Aerospatiale SA330J
Service difficulty reports · 69
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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 = 'SA330J' 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 = 'SA330J' 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 39LA201906254185Fan · seizedAFTER LANDING FOR PAUSE IN VERTREP, PILOTS REPORTED SMOKE SMELL IN COCKPIT. SMOKE WAS THEN NOTED COMING FROM COCKPIT FRESH AIR VENTS. TROUBLESHOOTING REVEALED FRESH AIR VENTILATION FAN/MOTOR SIEZED AND PRODUCED SMOKE. REMOVED AND REPLACED DISCREPANT FRESH AIR SDR 9EKA20181120004Compass · failedAIRCRAFT N902R AND CREW WERE FLYING A ROUTINE VERTICAL REPLENISHMENT MISSION IN THE SOUTH PACIFIC OCEAN. WEATHER WAS CLEAR AND 28 DEGREES CELSIUS. A LITTLE OVER ONE HOUR INTO THE FLIGHT THE FLIGHT CREW DECLARED TO THE SHIP THAT THEY COULD SMELL SMOKE IN THE COSDR 39LA201810085176Reinforcement · crackedCRACKS WERE DISCOVERED IN THE MGB ATTACH REINFORCEMENT AT FRAME 3855. THE MAXIMUM CRACK LENGTH IS APPROXIMATELY 3.0 INCHES IN THE VERTICAL LEG OF THE FITTING. REF SRM TABLE 11, FIGURE 17, ITEM 18 P/N 330A-22-9701-22. ASSEMBLY OF A TECHNICAL DATA PACKAGE IS CURSDR 39LA201810051175Floorbeam · corrodedWHILE PERFORMING A P2 INSPECTION, CORROSION WAS DISCOVERED ON THE FLOORBEAM END CAP IN TWO LOCATIONS AT FRAME 5295. THE CORROSION REMOVAL RESULTED IN A MAXIMUM MATERIAL LOSS IN THE PRIMARY STRUCTURE OF 0.035 INCHES IN DEPTH. TECHNICAL DATA PACKAGE PR2018023 WASDR 9EKA20180329002Hook · brokenWHILE FLYING, THE PILOTS FELT A BUMP IN THE AIRCRAFT AND LOOKED DOWN USING THE CARGO MIRRORS TO SEE THE LOAD IMPACT THE WATER. INSPECTION OF THE HOOK SYSTEM WAS DONE AND WAS FOUND TO BE BROKEN, INTERNAL STEEL CABLE STILL INTACT, ALLOWING FOR THE HOOK TO BSDR 9EKA20180126001Drive Shaft · shearedAFTER THE FLIGHT HAD BEEN COMPLETED AND THE AIRCRAFT WAS BACK ON THE SHIP AND CHOCKED AND CHAINED THE CREW PROCEEDED TO PERFORM THE FRESH WATER RINSE OF THE ENGINES. WITH THE #2 ENGINE AT FLIGHT IDLE AND THE #1 ENGINE AT GROUND IDLE THE FOR THE ENGINE RINSE TSDR 9EKA20170616003Relay · failedWHILE ON APPROACH FOR A SLING LOAD PICK THE AIRCRAFT EXPERIENCED A DUAL ALTERNATOR FAILURE. THE NR 2 TRANSFORMER RECTIFIER UNIT WAS INDICATING IT REMAINED ONLINE. THE NR 1 ALTERNATOR DISPLAYED 116 VAC ON ALL PHASES. "ELEC" AND "NAV" LIGHTS ON THE 7 ALPHA PANSDR 39LA20170518172Plate · corrodedCORROSION FOUND DURING P2 INSPECTION ON THE TRANSMISSION DECK UNDER THE MAIN GEARBOX FLEXIBLE MOUNTING PLATE BETWEEN STATION 4175 AND STATION 4555 EXCEEDING ALLOWABLE REPAIR CRITERIA IN THE STRUCUTRAL REPAIR MANUAL RESULTING IN