JASC 1430

Service difficulty reports · 705

Reports filed under 1430 · Fasteners, newest first.

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 jasc_code = '1430'
  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.

SDR UG8APA04005Fastener · corrodedCORROSION FOUND ON FASTENERS UNDER MAIN ENTRANCE DOOR SEAL AT THE HINGE AREA. DISSIMILAR MATERIAL CORROSION BETWEEN THE HUCK FASTENERS AND THE SURROUNDING COMPOSITE STRUCTURE. REPLACED HUCK FASTENERS WITH RECOMMENDED FASTENERS FROM THE MANUFACTURE. AIRCRAFTNov 18, 2004 · N920DC · Gulstm GULFSTREAMGVSDR AWXA200401379Bolt · corrodedDURING C-08 CHECK LEVEL II EXFOLIATION CORROSION WAS FOUND ON LT NR 1 SPOILER HINGE BOLTS. MAINTENANCE REMOVED AND REPLACED CORRODED NR 1 SPOILER HINGE BOLTS IAW AMM SUBTASK 27-64-41-020-050-B, AND SUBTASK 27-64-41-420-050-B.Nov 16, 2004 · N619AW · Airbus A320232SDR RG82005F00000Fastener · looseAFTER LANDING, PILOT PERFORMING POST-FLIGHT CHECK NOTICED LARGE AMOUNT OF OIL ON GROUND. UPON FURTHER INSPECTION IT WAS DISCOVERED THAT A FASTENER, PN 9550158060 ON LT SIDE OF OIL COOLER DUCTING PANEL PN 0401272790 HAD COME LOOSE AND WORN A HOLE ON THE IB SIDNov 7, 2004 · N370GS · Skrsky S76SDR 2005FA0000328Bolt · crackedA DOOR BYPASS VALVE WAS RETURNED FOR INVESTIAGTION. THE REASON FOR RETURN WAS ON PUSHBACK, FLIGHT CREW REPORTED GREEN RESERVOIR LOW LEVEL, WHERE THE INVESTIGATION FOUND A LEAK ON THE DOOR BYPASS VALVE. THE INVESTIGATION IDENTIFIED THAT BOLT HAD SHEARED. FURNov 5, 2004 · Airbus A330*SDR 2005FA0000325Bolt · crackedDOOR BYPASS VALVE WAS RETURNED FOR INVESTIGATION. REASON FOR RETURN WAS ON PUSHBACK, FLIGHT CREW REPORTED GREEN RESERVOIR LOW LEVEL, WHERE THE INVESTIGATION FOUND A LEAK ON DOOR BYPASS VALVE. IDENTIFIED THAT BOLT HAD SHEARED. INVESTIGATION AT MFG INDICATED Nov 5, 2004 · Airbus A330*SDR 2005FA0000038Bolt · improper partDURING ANNUAL INSPECTION, IT WAS FOUND THAT ONE OF THE NAS BOLTS HOLDING THE IB END OF THE LANDING GEAR WAS TOO SHORT AND DID NOT GO ALL THE WAY THROUGH THE NAS NUT. THESE BOLTS WERE INSTALLED AT THE FACTORY, DURING A REPAIR IN 2001. FAILURE WOULD RESULT IN Nov 2, 2004 · N76ML · Bbavia 7KCABSDR CA041102001Bolt · sheared(CAN) MSN 419 WAS UNDERGOING A C2 CHECK IN YUL. IN PREP FOR DOING A SEAL CHANGE ON RT MLG MAINT DISCOVERED SM9 PIN MIGRATED APPROX. 