JASC 5341
Service difficulty reports · 489
Reports filed under 5341 · Fuselage, Wing Attach Fittings, 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 = '5341' 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 = '5341' 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 FDEA201405030922Frame · crackedFRAME 40 TO CTR WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, FOUND A CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0308217 P1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201404060675Attach Fitting · crackedRIGHT WING ROOT REAR SPAR FOUND WITH A CRACK SIGNAL. REPAIRED IAW SRM 51-40-44. PERFORM ROTO-TEST INSPECTION PER NTM51-10-01 AND NO CRACK FOUND.SDR FDEA201404050654Attach Angle · crackedRIGHT WING ROOT REAR SPAR FOUND TO HAVE A CRACK SIGNAL. REPAIRED IAW SRM 51-40-44, SRM 51-40-21 & EA 6-5710-T0307760.SDR FDEA201404040652Attach Angle · crackedLEFT FUSELAGE TO CENTER WING BOX ATTACH ANGLE AT FRAME 47 FOUND CRACKED. REPAIRED IAW EA 6-5710-T0307375 PART 1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201404040651Attach Fitting · crackedLEFT FUSELAGE TO CENTER WING BOX ATTACH FITTING AT FRAME 47 FOUND CRACKED. REPAIRED IAW EA 6-5710-T0307375 PART 1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201404040650Attach Fitting · crackedLEFT FUSELAGE TO CENTER WING BOX ATTACH FITTING AT FRAME 47 FOUND CRACKED. REPAIRED IAW EA 6-5710-T0307375 PART 1. MAJOR REPAIR IAW FEDEX GMM 6-2-100.SDR FDEA201404040649Attach Fitting · crackedLEFT FUSELAGE TO CENTER WING BOX ATTACH FITTING AT FRAME 47 FOUND CRACKED. REPAIRED IAW EA 6-5710-T0307375 PART 1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201404040648Attach Fitting · crackedLEFT FUSELAGE TO CENTER WING BOX ATTACH FITTING AT FRAME 47 FOUND CRACKED. REPAIRED IAW EA 6-5710-T0307375 PART 1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201404040647Attach Fitting · crackedRIGHT FUSELAGE TO CENTERR WING BOX ATTACH FITTING AT FRAME 47 FOUND CRACKED. REPAIRED EA 6-5710-T0307375 PART 1. MAJOR REPAIR IAW GMM 6-2-100.SDR SWIA201436985Fitting · chafedLEFT WING TO FUSELAGE FITTING AT FS 473.15 CHAFED ON OTBD SIDE. C-CHECK, REMOVED CHAFE, FOUND TO BE WITHIN LIMITS, ROTO PEENED AND RESTORED FINISH IAW REO.SDR SIMA20140314008Attach Fitting · crackedRIGHT UPPER OVERWING ATTACHMENT FLANGE BETWEEN FRAME 50 - 51 IS CRACKED APPROX 5 INCHES. ACCOMPLISHED REPAIR OF RT UPPER OVERWING ATTACHMENT FLANGE BETWEEN FRAME 50 - 51 IAW SRM 53-23-12.SDR SWAA2014012024290Fitting · crackedRT MAIN FRAME WING TO FUSELAGE FITTING CRACKED AT BS 661 LONGERON 22R. R & R FITTING IAW SRM & DAC DRAWING.SDR