JASC 5300
Service difficulty reports · 8,206
Reports filed under 5300 · Fuselage Structure (General), 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 = '5300' 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 = '5300' 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 IPXA2023031791928Unknown · crackedINSPECTION TYPE:C6CRACK ON ANGLE OF AFT CARGO COMPARTMENT NEAR STA 1087, LBL 26.INSTALL NEW PART I.A.W BOEING DWG NO.:140T0130 SH 50, REV ''A'' AND 767-300F SRM 51-40-02-0G, REV 85.01SDR YENA2023031400239None · noneDURING HEAVY MAINTENANCE: A CRACK OF 0.150IN LENGTH AT FRAME 15 FLOOR STRUCTURE BEAM Y=270 RH AT FWD PASSENGER CABIN WAS FOUND; REF TO TOMX WO 2162 NR 00335, CRACK OF 0.150IN LENGTH AT FRAME 15 FLOOR STRUCTURE BEAM Y=270 RH AT FWD PASSENGER CABIN WAS REPAIRED SDR YENA2023031400234Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION ON SEAT TRACK BEAM FLOOR STRUCTURE LOCATED AT FR 84 BTW +Y 300 RH SIDE ON W2; REF TOMEX NRC 00312, WO 2162, SEAT TRACK BEAM FLOOR STRUCTURE LOCATED AT FR 84 BTW +Y 300RH SIDE ON W2 WAS REPAIRED PER EMB-190 SRM 53-00-10/REP.SDR IPXA2023031491829Angle · crackedINSPECTION TYPE:C6CRACK ON ANGLE (P/N:146T5651-6) OF BULK CGO COMPT NEAR STA 1578, RBL 78.INSTALL NEW PARTS I.A.W 767-300F SRM 51-40-02-0G REV. 85.01 AND BOEING DWG 146T5650 SH 5, REV.''C''SDR IPXA2023031491828Angle · crackedINSPECTION TYPE:C6CRACK ON ANGLE (P/N:146T5651-5) OF BULK CGO COMPT NEAR STA 1578, LBL 78INSTALL NEW PARTS I.A.W 767-300F SRM 51-40-02-0G REV.85.01 AND BOEING DWG 146T5650 SH5, REV.''C''SDR CALA2023031000706Floor Support · corrodedB737-53-3-0740 AFT CABIN SUPPORT FWD OF L/H WEB HAS CORROSION STA 1006SDR CALA2023031000705Panel · corroded(B737-53-3-0740) AFT CABIN STA 1016 L/H WEB HAS CORROSIONSDR CALA2023031000704None · corrodedB737-53-3-0740 AFT CABIN STA 1016 LBL 18" HAS CORROSIONSDR CALA2023031000703Beam · corrodedB737-53-3-0711 FLOOR BEAM AT STA 340 INBD OF L1 HAS SURFACE CORROSION.SDR CALA2023031000702Beam · corrodedPASSENGER CABIN FLOOR BEAM 947-RH END UPPER CAP CORRODED AT FAST ENER. EVALUATED DAMAGE ON FLOOR BEAM UPPER FLANGE AT STA 947.5. ORIGIN 4/27/23. PERFORMED REPAIR AT MAIN CABIN STA 947.5 BETWEEN LBL 58 AL THICKNESS IS .185". LOW MAT .046", R.M. .141" FOUND TO BSDR CALA2023031000701Seat Track · corrodedB737-53-3-0740 L/H O/B SEAT TRACK AT STA 907 HAS CORROSION REMOVED AND INSTALLED SEAT TRACK L/H OB STA 887 AT STA 927 IAW B 737-800 SRM 51-40-02 PAR 7, 9. SFR #1031562. DATA WAS TRANSCRIBE D FROM PAPER DOC AERSALE WO 3826 NR 24799 WORK ACP BY MECH V9428 59 INSSDR CALA2023031000699None · corrodedB737-53-3-0740 AFT CABIN SUPPORT BEAM STA 1016 RBL 18" HAS CORROSION PERFORMED WORK AT AFT CABIN STA 1016, RBL 18" IAW B737-800 SRM 5 1-40-02 PAR 407. FABRICATED