JASC 5710
Service difficulty reports · 4,462
Reports filed under 5710 · Wing Main, Frame Structure, 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 = '5710' 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 jasc_code = '5710' 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 DALA13025941201Tab · bentTABS BENT OVER NUT ON LT WING FOUND TAB BROKEN ON SPECIAL WASHER. REPLACED SPECIAL WASHER IAW ERA 389693-14ADMA, REV ORIG.SDR ASAA2013052295141Closeout Panel · chafedRIGHT T/E CLOSE OUT PANEL CHAFED ON OTBD NR 6 FAIRING. ACFT GROUNDED. REMOVED, FABRICATED AND INSTALLED NEW CLOSEOUT PANEL IAW SRM 51-40-02 AND DWG 65-69646 AND MM 20-50-11-912-002.SDR GTIA20130522528Structure · corrodedRIGHT WING CORROSION BETWEEN WS 7792 & 8268. REPAIRED IAW EA 5720-1307.SDR GTIA20130522627Structure · corrodedRIGHT WING CORROSION AT WS 6699. REPAIRED IAW EA 5720-1307.SDR GTIA20130522626Structure · corrodedRIGHT WING CORROSION AT WS 9704. REPAIRED IAW EA 5720-1307.SDR GTIA20130522625Structure · corrodedLT WING CORROSION AT WS 5512. REPAIRED IAW EA 5720-1308.SDR HNAA2013051700296Plate · crackedLADDER PLATE FOUND CRACKED UNDER STRESS PANEL 622AT. CUTOUT DAMAGE IAW RD8-57-2387 AND FABRICATED NEW PART IAW RD8-57-2387. HFEC INSPECTION DONE ON REPAIRED AREA. NO DEFECTS NOTED.SDR DALA13024660952Heater Blanket · crackedCRACK ON AFT SECTION OF LT WING HEATER BLANKET. LT WING HEATER BLANKET WAS REPLACED DUE TO 1 CRACK OF 0.531 WAS FOUND IAW AMM 30-80-02, PAGEBLOCK 401 AND 601 AND ER/A 494597-14 AD MA REVISION A. RII COMPLETED BY INSPECTION STAMP DELTA ID NR 298092, LIC 20080SDR 2013FA0000458Strut · damagedON INSPECTION OF WING UPPER LIFT STRUT ATTACHMENT POINTS, A BLACK RING WAS NOTED AROUND THE MOST FWD RIVET IN A CLUSTER OF FOUR. EXAMINATION SHOWED THAT THERE WAS MOVEMENT BETWEEN THE RIVET AND THE SURROUNDING STRUT ATTACHMENT. FURTHER EXAMINATION OF THE LT SDR UALA2013051303303Structure · damagedREMOVED RT WING FENCE DUE TO DAMAGE. REPLACED RT WING TIP FENCE IAW AMM.SDR USAA2013052100013Strut · corroded2S CHECK, CORROSION ON HOUSING INTERNAL AREA OF RT INTERCONNECTING STRUT BETWEEN WS 4862 TO 5512 AND BETWEEN RIB 9 TO 10. REPLACED RT INTERCONNECTING STRUT IAW AMM 27-51-44-400-001.SDR USAA2013052100012Strut · corroded2S CHECK, CORROSION ON HOUSING INTERNAL AREA OF LT INTERCONNECTING STRUT BETWEEN WS 4862 TO 5512 AND BETWEEN RIB 9 TO 10. REPLACED LT INTERCONNECTING STRUT IAW AMM 27-51-44-400-001.SDR FDEA201305040910Cap · misrepairedLT WING T/E LOWER ACCESS PANEL 541JB CUT-OUT FWD EDGE LOWER CAP MISREPAIRED. REPAIRED IAW EA 1-5710-167609. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.SDR ASOA2013052803678Structure · corrodedRIGHT BOOST PUMP CUTOUT LAND SURFACE AND VERTICAL SURFACE HAVE CORROSION INDICATIONS AROUND CIRCUMFERENCE, 50 PERCENT FULL SCREEN HEIGHT. FAILED NDT. REPAIRED IAW REO 601R-57-21-1930.SDR UALA2013050103050Screw · unsecureRIGHT WING ROOT HAS SCREW STICKING UP. SECURED FASTENER ON RIGHT WING ROOT AREA.SDR CA130429013Bolt · corroded(CAN) 3 REPLACEMENT WING STRUT ATTACHED BOLTS RECEIVED FROM MFG WITH SIGNIFICANT SURFACE PITTING. PN C3W114-3, 1 AND C3W129-3, 2.SDR IPXA3M78499Cap · corrodedINSPECTION TYPE:4C, CORROSION ON PANEL LANDING AT PANEL ACCESS 541JB LT WING STA XORS 372 TO 433. REPAIRED LT WING T/E BEAM ASSY LOWER CAP BETWEEN XW314 AND XW373 REF STASA EA 011-5710-01-A4599 IR, EO MD11-5720-50639-A AND FORM 8 110-3.SDR ASOA2013042303419Structure · crackedFOUND LT WING TO BE CRACKED AT W/S 149, LOWER SURFACE, JUST OTBD OF JACK PAD.SDR FDEA201304180805Structure · corrodedLT WING T/E LOWER CAP AT 541JB CUT OUT ACCESS FOUND SURFACE CORROSION AT XW326. REMOVED AND REPLACED WITH NEW CAP AS PER SRM 51-33-01 REVISION 52. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 116.SDR FAA20140228000106Block · damagedBEARING BLOCK FOUND DAMAGED.SDR KC8A201303250001Casting · crackedDURING ROUTINE INSPECTION, CRACKS WERE FOUND ON THE RIGHT TIP TANK UPPER AND LOWER FORWARD ATTACH CASTING. REPAIRED.SDR QXEA2013031300565Panel · crackedLEADING PANEL 611AR INBD AND OTBD RIB ANGLE REPAIR CRACKED. REMOVED UPPER INBD AND OTBD RIB ANGLE REPAIR FROM L/E PANEL 611AR IAW SRM 51-42-05-02-01, REV 12 AND SRM 51-40-15-02-01, REV 12 AND SRM 51-41-05-00-01, REV 12. FABRICATED INBD AND OTBD REPAIR ANGLES SDR UALA2013031201455Structure · damagedLEFT WING TIP DAMAGED AT THE FIXED L/E DUE TO AIRCRAFT DAMAGE THE EDGE OF THE SKIN IS TORN 1.75 INCH AND BENT UP ALONG 4 INCH. REPAIRED PER ECRA 5741-01 198 AND PART 3 PERMANENT REPAIR.SDR COZA20130311025Structure · corrodedDURING LT AND RT WINGLET ATTACH HOLE 144 MONTH INSPECTIONS, CORROSION WAS FOUND IN THE HOLES. USING MFG ENGINEERING DATA, HOLES WERE REPAIRED BY OVERSIZING AND LOCAL BLENDING. OVERSIZED FASTENERS WERE INSTALLED AS REQUIRED.SDR MK9A2013070800001Fitting · brokenDURING A ROUTINE INSPECTION, OF RT UPPER WING LIFT STRUT, AFT UPPER WING LIFT STRUT FITTING WAS DISCOVERED TO BE BROKEN THROUGH THE BOLT HOLE THAT ATTACHES THE WING LIFT STRUT TO THE WING.SDR DALA13013239208Fairing · crackedRT ALERON FAIRING BETWEEN T/E TABS CRACKED AT T/E. IAW ERA 512021-14 ACCOMPLISHED ENGINEERING APPROVED TIME LIMITED REPAIR IAW PS 900-5-1, NR 04 ASSOCIATED ER/A 00-512021 REMOVED FOR AC 9208. REPAIRED DAMAGED AILERON FAIRING IAW ERA 512021-14, REV A AND SRM SDR QXEA2013020800350Structure · corrodedRT WING INBD L/E INBD MATING SURFACE FOR 611AL HAS BARE METAL