SKIN REMOVAL AND REPLACEMENT. ASDR 9EKA20161122020Bearing · failedTHE PILOTS REPORTED THE TORQUE FLUCTUATING. SHUT DOWN OF THE A/C TO TROUBLESHOOT THE UPPER PORTION OF THE SWASHPLATE ASSEMBLY WAS NOTICED TO HAVE COLLAPSED AND HAD CONTACTED THE LOWER PORTION CREATING DAMAGE TO BOTH COMPONENTS.SDR 39LA20160728164Bracket · corrodedDURING INSPECTION, THE TIP CAP MOUNTING BRACKETS ON THE MAIN ROTOR BLADE WAS FOUND TO BE HEAVILY CORRODED.SDR 39LA20160728163Bracket · corrodedDURING INSPECTION, THE TIP CAP MOUNTING BRACKETS ON THE MAIN ROTOR BLADE WAS FOUND TO BE HEAVILY CORRODED.SDR 39LA20160728162Bracket · corrodedDURING INSPECTION, THE TIP CAP MOUNTING BRACKETS ON THE MAIN ROTOR BLADE WAS FOUND TO BE HEAVILY CORRODED.SDR 39LA20160728161Bracket · corrodedDURING INSPECTION, THE TIP CAP MOUNTING BRACKETS ON THE MAIN ROTOR BLADE WAS FOUND TO BE HEAVILY CORRODED.SDR 39LA20160716165Connector · dirtyWHILE OPERATING , THE PILOT REPORTED THE NR 1 ENGINE FIRE WARNING LIGHT FLICKERING DURING FLIGHT. MAINTENANCE CLEANED THE WIRE CONNECTION POSTS ON ALL THE FIRE DETECTORS. GROUND OPS CHECKED. NO FAULTS WERE DETECTED.SDR 39LA20160618160Angle · corrodedDURING AN AGING INSPECTION, AREAS OF CORROSION WAS FOUND ON THE UPPER ANGLE FORWARD AND REAR.SDR 39LA20160618159Bracket · corrodedDURING AN AGING INSPECTION, AREAS OF CORROSION WAS FOUND ON THE UPPER ANGLE BRACKET.SDR 39LA20160618158Angle · corrodedDURING AN AGING INSPECTION, AREAS OF CORROSION WERE FOUND ON THE LT DECK ANGLE.SDR 39LA20160618157Angle · corrodedDURING AN AGING INSPECTION, AREAS OF CORROSION WAS FOUND ON THE MAIN FRAME OF STRUCTURE AT JACK SUPPORT.SDR 9EKA20160227003Compressor · stalledDURING THE LAST FLIGHT OF THE DAY, THE ACFT WAS DESCENDING WITH 7.5% PITCH. AS SOON AS PITCH WAS PULLED IN, NR 1 ENG WENT INTO COMPRESSOR STALL WITH A TEMP OF 780F. A LOWER PITCH SETTING OF 8% WAS SET & PULLED IN POWER WITH THE SAME RESULT. ENG FLIGHT IDLESSDR 9EKA2015052721Fuel Filter · cloggedDURING THE FIRST TAKEOFF FROM THE SHIP AS SOON AS THE ACFT CAME OFF THE DECK, THE RT LOW PRESS FILTER CLOGGED LIGHT ILLUMINATED AS THE HELICOPTER WAS TRANSITIONING TO A HOVER. WHILE IN A HOVER THE FILTER CLOGGED LIGHT FLICKERED ON & OFF, THE PILOTS REQUESTED SDR 39LA20150522136Unknown · smokeDURING ILS APPROACH TO PGUM THE FLIGHT CREW NOTICED SMOKE COMING FROM THE OVERHEAD PANEL. AN EMER WAS DECLARED & ACFT DIVERTED WITHOUT FURTHER INCIDENT.SDR 9EKA20150612008Structure · corrodedDURING AN ACFT INSPECTION, SIGNIFICANT CORROSION WAS FOUND ON EXTRUSION AT FRAME 2480 UNDER PILOTS SEATS IAW SRM 53-12 PG 13 FIG 7 ITEM 24.SDR 9EKA20150612007Angle · corrodedDURING