AND REPLACED STRAP. DATA WAS TRANSCR IBED FROM PAPER DOC AERSALE WO 3826 NR 24790 WORK ACP BY MECHSDR CALA2023031000698Beam · corrodedB737-53-3-0740 FLOOR BEAM 986.5 RBL 23" AREA OF CORROSION FLOOR BEAM 986.5 RBL 23" WAS REPAIRED IAW SRM 53-00-51-2R-1 (REP AIR 1) PAR 4. DATA WAS TRANSCRIBED FROM PAPER DOC AERSALE WO 382 6 NR 24792 WORK ACP BY MECH V940458 INSP BY AQC008SDR CALA2023031000697Beam · corrodedB737-53-3-0740 FLOOR SUPPORT AT 927 RBL 9" HAS CORROSION THE FLANGE OF A TRANSVERSES FLOOR BEAM CHORD WAS REPAIR IAW SRM 53-00-51-2R-1 PAR 4, A THROUGH L. DATA WAS TRANSCRIBED FROM PAPE R DOC AERSALE WO 3826 NR 24768 WORK ACP BY MECH V940903 INSP BY AQC028SDR CALA2023031000696None · corrodedB737-53-3-0740 L2 DOOR SILL PLATE HAS CORROSION IN SEVERAL AREAS NEW SILL PLATE WAS INSTALLED IAW SRM 51-40-02-0G-0 PARA 4 AND 9. SFR 1031557. DATA WAS TRANSCRIBED FROM PAPER DOC AERSALE WO 382 6 NR 24764 WORK ACP BY MECH V937322 INSP BY AQC009SDR CALA2023031000694Intercostal · corroded(B737-53-3-0711) INBD SEAT TRACK AT STA 340 LBL & 24 END OF SEAT TRACK HAS CORROSION REMOVED CORROSION AND INSTALL NEW STIFFENER AT STA 325 TO 340 LB L 44 IAW B737-800 SRM 51-40-02-0G-0 PAR 7. SFR #1031555. DATA WA S TRANSCRIBED FROM PAPER DOC AERSALE WO 3826 SDR CALA2023031000692Intercostal · corroded(B737-53-3-0711) CORROSION BY 2 EA GALLEY FITTINGS AT BS 303 ON MAIN CABIN FLOOR STRUCTURE FOR GALLEY 1 REPLACED FITTINGS AT BS 303 ON MAIN CABIN FLOOR STRUCTURE GALLEY 1 IAW SRM 51-40-02-0G-0 PARA 7. SFR #1031553. DATA WAS TRANSCRI BED FROM PAPER DOC AERSALE SDR CALA2023031000691Intercostal · corrodedB737-53-3-0740 RH AFT LAV O/B MOUNT CORROSION ON FLOOR BEAM REMOVED AND REPLACED INTERCOSTAL AT RH AFT LAV OB MOUNT ON FLOOR BEAM IAW SRM 51-40-02-0G-0 PARA 7. D. SFR #1031552. DATA WAS TR ANSCRIBED FROM PAPER DOC AERSALE WO 3826 NR 24795 WORK ACP BY ME CH V93SDR CALA2023031000690Floor Support · corrodedB737-53-3-0740 FLOOR SUPPORT BETWEEN 927-947 RBL 10 HAS CORROSION. EVALUATED DAMAGE ON FLOOR STRUCTURE BTW STA 927 TO 947.5 RBL 10 REPLACED NEW ANGLE SUPPORT P/N: 147A5768-20 IAW B737-800 SRM 51- WITH DIMENSIONS L=2",W=2", D=.050". FOUND TO BE OUT OF LIMITS IASDR CALA2023031000689Fitting · crackedORIGINAL LOP PAGE CLOSED IN ERROR: R/H FR68 STGR22 INNER CAP WEB FLANGE HAS A CRACK INDICATION "CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS BEFORE NEXT FLIGHT" AD RELATED (AD 2022-15-05) PER HAECO LCQ NR 9292565/40565 GENERATED BY V061632. REFERENCE ORIGINAL SDR CALA2023030900664Web · crackedWING CENTER SECTION UPPER SURFACE HORIZONTAL PRESSURE WEB STA 665 RBL 40 CRACKED REF AAR N/R 974984 ACCOMPLISHED HORIZONTAL PRESSURE DECK WEB REPAIR BETWEEN STA 663 TO STA 675 FROM RBL38 TO EBL60 PER REF B737 SRM 53-40-51-2R-2 FIG 202 DETAIL