JASC 5740
Service difficulty reports · 3,003
Reports filed under 5740 · 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 = '5740' 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 = '5740' 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 SIMA20150121020Attach Angle · crackedRIGHT OVERWING TO FUSELAGE LOWER ATTACHMENT ANGLE NR 2 IS CRACKED 3/8 INCHES ON THE FWD EDGE & 2 1/2 INCHES ON THE TE. R & R RT OVERWING LOWER ANGLE NR 2 IAW ETN-EM-53-142.SDR IPXA2015012385412Attach Fitting · crackedINSPECTION TYPE: 3, LOWER WINGLET FORWARD ATTACHMENT FITTING CRACKED. INSTALLED REPLACEMENT FITTING ON LOWER WINGLET IAW EO 5720-27680-C APPROXIMATELY D.SDR DALA2015011400300Attach Fitting · corrodedCORROSION ON INBD, MID AND OTBD ATTACH FITTING FWD AND AFT BORES AT SLAT PANEL 3LT. CORROSION WERE REMOVED OF STA OUTB AND INBD HOLES WERE MEASURED 4EAS 0.1.126 THEREFORE OUT LIMIT MAXIMUM REWORK BUSHINGS WERE FABRICATED AND INSTALLED IAW ERA 531359-14, RSDR S9BA2015011500002Fitting · damagedDURING ACCOMPLISHMENT OF EDDY CURRENT INSPECTION IAW SIE-23-701, REV. G, DEFECT NOTED ON LT WING FITTING LUG, NR 7, INBD UPPER QUADRANT. DEFECT AT 30 PERCENT FSH. PROVIDED DAMAGE REPORT. UPON THEIR ANALYSIS, INSTRUCTIONS WERE PROVIDED TO REMOVE BUSHING AND SDR FQAR20150112004Bracket · crackedDURING A PROGRESSIVE INSPECTION EVENT, A BRACKET WAS FOUND CRACKED BELOW WHERE THE FLAP HANDLE IS MOUNTED. THE BRACKET IN QUESTION IS LOCATED IN THE TUNNEL IN THE CENTER OF THE CABIN FLOOR AND IS USED TO MOUNT THE FLAP HANDLE ASSEMBLY. IT CONTAINS NUT PLATES TSDR A6WA201542307Bracket · crackedLEFT WING LE TRANSITION DUCT OTBD BRACKET CRACKED.SDR A6WA201542306Bracket · crackedRIGHT WING LE TRANSITION DUCT INBD BRACKET CRACKED.SDR SCNA20141223217Bracket · crackedLEFT WING T/E, CRACKED BRACKET ATTACHED TO INBD SIDE OF FLAP DEFLECTION CONTROL ROLLER BRACKET. REMOVED, LOCATED, DRILLED AND INSTALLED NEW BRACKET.SDR SCNA20141223216Bracket · crackedRIGHT WING T/E, UPPER SHELF PANEL BRACKET CRACKED INBD OF FLAP DETECTION CONTROL ROLLER BRACKET FWD SIDE OF BULB SEAL BRACKET. R & R SHELF PANEL.SDR SCNA20141223215Bracket · crackedRT WING T/E UPPER SHELF PANEL BULB SEAL BRACKET CRACKED INBD OF FLAP DEFLECTION CONTROL ROLLER BRACKET. R & R SHELF PANEL BRACKET.SDR SWAA2015012636053Attach Fitting · crackedRIGHT WING RSS 553 WIPER WEB ATTACH CLIP CRACKED. R & R CLIP IAW SRM.SDR A6WA201442268Mount Bracket · crackedSPR PORT, OTBD MOUNT BRACKET CRACKED.SDR A6WA201442165Attach Angle · cracked55025-5000-0023 OTBD LE ATTACH ANGLE CRACKED AT LT WING TRANSITION DUCT.SDR FDEA201411123664Bracket · crackedLT WING TE BRACKET FOR FLIGHT CONTROL PULLEYS AFT OF PYLON IS CRACKED. REMOVED BRACKET & INSTALLED NEW BRACKET IAW SRM 51-31-01, PN ARB0107-5, MAJOR REPAIR.SDR YENA20141112245Fitting · corrodedDURING HEAVY MAINTENANCE CHECK, CORROSION WAS FOUND ON THE LT WING OTBD SIDE OF SPOILER NR 3 FITTING. GAINED ACCESS AND REMOVED CORROSION FROM SPOILER FITTING NR 3. FOUND CORROSION TO BE OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER AND RESTORED AREASDR IPXA2014112684933Attach Fitting · crackedINSPECTION 3C, LEFT LOWER WINGLET AFT INTERNAL ATTACH FITING BROKEN. REPLACED BOTH INTERNAL ATTACH FITTINGS IAW EO 5720-27680-C.SDR FDEA201410163186Attach