AND FRETTING CORROSION. REMOVED CORROSION IAW SRM 51-21-00-00-02. MIN REMAINING THICKNESS NOTED .034', CONFIRMED AFFECTED AREA CRACK FREE REF NTM 51-00-04-910-801 PT1 & 51-00-06-910-801 PT1 REV 7. SDR 2013FA0000094Cap · departedFUEL CAP ON THE WING INCORRECTLY INSTALLED AFTER REFUELING, FUEL CAP EVENTUALLY DEPARTED THE ACFT INFLIGHT. CAP WAS CHECKED DURING THE PREFLIGHT, AFTER REFUELING, AND THE CAP PLACEMENT WAS CLEARLY FLUSH WITH THE WING, AND THE "HANDLE" WAS FOLDED DOWN AND FLUSSDR SPUY201302020011Structure · crackedDURING ROUTINE C-CHECK INSPECTION, LT WING LOWER CHORD (NEAR MLG SUPPORT BEAM) CRACKED 4 WS 244.5, REF N/R 0305.SDR QXEA2013012300107Vent · crackedLT WING OTBD NACA VENT IS CRACKED ON THE TOP OF THE STANDPIPE THROUGH PANEL 524FT. REMOVED DAMAGED VENT AND MATCH DRILLED NEW VENT IAW SRM 51-42-05-02-01 AND 51-40-07-02-01. INSTALLED NEW VENT IAW SRM 51-42-05-02-01 AND 51-42-45-02-01. SEALED INTERIOR, EXTERSDR GLBA2013011400154Structure · crackedDURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE RT INBD WING, INBD LOWER AFT CORNER BY SPAR RIB FLANGE , 1" IN LENGTH. REPAIRED IAW EO 13-1900-57-003.SDR IPXA3M76930Beam · corrodedINSPECTION TYPE:4C, LT WING TEE BEAM ASSY LWR CAP BETWEEN XW311 AND XW373 CORRODED. REPAIRED TEE BEAM ASSY LWR CAP BETWEEN XW311 AND XW373 REF STASA EA 011-5720-01-A4405 REV I/R, EO MD11-5720-49716-A AND 8110-3.SDR IPXA3M76929Beam · corrodedINSPECTION TYPE:4C, RT WING TEE BEAM ASSY LOWER CAP BETWEEN XW311 AND XW373 CORRODED AT FASTENER HOLES. REPAIRED RT WING TEE BEAM ASSY LOWER CAP BETWEEN XW311 AND XW373 REF STASA EA 011-5720-01-A4404 REV I/R, EO MD11-5720-49715-A AND 8110-3.SDR IPXA3M76769Former · crackedINSPECTION TYPE: 4C, LT WING FIXED L/E FORMER AT XFS 544.5 IS CRACKED OTBD OF PANEL 518FB. REPLACED LT WING FIXED L/E FORMER AT XFS 544.5 AT AFT END OF PANEL 518F B REF SRM 51-35-00 AND SRM 51-33-00.SDR FDEA201212264381Structure · damagedRT WING OTBD L/E REPAIRED IAW EA 1-5730-164851, 1-5730-164849, 1-5710-164853, 1-5710-164850, 1-5730-166316, 1-5730-164854.SDR FDEA201212064257Structure · damagedLEFT WINGLET DAMAGED & AFT LIGHT ASSY. WINGLET REPLACED & ACFT RETURNED TO SERVICE.SDR DALA12017299238Horn · gougedDURING CHECK, FOUND LT WINGTIP L/E HORN GOUGED, WS 560. FOUND HORN OUT OF LIMITS. REMOVED HORN FROM L/E. WELDED, GROUND WELD FLUSH, HFEC AND MT. NO DAMAGE NOTED. ALODINED, PRIMED AND INSTALLED HORN ON LEFT WINGTIP L/E SRM 51-30-02, 51-10-03 AND ER/A 468102SDR DALA1255840183Fitting · scratchedRT WING, UNDERWING SIDE LOAD FITTING OTBD HOLE IS SCRATCHED AND REPAIRED IAW SB 767-54-0069, FIG 3 AND EO 01-074904-03AD REV D.SDR HYIA20121203003Spar · damagedDURING A ROUTINE MX INSPECTION DAMAGE WAS