Support Frame · elongatedDURING OUR INSPECTION, WE DISCOVERED WORKING HYLOC FASTENERS AT THE FS 345.6 FRAME AND THE BL -16.5 TRANSMISSION MOUNT INTERCOSTAL FITTING. WHEN WE GRABBED THE COLLAR WITH PLIERS, WE NOTICED THAT THE FASTENER SHOWING THE MOST SIGNS OF WEAR HAS SLIGHT MOVEMENT.SDR AC2A202502289201Frame · corrodedUPON INSPECTION OF THE L/H SPONSON UPPER CENTRAL ATTACHMENT POINT (FS 361) WE HAD EVIDENCE OF LOOSE HARDWARE. UPON REMOVAL OF HARDWARE, WE FOUND THE BOLTS CORRODED AND CORROSION WITHIN THE BUSHING OF THE HOLE. THERE IS NO EVIDENCE OF FRETTING OR MUD WHERE THE SDR HEEA202502200001Chip Detector · looseDURING CRUISE FLIGHT, IGB HOT LIGHT ILLUMINATED.SDR HEEA202501310001Plate · crackedDURING DEPARTURE FROM MC782/DEEPWATER POSEIDON THE AIRCRAFT EXPERIENCED AN UN-COMMANDED, INFLIGHT SHUTDOWN OF THE #1 ENGINE. THE AIRCREW FOLLOWED THE CHECKLIST EMERGENCY PROCEDURE AND LANDED AT HOUMA WITHOUT FURTHER INCIDENT.SDR AC2A202501209201Servo · leakingAPPROXIMATELY 10 MINUTES INTO THE FLIGHT, THE AIRCRAFT EXPERIENCED A NO. 2 HYDRAULIC PUMP LOW CAS AND THE AIRCRAFT RETURNED TO BASE. UPON INSPECTION, WE DISCOVERED THAT THE FORWARD SERVO SEAL WAS LEAKING EXTENSIVELY, WHICH LIKELY CAUSED THE NO. 2 HYDRAULIC SYSSDR HEEA202501070003Switch · inoperativeLANDING GEAR WILL NOT RETRACT.SDR HEEA202501020001Gearbox · making metalLN CRUISE ON A FLIGHT FROM HMA TO GB-386 POSEIDON, A MGB CHLP CAUTION ILLUMINATED, FOLLOWED BY INPUT 2 CHIP CAUTION APPROXIMATELY 4 MINUTES LATER. CREW DEVIATED TO KHUM UPON FIRST CAUTION.SDR HEEA202501070002Control Panel · inoperativeDURING CLIMB, LANDING GEAR WOULD NOT RETRACT WHEN GEAR HANDLE WAS RAISED. PILOT ELECTED TO LOWER GEAR HANDLE AND LAND.SDR HEEA202412290001Control Panel · inoperativeDURING CLIMB, LANDING GEAR WOULD NOT RETRACT WHEN GEAR HANDLE WAS RAISED.SDR HEEA202412060001Control Panel · inoperativeDURING TAKEOFF FROM HOUMA THE LANDING GEAR WOULD NOT RETRACT.SDR HEEA202409230001Gearbox · making metal#1 INPUT CHIP LIGHT ILLUMINATED.SDR U0GA2024091314429Wire Harness · damagedFIRE LIGHT FLASHES INTERMITTENTLY WITH NO AUDIO OR CAPTION LIGHT. : REMOVED AND REPLACED #2 ENGINE OUTBOARD FLAME DETECTOR HARNESS. OPERATIONAL CHECK GOOD.SDR U0GA2024091314425Connector · contaminatedFIRE LIGHT FLASHES INTERMITTENTLY WITH NO AUDIO OR CAPTION LIGHT. DURING SHUTDOWN FIRE TEST OUTBOARD CIRCUIT BREAKER POPS WHEN TESTING. DRIED WATER FROM CONNECTOR PLUG. OPS CHECKED GOOD.SDR U0GA2024091314412Fire