SWAA2014012024289Fitting · crackedLT MAIN FRAME WING TO FUSELAGE FITTING CRACKED AT BS 661 LONGERON 22L. R & R FITTING IAW SRM & DAC DRAWING.SDR CA140721020Bolt · damaged(CAN) DISCOVERED TO HAVE WATER LEAKING INTO THE CABIN AROUND THE AFT LT WING TO FUSELAGE ATTACH FRAME, X 373.150. THE FWD WING TO FUSELAGE ATTACH FRAME WAS INSPECTED FOR PRESENCE OF WATER. STAINING DUE TO WATER INGRESS WAS EVIDENT AROUND THE BOLT HEADS. CORSDR SWAA2013111322337Fitting · crackedMAIN FRAME WING TO FUSELAGE FITTING CRACKED AT STATION 661, LONGERON 22R. R & R FITTING IAW SRM & DRAWING. .SDR SWAA2013111322336Fitting · crackedMAIN FRAME WING TO FUSELAGE FITTING CRACKED AT STATION 661, LONGERON 22L. R & R FITTING IAW SRM & DRAWING.SDR SWAA2013082319453Strap · crackedRT FS FRAME TO WING STRAP CRACKED AT STATION 636. R&R STRAP IAW SRM.SDR A6WA2013082741152Angle · crackedANGLE AT RBL 36 AT AFT FS 484 IS CRACKED. REMOVED CRACKED ANGLE, FABRICATED AND INSTALLED SERVICEABLE ANGLE IAW REO 601R-53-41-059, REV B.SDR REXA2013080501476Mount · chafedRT AFT OTBD WING TO FUSELAGE MOUNT CHAFED. REPAIRED RT AFT OTBD WING TO FUSELAGE MOUNT IAW REO 690-57-11-026 AND EO R57138.SDR REXA2013080501475Mount · chafedLT AFT OTBD WING TO FUSELAGE MOUNT CHAFED. REPAIRED LT AFT OTBD WING TO FUSELAGE MOUNT IAW REO 690-57-11-025 AND EO R57137 S/M-114.SDR 39LA2013071900014Fitting · damagedBS 5744.3 RT SIDE FWD WING MOUNT INSIDE CABIN HAS ONE HOLE DRILLED ACROSS MOUNTING BRACKET. REPAIRED IAW EO 2021032-309 AND EO2012032-424, AND DWG NR 2012032-2032.SDR ASOA2013071608664Fitting · corrodedBS 473.15 AT LBL 45.0, WING TO FUSE FITTING CORRODED AT FLOOR LEVEL. REPAIRED IAW SRM 53-00-00, TR 53-27 AND IAW SRM 51-12-00.SDR REXA2013060600696Link · twistedRIGHT, FS 513, WING TO FUSELAGE PICK UP LINK TWISTED WITH A GAP OF 0.003" ON INBD SIDE AND 0.020" GAP ON OTBD SIDE. LEFT, FS 513, WING TO FUSELAGE PICK UP LINK TWISTED WITH A GAP OF 0.003" ON INBD SIDE AND 0.016" GAP ON OTBD SIDE. REPAIRED IAW REO 601R-53-41SDR SWAA2013061917371Fitting · crackedRT WING MAIN FRAME WING TO FUSELAGE FITTING CRACKED AT BS 661, LONGERON 22R. R & R FITTING IAW SRM & DWG.SDR SWAA2013061917370Fitting · crackedLEFT WING MAIN FRAME WING TO FUSELAGE FITTING CRACKED AT BS 661, LONGERON 22L. R & R FITTING IAW SRM.SDR SWAA2013050615629Fitting · crackedMAIN FRAME WING TO FUSELAGE FITTING CRACKED AT 661, LONG 22R. REMOVED AND REPLACED FITTING IAW SRM & DWG.SDR DALA12013020936Fitting · crackedRT WING TO FUSELAGE FITTING IS CRACKED AT APPROX 993 BS 86. VERIFIED 1 EA CRACK COMING FROM FASTENERS, CUT OUT DAMAGE AREA OF RT WING IAW ER/A 38516-14MA