1INCH OUT IN THE IB DIRECTION. GEAR WAS SPLIT,AND IT WAS DISCOVERED THAT THE SM9 PIN RETENTION BOLT (NAS6605D136) HAD SHEARED Nov 2, 2004 · Airbus A330*SDR 24331Bolt · chafedTHE BOLT (P/N AN3-34) THAT SERVES AS THE PIVOT FOR THE ALTERNATE AIR DOOR IN THE INDUCTION DUCT ASSEMBLY (P/N 15708-001) IS BEING CHAFFED BY THE INDUCTION DUCT SUPPORT BRACKET (P/N 15671-002). IN ADDITION TO THE CHAFFED BOLT THE INDUCTION DUCT ASSY IS SUSCEPTNov 2, 2004 · N361CD · Cirrus SR22SDR CA041102005Screw · short(CAN) TRANSISTOR SHORTED DUE TO WRONG (METAL) SCREWS INSTALLED IN PLACE OF THE NYLON SCREWS P/N JYRF284-001. HISTORY INDICATES THAT THE EL SHORT CAUSED BY METAL SCREWS CAN PRODUCE SMOKE IN CABIN. PHOTO ATTACHED.Oct 28, 2004SDR MWEA040195Bolt · missingRIGHT MAIN GEAR UNSAFE AND AUTO SPOILER DO NOT USE LIGHT CAME ON. FOUND BOLT MISSING FROM RIGHT MAIN LANDING GEAR DOOR TARGET ALLOWING TARGET TO ROTATE AND PREVENTING DOOR LATCH FROM FULLY SEATING IN DOOR. REPLACED MISSING HARDWARE.Oct 28, 2004 · N813ME · Doug DC981SDR BAQA097859Nut · brokenANCHOR NUT BROKEN/ REPLACED CELLOct 26, 2004 · N118NC · Bolkms BK117A1SDR 8445185Bolt · bentDURING INSPECTION, FOUND RUDDER CONTROL HORN CENTER PIVOT BOLT BENT. APPARENT CAUSE IS SHEAR STRESS. TOTAL OF 10 SIMILAR PROBLEMS DISCOVERED IN FLEET OF 26 AIRCRAFT SINCE 5/26/2002.Oct 20, 2004 · N844CA · Beech 1900DSDR OG52004F00002Bolt · wornDURING SCHEDULED INSPECTION, WING ATTACH BOLT WAS FOUND TO BE LOOSE. THIS SAME BOLT HAD BEEN REPLACED IAW EO 1 YEAR PRIOR. AT THAT TEIM 3 OTHER AC IN OUR FLEET WERE SIMIALRLY REPAIRED. MFG HAS BEEN CONTACTED AND IS WORKING ON REPAIR. (GL21200500264)Oct 7, 2004 · N283ND · Piper PA28R201SDR 0401863354Bolt · missingDURING CLIMB THE CREW OBSERVED DECREASING OIL QUANTITY AND PRESSURE ON THE NR 2 ENGINE. WHEN OIL PRESSURE DECREASED BELOW 70 PSI THE ENGINE WAS SHUT DOWN. THE AIRCRAFT RETURNED TO NRT. AFTER LANDING HEAVY, A BRAKE FIRE OCCURRED ON THE LEFT MAIN LANDING GEAROct 4, 2004 · N854NW · Airbus A330202SDR 2201092004Bolt · chafedDURING REMOVAL AND REPLACEMENT OF THE P/N 15708-001 INDUCTION DUCT ASSY IT WAS NOTED THAT DUCT WAS CRACKED IN THE AREA OF THE AN3-34 BOLT THAT SERVES AS THE HINGE POINT FOR THE ALTERNATE AIR DOOR. AFTER REMOVING THE BOLT IT WAS FOUND TO BE CHAFFED ALL THE WAYOct 4, 2004 · N968BG · Cirrus SR22SDR 220192004Bolt · chafedDURING REMOVAL AND REPLACEMENT OF PN 15708-001 INDUCTION DUCT ASSY IT WAS NOTED THAT INDUCTION DUCT WAS CRACKED IN AREA OF AN3-34 BOLT WHICH SERVES AS HINGE POINT FOR ALTERNATE AIR DOOR. AFTER REMOVING BOLT IT WAS FOUND TO HAVE A GROOVE WORN INTO BOLT SHANK AOct 4, 2004 · N968BG · Cirrus SR22SDR GTIA040797Bolt · looseRT FWD HOLD DOWN STRAP CLIP FOR AFT EVAC SLIDE HAS A LOOSE IB MOUNTING BOLT. TIGHTENED MOUNTING BOLT.Oct 2, 2004 · N827NK · Doug DC983SDR CA041001008Barrel Nut · damaged(CAN) WHEN TORQUE CHECK OF ENGINE MOUNT BOLTS PERFORMED OB BOLT CORRECT TORQUE COULD NOT BE ACHIEVED. BARREL NUT REMOVED AND FOUND TO HAVE DAMAGED THREADS AND WAS OF FIBER LOCK STYLE. BARRREL NUT AND BOLT REPLACED WITH IPC REQUIRED PARTS.Sep 29, 2004 · Dhav DHC6300SDR CA040924006Bolt · stripped(CAN) AN3-4A BOLTS ATTACHING IB BRACKET TO FLAP FOUND STRIPPED. BOLTS REPLACED WITH NEW AN3-4A. END OF DEFECT.Sep 24, 2004 · Cessna U206GSDR C2XA04BT100Connector · looseDURING SERVICE AND ROUTINE INSPECTION ON RON BTV, MAINTENANCE FOUND SEVERAL FORWARD CABIN EMERGENCY LIGHTS AND LT HAND FORWARD EXTERNAL EMERGENCY LIGHTS INOPERATIVE IN ALL MODES. RESECURED CONNECTOR TO NR 1 EMERGENCY LIGHT BATTERY AS REQUIRED, OPS CHECKED GOOSep 22, 2004 · N13949 · Emb EMB145LRSDR UPS04243259Bolt · damagedINSPECTION TYPE: C, NR 3 ENGINE FWD AND AFT CRANE BEAMS SHOULDER BOLTS HAVE CAD PLATING DAMAGE. BOLTS REPLACED IAW MM 71-10-32.Sep 17, 2004 · N944UP · Boeing 72722CSDR CA040915002Lock Bolt · corroded(CAN) DURING REPAIR OF RIGHT WING FUEL LEAK, THE HEAD OF THE LOWER HYLOCK BOLT ATFUSELAGE TO WING ATTACHMENT ASSEMBLY AT STATION 29 WAS DISLODGED BY A PLASTIC P RC SCRAPER (REF IPC 53-30-01-15 PAGE 0 ITEM 75).FURTHER INVESTIGATION FOUND THE HEAD OF THE BOLT SESep 10, 2004 · Bac 146200ASDR 2004FA0000740Bolt · brokenRT MAIN TIRE SIDEWALL AND TREAD DEPARTED AIRCRAFT ON LANDING ROLLOUT. DETERMINED BROKEN WHEEL THROUGH BOLT DISLODGED INSIDE WHEEL HALF CAUSED BREAKAGE OF FUSIBLE PLUG AND EVENTUAL DEFLATION OF TIRE DURING FLIGHT. AIRCRAFT LANDED ON DEFLATED TIRE. (CE0920040Sep 10, 2004 · N598JL · Beech 400BEECHSDR UPS04243237Bolt · corrodedINSPECTION TYPE: C, NR 2 ENG MOUNT FITTING RIGHT SIDE HAS ONE CORRODED ATTACH BOLT ON UPPER SURFACE OF HORIZONTAL FIRE WALL. BOLT REPLACED.Sep 9, 2004 · N938UP · Boeing 727173CSDR QXEA200400677Fastener · shearedON RIGHT HAND FLAP SHROUD (TRAILING WING BOX) BETWEEN NR 3 AND NR 4 FLAP CANOE HAS FOUR PLACES SHOWING SHEARED RIVET HEADS IN FLAP COVE. REPLACED FASTENERS PER SRM 51-42-06-001-001.Sep 7, 2004 · N600QX · Cndair CL6002C10SDR DHL2004801531Bolt · crackedRT MLG LWR AND UPPER TORSION LINK CTR BOLT CRACKED. REMOVED AND REPLACED CTR BOLT ON RT MLG LWR AND UPPER TORSION LINK IAW MM 32-11-4 PG 201 FOR OPS CHECK.Sep 6, 2004 · N801DH · Doug DC873FSDR DAT2004F00004Bolt · crackedIAW SDR REPLACEMENT OF POWER SECTION AND PROPELLER FOR VIABRATION, ON 09/01/04 (7) OF THE (8) PROP ATTACHMENT BOLTS, PN B3339 WERE FOUND CRACKED. ALL (8) PROP ATTACHMENT BOLTS, PN B3339, AND WASHERS PN A2048-2 WERE REMOVED AND REPLACED WITH NEW ONES PURCHASEDSep 1, 2004 · N937MA · Stbros SD330SDR USAABB04082Nut · unknownCLT - FLT 877 - AFTER TAKEOFF, CREW RECEIVED THE EICAS MESSAGE 'TE FLAP ASYM' AND FLAPS WOULD NOT MOVE. AIRCRAFT RETURNED TO CLT. ON FINAL, AT APPROXIMATELY FIFTY FEET AGL, VIOLENT BUFFETING WAS EXPERIENCED. MAINTENANCE FOUND THE INBOARD COUPLING OF THE TORSep 1, 2004 · N601AU · Boeing 757225SDR 2004UALA00816Fastener · spinningRT WING UPPER SURFACE ENG