Detector · contaminatedFIRE #2 ENG CAUTION AND AUDIO ACTIVATED DURING HEAVY RAIN AND STAYED "ON". FOUND WATER ON JUNCTION OF #2 INBOARD FIRE DETECTOR CONNECTOR HARNESS. CLEANED AND DRIED OUT CONNECTOR. OPS CHECK GOOD ON GROUND AT THIS TIME. ALL WORK PERFORMED IAW REF. S92 WIRING SSDR U0GA2024090914391Connector · contaminatedFIRE #2 ENGINE CAUTION LIGHT AND AUDIO WARNING ON FOR ONE MINUTE IN RAIN. INSPECTED #2 FIRE DETECTOR WIRE HARNESS AND DRIED CONNECTORS. TESTED SATISFACTORY. TL-265449-2024SDR U0GA2024090914385Connector · dirtyNO 2 ENGINE FIRE LIGHT ILLUMINATED IN HEAVY RAIN FOR 3 SECONDS WITH NO AUDIO WARNING. CLEANED #2 ENGINE FIRE DETECTOR CANNON PLUGS. OPS CHECK GOOD. REF. S92A AMM CHAPTER 26. TL-265397-2024SDR U0GA 202409014384Connector · dirtyNO #2 ENGINE FIRE LIGHT ILLUMINATED IN FLIGHT 10 MINUTES AFTER TAKE-OFF. CLEANED ALL ELECTRICAL CONNECTORS ON FLAME DETECTOR AND UPPER DECK. FIRE LIGHT WENT OFF, TESTED SATISFACTORY. TL-265393-2024SDR HEEA202409060001Connector · dirtyCHIP SYSTEMS FAULT AND IGB OIL HOT LIGHT ILLUMINATED.SDR HEEA202408300001Gcu · inoperative#1 GENERATOR FAILURE.SDR HEEA202408150001Generator · inoperativeWHILE IN CRUISE FLT @ 4000 FT, THE AC #1 GENERATOR FAILED. AFTER FOLLOWING THE EMERGENCY PROCEDURE CHECKLIST, WE CUT OFF THE AC #1 GENERATOR AND CONTINUED TO OUR DESTINATION OF HOUMA WITHOUT INCIDENT.SDR HEEA202407260001Engine · making metal#2 ENGINE CHIP CAUTION LIGHT ON.SDR HEEA202407150001Sensor · inoperativeON OUTBOUND LEG, DURING CLIMB OUT, MGB PRESSURE INCREASED INTO THE PRECAUTIONARY (YELLOW) RANGE. RTB, DECLARED EMERGENCY, LANDED RUNWAY 36 AT HOUMA.SDR HEEA202406280001Proximity Switch · inoperativeLANDING GEAR INITIALLY WOULD NOT RETRACT. AFTER CYCLING THE LANDING GEAR ONCE, IT FUNCTIONED PROPERLY AND RETRACTED.SDR HEEA202406170001Generator · inoperativeAPU FAIL CAUTION IN FLIGHT DURING BEFORE LANDING CHECKS. ATTEMPTS TO RESET THE GENERATOR WERE NOT SUCCESSFUL AND AIRCRAFT WAS RETURNED TO HMA.SDR HEEA202406140001Wire Harness · inoperative#2 ENGINE FIRE LIGHT ILLUMINATED WITH NO SECONDARY INDICATIONS. PERFORMED EMERGENCY PROCEDURES AND RETURNED TO BASE.SDR HEEA2024061100443Pylon · corrodedCORROSION INSIDE HORIZONTAL STABILIZER IN NUMEROUS AREAS ON FITTINGS AND LONGERONS.SDR HEEA202406110149Pylon · corrodedEXCESSIVE CORROSION FOUND INSIDE OF VERTICAL TAIL PYLON.SDR HEEA202405210002Fire Detector · false activationDURING CRUISE FLIGHT ENGINE #2 FIRE LIGHT AND