NOTED AT THE RT LOWER STUB WING IN THE AREA OF THE RT JACK POINT. INITIAL DAMAGE WAS IDENTIFIED AS A WRINKLING OF THE SKIN. SKIN WAS DERIVETED TO INSPECT UNDERLYING STRUCTURE (AFT CARRY THROUGH SPAR ASSY 5211173-2 ATSDR CA130114003Rib · worn(CAN) THE RT DEFLECTION CONTROL RIB AT T/E WING STA 278, WHERE THE TURNBUCKLE ATTACHES TO THE RIB WAS FOUND WORN AND TORN OPEN.SDR QXEA2012112801452Channel · corrodedGANG CHANNEL ATTACHING RIVETS CORRODED FOR PANEL 524AT. REMOVED CORRODED GANG CHANNEL RIVETS AND INSTALLED NEW IAW SRM 51-42-05-02-01. APPLIED SEALANT TO RIVETS IAW SRM 51-23-20-02-01.SDR QXEA2012112801455Channel · corrodedGANG CHANNEL ATTACHING RIVETS CORRODED FOR PANEL 524CT. REMOVED CORRODED GANG CHANNEL RIVETS AND INSTALLED NEW IAW SRM 51-42-05-02-01. APPLIED SEALANT TO RIVETS IAW SRM 51-23-20-02-01.SDR QXEA2012112801456Channel · corrodedGANG CHANNEL ATTACHING RIVETS CORRODED FOR PANEL 524DT. REMOVED CORRODED GANG CHANNEL ATTACHING RIVETS AND INSTALLED NEW IAW SRM 51-42-05-02-01. APPLIED SEALANT IAW SRM 51-23-20-02-01.SDR QXEA2012112801451Channel · corrodedGANG CHANNEL ATTACHING RIVETS CORRODED FOR PANEL 525AT. UPON FURTHER INSPECTION CORROSION FOUND TO BE ON SURFACE ONLY. REMOVED SURFACE CORROSION IAW SRM 51-21-00-00-02. RESTORED SURFACE PROTECTION IAW SRM 51-21-00-00-02.SDR TRBA20121126010Fastener · corrodedDURING MX INSPECTION, FOUND THE RT WING FASTENERS AT T/E BETWEEN RIB 8-13 WITH CORROSION. ACFT REMOVED FROM SERVICE. INSTALLED RT WING T/E RIB 8-10 PANEL JIC 53-93-00 RAI-10000. ACFT RETURNED TO SERVICE.SDR TRBA20121126009Hinge · corrodedDURING MX INSP, FOUND THE T/E ACCESS PANEL HINGE CORRODED. THE ACFT WAS REMOVED FROM SERVICE. CLEANED AND TREATED CORROSION AT T/E ACCESS PANEL HINGE IAW SRM 51-21-42. NO MATERIAL REMOVED. THE ACFT WAS RETURNED TO SERVICE.SDR FY4Y20121122197Web · corrodedDURING PERFORMED 7C CHECK, CORROSION WAS FOUND ON CENTER FUEL TANK AFT VERTICAL WEB AT STATION BS 865, LBL 38, 39,WL 165-168 (DIMENSIONS OF CORROSION AREA:2 .3750" × 1.5"). AFTER BLEND OUT CORROSION, THE PENETRATION DEPTH WAS OVER LIMIT IAW SRM 57-10-01, PAGESDR DALA1404540191Fitting · damagedUPPER WING SKIN PANEL LOAD FITTING DAMAGED. REPAIRED IAW AA 5724-01005.SDR ASOA2012112802544Structure · crackedRT WING CRACKED AT WS 148 AT REAR SPAR, CONFIRMED BY EDDY CURRENT. REPAIRED IAW REO 601R-57-21-1794, REV A, REO 601R-57-21-130-01, REO 601R-57-21-130, REV J DATED 03/08/2011, REO 601R-57-21-131, AND IAW REO 601R-57-21-131, REV A DATED 08/29/2011.SDR ASOA2012112802555Seal · crackedRIGHT WING FLIGHT SPOILER CUTOUT CENTER SILL PLATE CRACKED. R & R CRACKED SEAL IAW SRM 51-40-06,51-42-01 & 51-40-2.
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