NR 4 NACELLE UPPER LINK WING FITTING HAS 1 SPINNING FASTENER WS 1168. FASTENER REMOVED. HFEC OF HOLE, NO DEFECTS NOTED. INSPECTION OF STACK UP ACCOMPLISHED WITH NO DEFECTS NOTED. BOLT REINSTALLED WITH RETAINED BOLT AND NEW NUT.Aug 31, 2004 · N107UA · Boeing 747422SDR 2004UALA00815Fastener · rotatedNR 3 PYLON UPPER LINK TO WING ATTACH FITTING HAS ONE FASTENER THAT HAS ROTATED INBD VERTICAL FASTENER MOST AFT. FASTENER REMOVED, HFEC OF HOLE AND NO DEFECTS NOTED. BOLT REINSTALLED WITH RETAINED BOLT AND NEW NUT.Aug 31, 2004 · N107UA · Boeing 747422SDR 2004UALA00814Fastener · rotatedNR 2 PYLON UPPER LINK TO WING FRONT SPAR ATTACH FITTING, ONE FASTENER HAS ROTATED AT INBD ROW UPPER HORIZONTAL FASTENER. FASTENER REMOVED, HFEC OF HOLE AND NO DEFECTS NOTED. BOLT REINSTALLED WITH RETAINED BOLT AND NUT.Aug 31, 2004 · N107UA · Boeing 747422SDR 2004UALA00813Fastener · rotatedNR 1 PYLON UPPER LINK TO WING FRONT SPAR ATTACH FITTING INBOARD & OUTBOARD ROW UPPER HORIZONTAL FASTENERS HAVE ROTATED (2 TTL FASTENERS). FASTENER REMOVED, HFEC ON HOLE AND NO DEFECTS NOTED. BOLT REINSTALLED WITH RETAINED BOLT AND NUT.Aug 31, 2004 · N107UA · Boeing 747422SDR CA040830002Nut · failed(CAN) DISCOVERED RT FWD TRUNION FITTING ATTACH BOLT ANCHOR NUT NOT RETAINING TORQUE DURING INSPECTION OF LANDING GEAR. LANDING GEAR REMOVED TO FACILITATE ANCHOR NUT REPLACEMENT. ALL ANCHOR NUTS REPLACED ON BOTH MLG FWD FITTINGS. ALSO FOUND HEAVY CORROSION OAug 26, 2004 · Piper PA34200TSDR CA040902004Bolt · missing(CAN) STARTER, ALL BOLTS LOOSE AND TWO MISSING.Aug 23, 2004 · Piper PA31350SDR CA040831008Bolt · seized(CAN) WHEN THE PILOT SELECTED GEAR DOWN, THE RT GEAR LIGHT DID NOT ILLUMINATE.AFTER NUMEROUS RETRACTIONS AND EXTENSIONS NEAR THE AIRPORT, THE LIGHT NEVER CAME ON. AFTER LANDING THE RT DOWNLOCK HOOK WAS NOT COMPLETELY ENGAGED. WERE MOVED THE BOLT AND REPLACED WAug 20, 2004 · Piper PA31SDR 2004UALA00774Screw · looseDOOR 2L GIRT BAR LIGHT DOES NOT ILLUMINATE WITH DOOR CLOSED AND ARMED. MOUNTING SCREW FOR FLOOR ATTACH FITTING WAS BACKED OUT AND DID NOT ALLOW GIRT BAR TO ENGAGE FLOOR FITTING. SCREW WAS SECURED AND DOOR ARMS NORMALLY.Aug 17, 2004 · N563UA · Boeing 757222SDR 2004FA0000796Bolt · looseINSPECTION AFTER TURBULENT AIR, DISCOVERED BOTH UPPER FWD WING BOLTS AND NUTS WERE ONLY INSTALLED HAND TIGHT. REVEALED THAT WING BOLT INSP HAD BEEN COMPLETED 116.8 HOURS BEFORE. WING BOLT RETORQUE CHECK HAD BEEN COMPLIED WITH 72.8 HOURS AFTER THAT. AIRCRAFTAug 15, 2004 · N148Z · Beech B90SDR CA040814002Fastener · worn(CAN) UPON INSP OF AC DURING ROUTINE MAINTENANCE, THE RT ENGINE FORWARD LOWER COWL WAS FOUND TO HAVE 3 CAMLOCK FASTENERS PULLED THROUGH THE COWL WHILE STILL LOCKED IN THEIR RECEPTACLES, ON