A WORK ACCOMPLISHESDR CALA2023030900662Frame · crackedFRAME CRACKED THROUGH RIVET HOLE SEEN ON AFT SIDE OF L/H FRAME STA 760 FOR OVERHEAD BIN ATTACH BRACKET BETWEEN STR 8 AND 9L. REPAIRED FRAM CRACK AT STA 760 LH SIDE IAW B757 SRM 53-00-07 REPAIR#8 SHEET 1 DETAIL 1. ACCOMPLISHED ON AMES NR 155339-0200-0215 ENTERESDR ABXA2023031333Unknown · unknownDURING ROUTINE LINE OPS IN CVG, A SMALL CRACK WAS FOUND IN THE FUSELAGE SKIN AT STA 347 ALONG STRINGER 39R. FURTHER INVESTIGATION REVEALED THAT THE SKIN AND STRINGER 39R IN THIS AREA WERE CORRODED BEYOND SRM LIMITS AND REQUIRED REPAIR/REPLACEMENT. A NEW PIECSDR UIEA2023031000242None · noneDEVIATION - PERFORM STA 2598 BULKHEAD MODIFICATION FOUND DEVIATION AT DOUBLER(<P>1. PERFORMED EI T2023A53M-310 REV 0 SEQUENCE A. 2. PERFORMED EI T2023A53M-310 REV 1 SEQUENCE B. 3. PERFORMED EI T2023A53M-384 REV 0 SEQUENCE A. 4. ACCOMPLISHED EI T2023A53M-310 RESDR UIEA2023031000239None · noneFOUND EXISTING REPAIR DOUBLER ON OUTER SIDE SKIN OF FUSELAGE AT STA 2658 BETWEEN S-11L AND 13L(<P>1. REMOVE THE EXISTING DOUBLER IAW SRM 51-40-02-0G-0 REV 96. 2. PERFORM EI T2023A53M-272 REV 0 SEQUENCE A. 3. ACCOMPLISHED EI T2023A53M-272 REV 1. 4. JOB COMPLETESDR UIEA2023031000238Fitting · noneCRACK ON FRONT SPAR INTERCOSTAL LUG FITTING AT STA 1000 LBL 11.33(<P>1. REMOVED DAMAGE PARTS IAW SRM 51-40-02-0G-0 REV 96. 2. INSTALL NEW PARTS IAW SRM 51-40-02-0G-0 REV 96 AND EO 4453C024 REV 3 AND EI T2023A53M-134 SEQUENCE B. 3. ACCOMPLISHED EI T2023A53M-134SDR UIEA2023031000237None · noneWORN OUT - FOUND MAIN DECK SEAT TRACK WORN OUT AT STA 1100, LBL 11.33(<P>REMOVED THE AFFECTED FASTENER IAW SRM 57-00-02-0G-0 REV 96. 2. PERFORM REPAIR IAW EO T2023A53M-191 SEQUENCE A AND SEQUENCE B REV 1. 3 INSTALLED FASTENERS IAW SRM 51-44-02-0G-0 REV 96 AND SDR UIEA2023030900230Stiffener · noneCORROSION ON LWR FUSELAGE KEEL BEAM STIFFENER AT STA 1000 WL 90 LBL9(<P>1. REMOVE DAMAGE PARTS IAW SRM 51-40-02-OG-0 REV96 2. INSTALL NEW PARTS IAW SRM 51-40-02-0G-0 REV96 AND DWG NO: 65B01828 SH34 REV-A AND DWG NO: 65B01828 SH44 REV-C 3. JOB COMPLETED AND CONSDR UIEA2023030900229None · noneM/D CGO FLOOR STRUCTURE CORROSION AT STA 1860 RBL 117(<P>1. BLENDED OUT THE DAMAGE AREA IAW SRM 51-10-02-0G-0 REV96 2. PREFORM NDT INSPECT REFER JOB CARD ATTACHING SHEET NO: 0373340 3. ACCOMPLISHED EI NO: T2023A53M-328 REV1 4. JOB COMPLETED AND COND CHK NML.