Angle · crackedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION, FOUND A CRACK AT RT WING STRINGER BUTTERFLY CLIP AT XORS 402 STRINGER 39, APPROX 0.5 INCHES IN LENGTH. REMOVED AND REPLACED WITH NEW ATTACH ANGLE IAW SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-SDR SWAA2014102933489Attach Angle · crackedRIGHT WING PROGRAM ROLLER SUPPORT ARM TO TRANSVERSE WEB ATTACH ANGLE CRACKED. R & R ANGLE IAW SRM.SDR SWAA2014102933488Attach Fitting · crackedLEFT WING RSS 70.5 UPPER TE SUPPORT BEAM, FWD ATTACH CLIP AT REAR SPAR CRACKED. R & R CLIP IAW SRM.SDR SWAA2014101633006Attach Angle · crackedRIGHT WING INBD TE VERTICAL ATTACH ANGLE CRACKED JUST OTBD OF NR 6 FLAP TRACK FAIRING. R & R ANGLE IAW DWG.SDR SWAA2014110433693Attach Fitting · crackedRIGHT WING RSS 78 UPPER TE SUPPORT BEAM FWD ATTACH CLIP CRACKED AT REAR SPAR ATTACH POINT. R & R CLIP IAW SRM.SDR SWAA2014102933477Attach Angle · crackedRIGHT WING TRANSVERSE WEB UPPER ATTACH ANGLE ABOVE NR 2 PYLON AFT TIP CRACKED JUST INBD OF PROGRAM ROLLER SUPPORT ARM ATTACH POINT. R & R ANGLE IAW SRM.SDR A6WA201441959Attach Bracket · crackedLEFT WING LE ATTACH BRACKETS ARE CRACKED AT WS 139 & WS 149.SDR DALA1701479227Support Fitting · damagedMLG ACTUATOR SUPPORT FITTING DAMAGED. REPAIRED IAW 5740-01140SDR A6WA201441899Mount Bracket · crackedRIGHT LE DE-ICE TRANSITION DUCT MOUNTING, OTBD BRACKET CRACKED.SDR IPXA201409084197Attach Fitting · crackedINSPECTION 3C, LEFT WING LOWER WINGLET FORWARD ATTACHMENT FITTING IS CRACKED. R & R FORWARD ATTACH FITTING IAW EO 5720-2720-27680-C.SDR ABXA20140822269Support Fitting · corrodedSUPPORT TEE UNDER INBD END OF RT WING PANEL 651MT CORRODED IN SEVERAL PLACES ALONG ENTIRE LENGTH. REMOVED OLD CHORD & INSTALLED NEW CHORD PN 113T1623-158AX IAW SRM 51-40-02. REINSTALLED PANELS IAW SRM 51-40-02 & PAINTED AREA IAW MM 57-21-02. REMOVED RED MARSDR A6WA201441909Mount Bracket · crackedLEFT WING LE DE-ICE TRANSITION DUCT OTBD MOUNT BRACKET CRACKED.SDR GR4D201408221408Fitting · corrodedLEFT FLAP TRACK LOWER ATTACH FITTING CORRODED, R & R FITTING.SDR GR4D201408220408Attach Fitting · corrodedRT D TRACK UPPER ATTACH FITTING CORRODED, REPLACED ATTACH FITTING REF W/O SC2617.22.20.SDR SWAA2014082531121Attach Angle · crackedRIGHT WING UPPER FIXED PANEL BETWEEN SPOILER NR 7 & 8 OTBD ATTACH ANGLE CRACKED. R & R ANGLE IAW SRM & EA.SDR A6WA201441865Mount Bracket · crackedREFUEL DEFUEL DOOR NOZZLE MOUNTING BRACKET ON RT FRONT WING SPAR IS CRACKED AT LOWER OTBD CORNER AT RBL 50.0.SDR A6WA201441861Mount Bracket · crackedRIGHT LE INBD TRANSITION DUCT OTBD MOUNT BRACKET CRACKED.SDR ABXA20140806280Support Fitting · corrodedNUMBER 1 FLAP SUPPORT NR 3 TENSION BOLT HOLE HAS A DEFECT INDICATION WITH ROTARY SCAN, HOLE IS REAMED TO .656. SDR INFO CORRODED L2, PN 113T1345-43, SN NSN, PART NAME NR 1 FLAP SUPPORT FITTING, STRINGER & WS LOC ON ACFT 798.2. ACFT WAS GNDED.SDR ABXA20140806278Support Fitting · corrodedLEFT WING OTBD & INBD ROTARY ACT SUPPORT HOLE AT 9 O`CLOCK LOOKING INBD SHOWS DEFECT INDICATION HFEC. SEE REA NR B657-61118-MR. SDR INFO CORRODED L2, PN 113T1345-43, SN NSN, PART NAME NR 1 FLAP SUPPORT FITTING, STRINGER & WS LOC ON ACFT 792.2. ACFT WAS GNDESDR ABXA20140806276Support Fitting · corrodedRIGHT WING OTBD