THE IB TRAILING EDGE. THE COWL WAS REMOVED, INSPECTED, AND THE THREE AAug 13, 2004 · Cndair CL6002B19SDR 2004UALA00758Fastener · looseNR 1 PYLON UPPER LINK TO WING FRONT SPAR ATTACH FITTING INBOARD & OUTBOARD ROW UPPER HORIZONTAL FASTENERS HAVE ROTATED, 2 TTL FASTENERS.Aug 10, 2004 · N107UA · Boeing 747422SDR 2004UALA00757Fastener · looseNR 2 PYLON UPPER LINK TO WING FRONT SPAR ATTACH FITTING, ONE FASTENER HAS ROTATED AT INBOARD ROW UPPER HORIZONTAL FASTENER.Aug 10, 2004 · N107UA · Boeing 747422SDR 2004UALA00756Fastener · looseNR 3 PYLON UPPER LINK TO WING ATTACH FITTING HAS ONE FASTENER THAT HAS ROTATED, INBOARD VERTICAL FASTENER MOST AFT.Aug 10, 2004 · N107UA · Boeing 747422SDR 2004UALA00755Fastener · looseRIGHT WING UPPER SURFACE ENGINE NR 4 NACELLE UPPER LINK WING FITTING HAS 1 SPINNING FASTENER WS 1168.Aug 10, 2004 · N107UA · Boeing 747422SDR 2004FA0000750Bolt · incorrectAFT UPPER LT WING ATTACH BOLT FOUND INSTALLED AND PRESUMABLY TORQUED WITHOUT CHAMFERED WASHER UNDER HEAD. DAMAGE TO BATHTUB FITTING UNKNOWN AT THIS TIME.Aug 3, 2004 · N444FC · Beech A36TCSDR SWAA042213Bolt · wornDURING SCHEDULED C4 CHECK, RIGHT ELEVATOR TAB FAILED FREEPLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB CONTROL ROD END BOLTS PER MM.Aug 3, 2004 · N680AA · Boeing 7373A4SDR 2004FA0000682Bolt · shearedDURING AN INSPECTION, FOUND 2 OF THE 3 THROUGH BOLTS SHEARED OFF AT THE THREADS, REPLACED THE STARTER. IF LT UNATTENDED WOULD CAUSE THE BACKPLATE OF THE STARTER TO COME OFF.Aug 2, 2004 · N7275R · Cessna 172SSDR 04FDEA02300Barrel Nut · corrodedLT NR 32 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79832, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 32L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-551Jul 30, 2004 · N613FE · Doug MD11SDR 04FDEA02299Barrel Nut · corrodedLT NR 36 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-80292, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 36L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-551Jul 30, 2004 · N613FE · Doug MD11SDR 04FDEA02298Barrel Nut · corrodedRT NR 33 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-80290, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 33R - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-551Jul 30, 2004 · N613FE · Doug MD11SDR 04FDEA02297Barrel Nut · corrodedRT NR 31 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-80291, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 31R - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-551Jul 30, 2004 · N613FE · Doug MD11SDR DL76G040708Bolt · shearedNR 3 MLG WHEEL MISSING TIE BOLT. REPLACED WHEEL ASSY.Jul 29, 2004 · N154DL · Boeing 7673P6
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