AUDIO WOULD COME ON MOMENTARILY AND THEN EXTINGUISH MULTIPLE TIMES. WE THEN RETURNED TO BASE.SDR HEEA202405140001Switch · faultedDOOR OPEN LIGHT ILLUMINATED UPON REACHING CRUISE FLIGHT. EMERGENCY PROCEDURE PERFORMED AND LIGHT EXTINGUISHED WHILE SLOWING AIRSPEED TO 80 KNOTS. VERIFIED THE DOOR WAS LATCHED CORRECTLY AND THE PINS WERE IN. AFTER SPEEDING BACK UP TO CRUISE SPEED THE LIGHT CAMSDR HEEA202403210001Pump · inoperativeHYD 2 RSVR LOW ILLUMINATED INITIALLY 2-3 MINUTES AFTER REACHING CRUISING ALTITUDE AND RESULTED IN HYD 2 FAILURE. REQUESTED TO RETURN TO KGLS. UPON RETURN HYD 2 PUMP FAIL, SAS 2 PRESS, PSAS 2 FAULT, BOOST PRESS CAUTIONS ILLUMINATED.SDR AC2R921GL03192024Bushing · crackedTHREE OF THE BUSHINGS ON THE RH MOUNTING FOOT WAS FOUND TO BE FRACTURED.SDR U0GA2024030612717Fire Detector · faultedOUTBOUND LEVEL AT 3000' THE AIRCRAFT BEGAN TO GIVE INTERMITTENT APU FIRE WARNINGS. THE AIRCRAFT WAS TURNED BACK TO RETURN TO BASE AND THE FIRE WARNINGS STOPPED APPROXIMATELY 5 MINUTES AFTER IT HAD BEGUN. WHILE ON APPROACH WHEN THE AIRCRAFT ENTERED CLOUDS THE WSDR HEEA202402190001Control Unit · inoperativeDURING CRUISE, #1 AC GENERATOR FAILED AND WOULD NOT RESET. THEN RETURNED TO BASE.SDR HEEA202402160001Generator · inoperativeON SHORT FINAL TO MV C-CONSTRUCTOR #2 GEN FAIL CAUTION LIGHT ILLUMINATED. CONDUCTED A WAVE-OFF INTO A HOLDING PATTERN. EXECUTED CHECKLIST TOR #2 GEN FAIL TO RECYCLE/RESET THE GENERATOR. GENERATOR RETURNED WITHOUT ISSUE. CONTINUED FLIGHT IAW PROCEDURES.SDR HEEA202402050001Adc · inoperativeDURING CRUISE, #1 ADC FAILED, PERFORMED EMERGENCY PROCEDURES.SDR U0GA202402020001Unknown · odorWHILE ENROUTE TO GC468 ON HAA TASKING CREW STATED THAT THEY HAD A STRONG INDICATION OF FUEL SMELL. THE ODOR INCREASED AND CREW STATED THAT THEY WERE HAVING NEGATIVE EFFECTS ON VISION, NAUSEA AND HEADACHES. VISUAL OBSERVATION OF LEAKING FUEL UNDER MEDIC SEAT AFSDR HEEA202401310002Generator · inoperativeDURING CRUISE, #2 AC GENERATOR FAILED CAUTION ILLUMINATED, AS WELL AS AP#2. EMERGENCY PROCEDURE PERFORMED PER THE CHECKLIST, #2 AC GENERATOR CAME BACK ONLINE. #2 AC GENERATOR CAUTION ILLUMINATED AGAIN, PERFORMED EMERGENCY PROCEDURE ONCE AGAIN. RETURN TO HOUMA.SDR HEEA202312010001Compass · inoperativeAUTO PILOT FAILED IN FLIGHT DUE TO A HEADING MISCOMPARE.SDR HEEA202311280001Processor · inoperativeENROUTE, AHRS #2 AND AP #1 & 2 FAILED, RETURNED TO HOUMA
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