P4 AGEING INSPECTION, SIGNIFICANT CORROSION WAS FOUND ON UPPER LT FUSELAGE ANGLE IAW 53-12 PG 32 & E3 FIG 17 ITEM 26.SDR 9EKA20150612006Beam · corrodedDURING P4 AGEING INSPECTION, SIGNIFICANT CORROSION WAS FOUND ON LT & RT BEAMS AT THE HOOK WELL AREA IAW SRM 53-12 PG 35E FIG 18A ITEMS 21 & 22.SDR 9EKA20150612005Beam · corrodedDURING P4 AGEING INSPECTION, SIGNIFICANT CORROSION WAS FOUND BELOW MAIN GEARBOX LT BEAM A-38. IAW SRM 53-13 PG 77 & 78 ITEM 6.SDR 9EKA20150612004Structure · corrodedDURING P4 AGEING INSPECTION, SIGNIFICANT CORROSION WAS FOUND ON EXTRUSION AT FRAME 2480 UNDER PILOTS SEATS IAW SRM 53-12 PG 13 FIG 7 ITEM 24.SDR 9EKA20140527001Pipe · leakingDURING A POST FLIGHT INSPECTION OF THE TAIL BOOM DECK NEAR FRAME STATION 9000 HYD FLUID WAS NOTICED UNDER THE TAIL ROTOR HYD RETURN PIPE. UNABLE TO DETERMINE THE SOURCE OF LEAK SO A GND POWER HYD TEST UNIT WAS HOOKED TO THE LT HAND SYS. AS SOON AS PRESS WASSDR 9EKA20140314001Fcu · damagedDURING FLIGHT, NR 2 ENGINE HAD AN NON-COMMANDED PARTIAL POWER LOSS. A LOUD BANG WAS HEARD, THE NR 2 ENGINE NG DROPPED FROM 91 TO 72 PERCENT, T4 DROPPED FROM 568 TO 441. AFTER 90 SECONDS, ENGINE SPOOLED BACK UP TO 80 PERCENT NG. ACFT LANDED WITHOUT FURTHER SDR 39LA2014011751Engine · overspeedDURING HOVER NR 2 ENG BEGAN TO OVER SPEED. TOOK MANUAL CONTROL OF THE ENG, FOLLOWED EMERGENCY CHECKLIST & PERFORMED NORMAL LANDING.SDR 39LA2013111516Rod · failedUPON LANDING THE NR 2 ENGINE COWLING WAS FOUND UNSECURED & DAMAGED. INSPECTION OF THE NR 2 ENGINE COWLING REVEALED THE COWLING ROD ASSEMBLY HAD FAILED. AFTER FURTHER INSPECTION THE NR 1 ENGINE COWL & SWASH PLATE ALSO HAD DAMAGE DUE TO THE UNSECURED NR 2 ENGISDR 39LA2013111514Doubler · corrodedMOORING RING EXTERNAL DOUBLER RT FUSELAGE FS 6815 FOUND TO BE CORRODED. REPAIRED DOUBLER BY ADDING A REPAIR DOUBLER IAW STS EA 10-2013-124.SDR 39LA2013111513Skin · corrodedCORROSION FOUND LT FUSELAGE SKIN JUST BELOW CABIN WINDOW BETWEEN FS 6405 AND 6815. REPAIRED IAW STS EA 10-2013-070.SDR 39LA2013111512Skin · corrodedCORROSION FOUND RT FUSELAGE SKIN FS 5905 AND 7225. REPAIRED IAW STS EA 10-2013-071.SDR 39LA2013111500011Beam · corrodedCORROSION FOUND ON NLG WELL BEAM AT FS 3223, WL 0, LT BUTT LINE 310. REPAIRED IAW DWG 13021-2029.SDR 39LA2013111500010Frame · corrodedCORROSION FOUND LT FRAME FS 2480, WL 1010 TO 1100 AND WL 1200 TO 1265. REPAIRED IAW STS EA 10-2013-069.SDR 39LA2013111500009Angle · corrodedCORROSION FOUND ON BULKHEAD HORIZONTAL ANGLE FLANGE AT FS 2480. REPAIRED IAW STS EA 10-2013-068.SDR 39LA2013111500008Structure · crackedWHILE PERFORMING P4 INSPECTION, FOUND UPPER DECK STRUCTURE