ROTARY FLAP SUPPORT NR 8 HOLE LOOKING INBD SHOWS DEFECT INDICATION HFEC. SDR INFO CORRODED L2, PN 113T1345-44, SN NSN, PART NAME NR 8 FLAP SUPPORT FITTING, STRINGER & WS LOC ON ACFT ROWS 798.2. ACFT WAS GNDED.SDR ABXA20140805267Support Fitting · corrodedRIGHT WING TE PANEL SUPPORT TEE CORRODED IN 2 PLACES NEAR PANEL 652FB. INSTALLED NEW SUPPORT, TEC CHORD, SRM 51-40-02 & REINSTALLED. REMOVED TE PANEL IAW SRM 51-40-02. SDR INFO CORRODED L2, PN 113T1407-6, PART NAME CHORD, SN N/A, EXACT FS & BS FROM WS 431 -SDR SWAA2014101432922Attach Angle · crackedRIGHT WING REAR SPAR TO TE BEAM ATTACH ANGLE CRACKED AT RSS 76. R & R ANGLE IAW SRM.SDR SWAA2014092332222Support Fitting · crackedRIGHT WING HYD LINE SUPPORT BRACKET CRACKED ON INBD SIDE OF NR 5 SPOILER INBD ACTUATOR SUPPORT FITTING. R & R FITTING IAW SRM.SDR FDEA201407241945Attach Angle · crackedRIGHT WING LE COMPARTMENT FIXED LE SUPPORT RIB AT XOS 584 OTBD ATTACHED ANGLE FOUND CRACKED. ATTACHED ANGLE REMOVED AND REPLACED IAW SRM 51-31-01 VOLUME II REVISION 101. NEW ANGLE FABRICATED IAW DRAWING ARB1162 REVISION S. REPAIR CLASSIFIED AS MAJOR PER GMSDR FDEA201407241937Attach Angle · crackedRIGHT WING LE COMPARTMENT FIXED LE SUPPORT RIB OTBD ATTACHED ANGLE AT XOS 584 FOUND CRACKED. REMOVED IAW SRM 51-31-01 REVISION 56. NEW ANGLE FABRICATED IAW DRAWING ARB2931 REVISION H. ANGLE INSTALLED IAW SRM 51-33-01 REVISION 56. REPAIR CLASSIFIED MAJOR SDR FDEA201407211890Attach Angle · crackedLEFT WING LE FIXED LE SUPPORT RIB AT XOS 584 OTBD ATTACHED ANGLE FOUND CRACKED. RIB ATTACH ANGLE REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II REVISION 101. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 122.SDR A6WA201441818Attach Bracket · crackedRT WING LE REFUEL PORT MOUNT, OTBD ATTACHMENT BRACKET CRACKED.SDR V0XD2014070916238Attach Angle · crackedLT LOWER WING TO FUSELAGE LATERAL FAIRING ATACH ANGLES ARE CRACKED. REMOVED AND REPLACED THE ATTACH ANGLES IAW SRM 51-40-02, 51-20-03, 51-40-06, 51-20-01, CPM 51-21-04.SDR SWAA2014071429926Attach Angle · crackedLEFT WING ORSS 271 APPROX BELOW TE FIXED PANEL, TE VERTICAL RIB AFT BUMPER SEAL ATTACH ANGLE CRACKED. R & R ANGLE IAW DWG.SDR DALA2014070503977Bushing · corrodedCORROSION FOUND ON LT WING HEATER BLANKET AFT MOUNTING BUSHINGS. MOUNTING BUSHING REMOVED AND REPLACED IAW EA 04-070683-03 AD REV L.SDR V0XD2014070316237Attach Angle · crackedRIGHT UPPER WING TO FUSELAGE LATERAL FAIRING ATTACH ANGLE CRACKED. R & R ATTACHMENT ANGLE IAW SRM 51-40-02, 51-20-03, 51-40-09, CPM 51-21-06.SDR ASOA20140702172Attach Angle · crackedDURING C-CHECK, SEVERAL CRACKS IN ATTACH FLANGE FOR PANEL ON LT UPPER INBD WING SKIN BETWEEN FRAMES 40-41. MAINTENANCE REMOVED DAMAGED PORTION, FABRICATED NEW ANGLE AND INSTALLED BETWEEN FRAMES 40-40 IAW SRM 51-40-02 AND EC5720-01079. THE ACFT WAS APPROVED FSDR SWAA2014073030481Lug · corrodedLEFT WING NR 4 FLAP TRACK AFT ATTACH POINT, OTBD LUG, OTBD FACE CORRODED ADJACENT TO BUSHING. REPAIRED LUG IAW EA.SDR GO3S2014FA0000443Attach Fitting · crackedLEFT WING FORWARD SPAR ATTACH FITTING, CRACKED IN HALF. ALLOWED WING TO SHIFT FORWARD AND AFT CAUSED AFT SPAR PLATE, TO LOOSEN AND ELONGATE BOLT IN BOTH FUSELAGE AND WING FITTINGS.
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