</SDR UIEA2023030900227None · noneEXISTING UNDOCUMENTED REPAIR DOUBLER ON OUTER SKIN OF FUSELAGE AT STA 2598 AFT SIDE BETWEEN S-26R AND S-49R(<P>1. REMOVED EXISTING DOUBLER IAW SRM 51-40-02-0G-0 REV96 2. REPAIR THE SKIN DOUBLER IAW EI NO. T2023A53M-436 REV1 AND DWG NO. 65B02707 SH2 REV1 3. CONSDR UIEA2023030900226None · noneEXISTING UNDOCUMENTED REPAIR DOUBLER ON SKIN OF FUSELAGE AT STA 2598 FWD SIDE BETWEEN S-26R AND S-42R(<P>1. REMOVED EXISTING DOUBLER IAW SRM 51-40-02-0G-0 REV96 2. ACCOMPLISHED THE SKIN REPAIR IAW EI NO. T2023A53M-433 REV1 AND DWG NO. 65B02698 SH13 REV A 3. COSDR UIEA2023030900225None · noneEXISTING UNDOCUMENTED REPAIR DOUBLER ON FUSELAGE SKIN AT STAÂ 1880 BETWEEN S-43L AND S-46L(<P>1. REMOVE EXISTING REPAIR DOUBLER IAW SRM 51-40-02-0G-0 REV96 2. REPAIR SKIN IAW EI NO: T2023A53M-494 REV1 3. ACCOMPLISHED THE REPAIR AREA IAW EI NO: T2023A53M-494 RSDR UIEA2023030900224Shear Tie · noneCRACK ON FRONT SPAR SHEAR TIE AT STA 1000 RBL 57.50(<P>1. REMOVE DAMAGE PARTS IAW SRM 51-40-02-0G-0 REV96 2. INSTALL NEW PARTS IAW SRM 51-40-02-0G-0 REV96 AND EO NO. 4453C024 REV3 AND EI NO: T2023A53M-134 SEQUENCE B 3. ACCOMPLISHED EI NO: T2023A53M-134 REV2 4.SDR UIEA2023030900223Shear Tie · noneCRACK ON FRONT SPAR SHEAR TIE AT STA 1000 RBL 75.92(<P>1. REMOVED DAMAGED PARTS IAW SRM 51-40-02-OG-0 REV96 2. INSTALL NEW PARTS IAW SRM 51-40-02-0G-0 REV96 AND EO NO: 4453C024 REV3 3. JOB COMPLETED</P>)SDR UIEA2023030900222Shear Tie · noneCRACK ON FRONT SPAR SHEAR TIE AT STA 1000 RBL 33.99(<P>1. REMOVED DAMAGE PARTS IAW SRM 51-40-02-0G-0 REV96 2. INSTALL NEW PARTS IAW SRM 51-40-02-0G-0 AND EO NO: 4453C024 REV3 AND EI NO: T2023A53M-134 SEQUENCE B 3. ACCOMPLISHED EI NO: T2023A53M-134 REV2 4. ORIGSDR UIEA2023030900220None · noneDEVIATION- DURING PERFORM SB 747-53A2443 REV2 HAVE SHORT EDGE MARGIN(<P>1. ACCOMPLISHED EI NO: T2023A53M-132 REV1 AND 2. JOB COMPLETED AND CONDITION CHECK NORMAL</P>)SDR UIEA2023030900219None · noneCRACK ON SIDE ANGLE OF NOSE WHEEL WELL TOP PANEL ASSY NEAR STA 300, LBL 30 WL 190(<P>1. ACCOMPLISHED EI NO. T2023A53M-157 REV1 2. JOB COMPLETED AND CONDITION CHECK NORMAL</P>)SDR UIEA2023030900218None · noneWORN OUT- FOUND MAIN DECK SEAT TRACK WORN OUT STA 1110 RBL 11.33(<P>1. REMOVED THE AFFECTED FASTENER IAW SRM 51-40-02-0G-0 REV96 2. REPAIRED DAMAGE AREA IAW EI T2023A53M-130 SEQUENCE A AND SEQUENCE B REV 1 3. INSTALLED FASTENERS IAW SRM 51-40-02-0G-0 REV96 ANDSDR UIEA2023030900215None · noneCORROSION ON M/D FLOOR BEAM UPPER CAP NEAR STA 1580 LBL 77 ~ LBL 99(<P>1. ACCOMPLISHED JOB IAW EI NO T2023A53N-170 SEQUENCE A REV0 AND DWG 65B338079 SH9 REV- 2. ACCOMPLISHED FINAL EI NO. T2023A53M-170 REV1 3. CONDITION CHECK NORMAL AND JOB COMPLETED</P>)SDR UIEA2023030900214None · noneWORN OUT - FOUND MAIN DECK SEAT TRACK WORN OUT STA 1840 LBL 11.33(<P>1. REMOVED THE AFFECTED FASTENER IAW SRM 51-40-02-0G-0 REV96 2. REPAIR DAMAGE AREA IAW EI NO. T2023A53M-270 SEQUENCE A REV0 3. INSTALLED FASTENERS IAW SRM 51-40-02-0G-0 REV96 AND DWG NO. 65B3SDR UIEA2023030900213None · noneFOUND MAIN DECK SEAT TRACK WORN OUT STA 1600 LBL 11.33(<P>1. REMOVED THE AFFECTED FASTENER IAW SRM 