CRACKED IN THREE PLACES AT FS 6405, RT SIDE, BUTT LINE RBL260. REPAIRED IAW AIRLIFT DWG 13021-2027 AND 13021-2028.SDR 39LA2013111500007Structure · crackedWHILE PERFORMING P4 INSPECTION, FOUND UPPER DECK STRUCTURE CRACKED IN FOUR PLACES BETWEEN FS 6138 AND 6405, LT SIDE. REPAIRED IAW DWG 13021-2026.SDR 9EKA2013081200001Engine · failedTHE NR 2 FAILED IN FLIGHT. THE ENGINE HAS BEEN SENT FOR EVALUATION.SDR 2013FA0000042Oil Cooler · leakingNR 2 ENGINE OIL COOLER LEAKS. FOUND DURING DAILY INSPECTION PRIOR TO FLIGHT. REPLACED WITH O/H UNIT.SDR 2013FA0000043Oil Cooler · leakingNR 1 ENGINE OIL COOLER LEAKAGE FOUND DURING DAILY INSPECTION PRIOR TO FLIGHT. COOLER REPLACED WITH A SERVICEABLE UNIT FROM ANOTHER ENGINE. COOLERS ARE BEING REPAIRED/REBUILT.SDR 2013F00033Oil Cooler · leakingNR 1 ENGINE OIL COOLER LEAKAGE FOUND DURING DAILY INSPECTION PRIOR TO FLIGHT. COOLER REPLACED WITH A SERVICEABLE UNIT FROM ANOTHER ENGINE. COOLERS ARE BEING REPAIRED/REBUILT BY PACIFIC OIL COOLERS OF LA VERNE, CA, CERTIFICATE # RF3R813L.SDR LCFA2012F00105Blade · damagedDURING FLIGHT, CREW HEARD A "LOUD BANG" AND NOTED A CORRESPONDING RISE OF THE NR 1 ENGINE EGT. REDUCED POWER TO STABILIZE NR 1 ENGINE EGT AND SUBSEQUENTLY MADE A SAFE RUNNING LANDING AT HOME BASE. A POST SHUTDOWN BORESCOPE INSPECTION OF ENGINE REVEALED THASDR 3S8R2011041600018Bushing · corrodedRIGHT MLG STRUT EXTERNAL FITTING BUSHING CORRODED BEYOND LIMITS. PART WAS REPLACED WITH NEW IAW MFG RE-WORK SHEET 330 21 505 00 BY FACTORY TECHS. ASSEMBLY, CORROSION WAS REMOVED OUTSIDE THE BALL BUSHING SEAT IAW SAME RE-WORK SHEET.SDR 3S8R2011041600017Bushing · corrodedLEFT MLG STRUT, EXTERNAL FITTING BUSHING CORRODED AND WORN BEYOND DIMENSIONAL LIMITS. PART WAS REPLACED WITH NEW IAW MFG RE-WORK SHEET 330 21 505 00 BY FACTORY TECHS. ADDITIONALLY, CORROSION WAS REMOVED OUTSIDE THE BALL
BUSHING SEAT IAW SAME RE-WORK SHEET.SDR 3S8R2011041600016Beam · damagedRT LONGITUDINAL BEAM LOWER SKIN AND BEAM DAMAGED. REPAIR TO BE CARRIED OUT IAW MX 20-03-05-420. DAMAGE IS BETWEEN FS 3855 AND 5295.SDR 3S8R2011041600015Beam · damagedLEFT LONGITUDINAL BEAM LOWER SKIN AND BEAM DAMAGED. REPAIR TO BE CARRIED OUT IN ACCORDANCE WITH EUROCOPTER MTC 20 03 05 420.SDR 3S8R2011041600014Frame · corrodedFRONT UPPER ANGLE OF FRAME AT FS X5295 CORRODED. TO BE REPLACED WITH NEW.SDR 3S8R2011041600013Stringer · deformedSTRINGER IN REAR TRANSVERSAL FUEL TANK COMPARTMENT DEFORMED. TO BE REPLACED WITH NEW.SDR 3S8R2011041600012Stringer · deformedSTRINGER IN REAR TRANSVERSAL FUEL TANK COMPARTMENT DEFORMED. TO BE REPLACED WITH NEW.
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