REV A. INSPECTED NDT ALONG EDGE OF CUT OUT AREA NO CRACK NOTED AT OPEN FASTENER HOLE. FABRICATED 1EA RESDR ASOA201201076Link · crackedWING TO FUSELGAE PICK UP LINKS AT FS 797 LT & RT SIDE CRACKED. REINSPECTED IAW REO 670-57-21-381, REV E. NO FURTHER DEFECTS NOTED.SDR ERAA201200015Attach Bolt · crackedLEFT FUSELAGE TO WING ATTACH BOLT HEAD CRACKED.SDR ABXR20120003Tee Fitting · corrodedDURING C-CHECK FOUND TEE FITTING CORRODED IN LT WW. R & R TEE FITTING IAW SRM AND REA 46963REA03.SDR ABXR201201230002Tee Fitting · corrodedDURING C CHECK, FOUND TEE FITTING CORRODED IN RT WW. R & R TEE FITTING IAW REA 46963REA-07.SDR 2012FA0000067Attach Bolt · corrodedDURING INSPECTION OF THE WING ATTACH BOLTS, THE HEADS AND NUTS WERE FOUND CORRODED. INSTALLED NEW BOLTS AND FOUND THAT THE REMOVED BOLTS HAD SOME CORROSION ON THE SHANK. 3 OF THESE BOLTS WERE SEVERELY CORRODED WITH MAJOR PITTING ON THE SHANKS. THESE BOLTSSDR REXA201100501Bulkhead · crackedBULKHEAD, F.S.559 RBL 18 W.L.59.10 AN INDICATION WAS NOTED APPROX .100 IN LENGTH VERTICALLY IN CHEM-MILL 80% FULL SCREEN HEIGHT FAILS NDT. REPAIRED IAW REO 601R-53-41-260 REV E, REO 601R-53-41-609 REV B, & STANDARD REPAIR 601R-53-0114.SDR CA110627014Attach Fitting · damagedDURING A "C-CHECK, MX FOUND A HALF CRADLE FROM THE RT OTBD WING FRONT SPAR TO FUSELAGE ATTACHMENT POINT. THE HALF OF CRADLE HAD FALLEN OUT OF THE ASSY. ON REMOVAL OF HARDWARE IT WAS NOTED THAT THE BARREL NUT WAS ALSO CRACKED. ALL HARDWARE REPLACED IN THE RTSDR V0XR20110404024Attach Angle · crackedNR 3 LT UPPER WING FAIRING ATTACH ANGLE IS BROKEN. REMOVED AND REPLACED L/H WING - BODY FAIRING STRIP NR 3 IAW SRM 51-40-02. LOCATED AND DRILLED IAW SRM 51-20-03. W/C 5065SDR V0XR20110404023Attach Angle · crackedNR 3 LT LOWER FAIRING ATTACH ANGLE BROKEN. (WING FAIRING). REMOVED AND REPLACED NR 3 LT LOWER FAIRING ATTACH ANGLE IAW SRM 51-40-02. LOCATED AND DRILLED IAW SRM 51-20-03. W/C 5063SDR V0XR20110404022Attach Angle · crackedNR 2 LT LOWER WING TO FUSELAGE FAIRING ATTACH ANGLE IS CRACKED. REMOVED AND REPLACED NR 2 LT LOWER FAIRING ATTACH ANGLE IAW SRM 51-40-02. LOCATED AND DRILLED IAW SRM 51-20-03. W/C 5062SDR AUCR20110215004Fitting · crackedDURING ANNUAL INSPECTION, A DETAILED ULTRA-SONIC INSPECTION OF THE FUSELAGE WING ATTACH RING FITTINGS WERE INITIATED BY OUR BY OUR INTERNAL SB. A FATIGUE CRACK WAS APPRECIATED IN THE RT FWD FITTING JUST BELOW THE UPPER MOST AFT HOLE ON THE VERTICAL OTBD FLANGSDR AUCR20110215Attach Fitting · crackedDURING ANNUAL INSPECTION, A DETAILED ULTRA-SONIC INSPECTION OF THE FUSELAGE WING ATTACH RING FITTINGS WERE INITIATED BY AN