51-40-02 REV96 2. REPAIR DAMAGE AREA IAW EI NO. T2023A53M-269 SEQUENCE A REV 0 3. FASTENER INSTALLED IAW SRM 51-40-02 REV96 AND DWG NO. 65B38253 SH48 REV- 4. ACCSDR UIEA2023030900212None · noneFOUND MAIN DECK SEAT TRACK WORN OUT STA 1746 RBL 11.33(<P>1. REMOVED THE AFFECTED FASTENER I.A.W SRM 51-40-02 REV 96 2. REPAIRED DAMAGE AREA I.A.W SRM 53-00-52-2R-12 REPAIR 12 FIG 201 REV96 3. INSTALLED NEW FASTENER I.A.W SRM 51-40-02 REV 96 AND DWG NO. 65B382SDR UIEA2023030900211None · noneCORROSION - FOUND MAIN DECK SEAT TRACK CORROSION AT STA 1928 RBL 98.58(<P>1. REMOVED THE AFFECTED FASTERNER I.A.W SRM 51-40-02 REV-96 2. REPAIRED DAMAGE AREA I.A.W EI NO. T2023A53M-147 SEQUENCE A REV 0. 3. INSTALLED FASTENERS I.A.W SRM 51-40-02 REV9 AND DWG 65SDR UIEA2023030900210None · noneFND M/D CGO FLOOR SEAT TRACK CRACK AT STA 2238 RBL 75.92(<P>1. REMOVED AFFECTED FASTENER IAW SRM 51-40-02-0G-0 REV96 2. REPAIRED DAMAGE AREA IAW SRM 53-00-52-2R-13 REPAIR 13 FIG 201 REV 96 3. INSTALLED NEW FASTENERS IAW SRM 51-40-02-0G-0 REV 96 AND DWG NO: 65BSDR UIEA2023030900209None · noneFND M/D CGO SEAT TRACK CRACK AT STA 940-960 RBL 75.92(<P>1. REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 96 2. REPAIRED DAMAGE AREA IAW SRM 53-00-52-2R-13 REPAIR 13 FIG 201 REV 96 3. INSTALLED NEW PARTS IAW SRM 51-40-02-0G-0 REV 96 AND DWSDR UIEA2023030900208None · noneFND M/D CGO FLOOR STRUCTURE CRACK AT STA 1480, LBL 75.92(<P>1. REMOVED AFFECTED FASTENERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 96 2. REPAIRED DAMAGE AREA IAW SRM 53-00-52-2R-13 REPAIR 13 FIG 201 REV 96 3. INSTALLED NEW PARTS IAW SRM 51-40-02-0G-0 REV 96 ANSDR UIEA2023030900207None · noneFND M/D CGO SEAT TRACK CRACK AT STA 750. LBL 75.92(<P>1. REMOVED AFFECTED FASTERNERS TO GET ACCESS IAW SRM 51-40-02-0G-0 REV 96 2. REPAIRED DAMAGED AREA IAW SRM 53-00-52-2R-13 REPAIR 13 FIG 201 REV 96 3. INSTALLED NEW PARTS IAW SRM 51-40-02-0G-0 REV 96 AND DWGSDR UIEA2023030900205None · noneCORROSION DAMAGE ON INNER SIDE OF FUSELAUGE SKIN BETWEEN STA 1720 AND 1740 AT S-45L(<P>1. REPAIR THE DAMAGE AREA I.A.W SRM 53-00-01-2R-1, REV=96 AND EI NO. T2023A53M-057, REV 1 2. JOB COMPLETED AND COND CHECK NML</P>)SDR UIEA2023030900204None · noneDEFORM - FOUND FWD CARGO, CARGO TRACK DEFORM NEAR STA 590, RBL 24.75(<P>1. REMOVE THE DAMAGE PARTS IAW SRM 51-40-02 REV96. 2. REPAIR THE DAMAGE AREA IAW EI #T2023A53M-110 REV 2. 3. JOB COMPLETED.</P>)SDR CALA2023030900654Frame · crackedFRAME CRACKED THROUGH RIVET HOLE SEEN ON AFT SIDE OF L/H FRAME STA 760 FOR OVERHEAD BIN ATTACH BRACKET BETWEEN STR 8 AND 9L. 155339-0200-0215.ACCOMPLISH A DETIALED VISUAL INSPECTION 37500 CYCLES, WHICHEVER COMES FIRST. FLIGHT CYCLES FROM REPAIR INSTALLATION, O
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