INTERNAL SB. A FATIGUE CRACK WAS APPRECIATED IN THE LT FWD FITTING, VERTICAL OTBD FLANGE APPROX 6" ABOVE UPPER TENSION BOLT.SDR AUCR20110215003Attach Fitting · crackedDURING ANNUAL INSPECTION, A DETAILED ULTRA-SONIC INSPECTION OF THE FUSELAGE WING ATTACH RING FITTINGS WERE INITIATED BY AN INTERNAL SB. FATIGUE CRACKS WERE APPRECIATED IN THE RT FWD FITTING'S CHORDWISE FLANGE AT THE UPPER TENSION BOLT.SDR AUCR20110215002Fitting · crackedDURING ANNUAL INSP, A DETAILED ULTRA-SONIC INSP OF THE FUSELAGE WING ATTACH RING FITTINGS WERE INITIATED BY AN INTERNAL SB. A FATIGUE CRACK WAS APPRECIATED IN THE RT AFT FITTING'S VERTICAL OTBD FLANGE.SDR CA110208022Bushing · loose(CAN) WING REAR ATTACH BOLT & ECCENTRIC BUSHING ROTATED WHICH LED TO A INCIDENCE ANGLE CHANGE ON THE R/H WING. AN INSPECTION OF THE ATTACH BOLT & BUSHINGS WAS CONDUCTED WITH NO DEFECTS FOUND. AN INSPECTION OF THE WING STRUCTURE, SKINS, FLAP SYSTEM & FUEL SYSTESDR V0XR201101110001Attach Angle · cracked(V0XR) LT LOWER FWD WING ATTACHMENT ANGLE CRACKED. R & R ATTACHMENT ANGLE.SDR REXA201000236Bulkhead Web · crackedFS 559.00 BULKHEAD WEB CRACK DETECTED DURING INSPECTION AND REQUIRES REPAIR. REPAIRED FS 559.00 BULKHEAD WEB IAW BOMBARDIER REO 601R-53-41-260 REV E AND BOMBARDIER REO 601R-53-41-609 REV B DEVIATION C.SDR ZZDA2010042Strap · corrodedLEFT EXTERIOR WING TO BODY SUPPORT STRAP, STA 851, LONG 28L, CORROSION. ACCOMPLISHED EXTERIOR WING TO BODY SUPPORT STRAP REPLACEMENT PER B717 SRM 51-41-02.SDR ZZDA2010041Strap · corrodedRIGHT EXTERIOR WING TO BODY SUPPORT STRAP, STA 851, LONG 28R, CORROSION. ACCOMPLISHED EXTERIOR WING TO BODY SUPPORT STRAP REPLACEMENT PER B717 SRM 51-41-02.SDR A6WA201040154Link · interferenceLT AND RT 513 DOGBONE LINKS TOUCHING. INSP AND DEFERRED IAW REO 601R-53-41-1148 5000 HR PERM REPAIR 1000 HR REINSPECT.SDR 2009FA0000963Attach Fitting · brokenDURING SCHEDULED ROUTINE INSP OF THE LT WING ATTACH FITTINGS, CLIP PN 27-31264-013 WAS FOUND CRACKED/BROKEN VERTICALLY THROUGH AT BOTH CORNERS. CLIP WAS IN 3 PIECES WHEN REMOVED.SDR 2009FA0000962Attach Fitting · brokenDURING SCHEDULED ROUTINE INSP OF THE LT WING ATTACH FITTINGS, CLIP PN 27-31264-013 WAS FOUND CRACKED/BROKEN VERTICALLY THROUGH AT BOTH CORNERS. CLIP WAS IN 3 PIECES WHEN REMOVED.SDR 2009FA0000228Attach Fitting · looseLAST YEAR ABOUT THIS TIME WE WERE PERFORMING PERFORMANCE MODS ON THE ACFT. FOUND THE MAIN WING ATTACH POINTS TO HAVE EXCESSIVE PLAY ON BOTH WINGS WHEN ACFT WAS ON JACK. ENGINEERING LOOKED AT THE DATA WE PRESENTED TO THEM AND SAID "THE PLAY WAS WITHIN LIMITS."
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