JASC 5101
Service difficulty reports · 482
Reports filed under 5101 · Aircraft Structures, 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 = '5101' 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 = '5101' 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 ASOA06051Unknown · corrodedDURING A C-CHECK IN MCN, CORROSION FOUND AROUND THE NUT PLATE AT FS 459, LBL 42. (M) MAINTENANCE REPAIRED AROUND THE NUT PLATE AT FS 459, LBL 42, IAW REO. (K)SDR IXXA06SMN060SRepair · misinstalledDURING C CHECK, 'NON-STANDARD REPAIR ON FUSELAGE EXTERNAL SKIN (STA 1540.000 - 1550.000,L-17R TO L-19R. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 7 (SHEET 1, 4, 5). REMOVED NON STANDARD REPAIR IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D. REMOVED DAMAGED SECTISDR IXXA06SMN055SPlate · unknownFWD LAVATORY DRAIN MAST BLANKING PLATE AT 460 BL O REPLACES 53-DC8-928. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 09-21-05, AT SKETCH FO3-RO5 REV. B DATED 09-21-05, EO SEMAN 2006112 DATE 01-05-06. REMOVED (02 EA) EXISTING DRAIN MAST IAW DC-8 SRM 51-3-0SDR 06FDEA0349Repair · noneDURING AIRPLANE'S MODIFICATION FROM P TO F/ACF FOUND STA1159 STR 37-40 LT, EXTERNAL REPAIR DOUBLER. NO ACTION REQUIRED. THE REPAIR IS CONFORM TO SRM 53-40-00 FIG 8, PERFORMED E.A. 8-5330-94669 PT 1. NO DEFECT FOUND.SDR 06FDEA0348Repair · noneDURING AIRPLANE'S MODIFICATION FROM P TO F/ACF FOUND BETWEEN STA 421-430 STR 35-36 LT, 1EA FLUSH PATCH WITH INTERNAL DOUBLER. NO ACTION REQUIRED, THE REPAIR IS CONFORM TO SRM 53-20-00 FIG 13 SH 4. PERFORMED EA 8-5330-94667 PT 1 INSPECTION, NO DEFECT FOUNSDR USAA060131Repair · not an sdrAPPROX 33 INCHES OUT FROM INBOARD END OF REMOVABLE L/E PREVIOUS REPAIR. FLUSH REPAIR IAW 55-10-01 REPAIR 2, DEFECT SIZE: 5.5 X 5.5 INCHES.SDR USAA060130Repair · not an sdrAPPROX 33 INCHES OUT FROM INBOARD END OF REMOVABLE L/E PREVIOUS REPAIR. FLUSH REPAIR IAW 55-10-01 REPAIR 2, DEFECT SIZE: 5.5 X 5.5 INCHES.SDR 06FDEA0339Repair · unknownREPAIR LOCATED AT STA LT INBD FLAP LOWER SURFACE XIFH 189-195 REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION USING FAA APPROVED DATA. INSPECTED REPAIR FOUND TO BE OUT OF LIMITS WITH REGARDS TO FAA APPROVED DATA. REMOVED AND REPLACED REPAIR DOUBLER IAW DSDR 06FDEA0337Repair · unknownTHERE IS NO DOCUMENT RECORD THAT THIS REPAIR HAS BEEN EMBODIED ON THE AIRPLANE. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND TO CONFORM REF:RAS DA/ BRE503/92 ASDR 06FDEA0336Repair · unknownTHERE IS NO DOCUMENT RECORD THAT THIS REPAIR HAS BEEN EMBODIED ON THE AIRPLANE. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND TO CONFORM REF:RAS DA/ BRE503/92 ASDR 06FDEA0334Repair · noneTHERE WAS NO DOCUMENTED RECORD OF APPROVED DATA FOUND. IN ADDITION ,THERE WAS NO RECORD THAT THE REPAIR HAS BEEN EMBODIED ON THE AIRCRAFT. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. RSDR 06FDEA0333Repair · unknownTHERE IS NO DOCUMENT RECORD THAT THIS REPAIR HAS BEEN EMBODIED ON THE AIRPLANE. REPAIR REQUIRES EVALUATION FOR MAJOR /MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR IN ACCORDANCE BY REF:RAS DA/HAM -1357-96. RSDR 06FDEA0323Repair · misinstalledFOUND REPAIR LOCATED LT HS683-696. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 55-1SDR 06FDEA0322Repair · misinstalledFOUND REPAIR LOCATED LT HS683-696. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 55-1SDR 06FDEA0321Repair · misinstalledFOUND REPAIR LOCATED LEFT HS683-696. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 55SDR 06FDEA0320Repair · misinstalledFOUND REPAIR LOCATED AT LEFT HS330-350 REPAIR REQUIRES EVALUATION FOR MAJOR - MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRMSDR QXEA200600408Repair · unknownPDX - REMOVE EXISTING REPAIR. LOWER FUSELAGE SKIN STATION X531.5 BETWEEN STRINGER 32S AND 32P. COMPLIED WITH HORIZON AIR EA 2-53-549 AND RD 8-53-7868.SDR USAA060122Repair · unknownSKIN REPAIR - 60 INCHES I/B OF O/B END. UPDATED SDA, DEFECT SIZE: 60 INCHES.SDR 06FDEA0297Repair · noneFOUND LEFT HORIZONTAL STAB INBOARD ELEVATOR UPPER SKIN HAS DOUBLER REPAIR. PERFORMED INSPECTION ON REPAIR IAW SRM 55-10-00 FIG 8 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO# 8-5100-7-5001 P2.SDR 06FDEA0296Repair · noneLT HORIZONTAL STAB FRONT SPAR UPPER SIDE DOUBLER REPAIR. PERFORMED INSPECTION REPAIR IAW SRM 55-20-00 FIG 9 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO NR 8-5100-7-5001 P2.SDR 06FDEA0262Repair · misinstalledFOUND REPAIR LOCATED RT WS 339-339. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO EXISTING SRM REPAIR RIGHT WING INBOARD FLAP REPAIRED PER EASDR 06FDEA0261Repair · misinstalledFOUND REPAIR LOCATED LT FS 4100 AND FS 4120 , FR 76. REPAIR REQUIRES EVALUATION FOR MAJOR /MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO EXISTING SRM REPAIR. REPAIR ACCOMPLISHED SDR 06FDEA0260Repair · misinstalledAGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A DISCREPANCY (N0329): FOUND REPAIR LOCATED LT; FS 3514 AND FS 3567, FR 65 AND FR 66 REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. SDR 06FDEA0256Repair · unknownDURING AIRPLANE'S MODIFICATION FROM P TO F/ACF FOUND: STA 1248-1256, LT SIDE, STR 25-27, EXISTING REPAIR ON JAMB DOOR. ADDED 2 EA RIVETS IAW SRM 53-50-00 FIG 19 SH 1. REPAIR MEETS SRM 53-50-00 FIG 19 REQUIREMENTS.SDR 06FDEA0257Repair · unknownDURING AIRPLANE'S MODIFICATION FROM P TO F/ACF FOUND: RT HORIZONTAL STABILIZER, FOUND REPAIR DOUBLER ON UPPER FRONT SPAR CAP, 4.5 X 18 INCHES. THE EXISTING REPAIR COMPLY ROD SKETCH 94-07-02-006 FOLLOWING FEDEX EO 8-5100-7- 5001 PT 2 CRITERIA.SDR USAA060092Repair · unknownFOUND PREVIOUS REPAIR NR 2 SLAT LOWER T/E SURFACE BELOW ACTUATOR. FABRICATED DOUBLER IAW TR 54-43-01, DEFECT SIZE: 24" BY 4".SDR USAA060091Repair · unknownFOUND PREVIOUS REPAIR UPPER I/B T/E WEDGE SURFACE. FABRICATED DOUBLER IAW TR 57-42-01, DEFECT SIZE: 3" BY 5".SDR USAA060090Repair · unknownFOUND PREVIOUS REPAIR NR 2 SLAT UPPER O/B T/E WEDGE SURFACE. FABRICATED DOUBLER IAW 57-42-02, DEFECT SIZE: 3" BY 5".SDR USAA060089Repair · unknownFOUND PREVIOUS REPAIR STA 179 BETWEEN S-16L AND S-15L. FABRICATED DOUBLER IAW EO 5300V157, DEFECT SIZE: 3" BY 5".SDR USAA060082Repair · unknownFOUND PREVIOUS REPAIR NR 2 SLAT LOWER T/E SURFACE BELOW ACTUATOR. FABRICATED DOUBLER THAT MEASURES 24" BY 4" IAW TR 54-43-01, DEFECT SIZE: 24" BY 4".SDR USAA060079Repair · unknownFOUND PREVIOUS REPAIR I/B T/E WEDGE. DOUBLER INSTALLED IAW TR 57-42-03 DEFECT SIZE: 4" BY 4".SDR USAA060078Repair · unknownFOUND PREVIOUS REPAIR, UPPER T/E SURFACE. DOUBLER INSTALLED IAW TR 57-42-03 DEFECT SIZE: 4" BY 4".SDR 06FDEA0239Repair · damagedSMIS 442 51-00 0007189 03NOV05 MC1 OPEN R WS-C 00031301 MOD TYPE Y MOD NO. 9-AGING-INSP REV NO. PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A DISCREPANCY (N0328): FOUND REPAIR LOCATED RT FS 1605-1658 FR23-24. REPAIRS REQUIRES ESDR 06FDEA0238Repair · correctSMIS 442 51-00 0007189 03NOV05 MC1 OPEN R WS-C 00031301 MOD TYPE Y MOD NR 9-AGING-INSP REV NO. PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A DISCREPANCY (N0324 FOUND REPAIR LOCATED LT FS1067AND FS1091 FR 12 AND FR12A EXT DOSDR 06FDEA0241Repair · unknownEXTERNAL DOUBLER AROUND LT BLOW-OUT PANEL AT BS 1323, BELOW STR 14L, REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR DETERMINED NOT TO BE PER FAA APPROVED DATA AND TO BE A MAJOR RSDR 06FDEA0240Structure · contaminatedPILOT REPORT ACFT WILL TAKE AN ATTITUDE OF 3 DEGREES NOSE UP AT ALL PHASES OF FLIGHT ANY TIME. THE AUTO PILOT IS DISCONECTED. OPEN T.H.S ACCESS PANEL AND NOTICED ACCUMULATION OF WATER ABOUT 14 INCHES HIGH RIGHT BEHIND PRESSURE BULKHEAD. UNPLUGED DRAIN IN SDR USAA060066Repair · unknownFOUND PREVIOUS REPAIR LE VERTICAL FIN 70" DOWN FROM TOP. MAJOR REPAIR: UPDATED SDA AS REQUIRED IAW SRM 55-30-01. DEFECT SIZE: PREVIOUS REPAIR ON VERTICAL FIN REMOVABLE L/E 70" DOWN FROM TOP END 28" BY 18" DOUBLER.SDR USAA060076Repair · unknownFOUND SLAT SKIN WITH PREVIOUS REPAIR, LWR T/E BY AUX TRACK. SDA UPDATED AS REQUIRED IAW TR 54-43-01, DEFECT SIZE: 12" BY 4".SDR USAA060056Repair · unknownFOUND SKIN WITH PREVIOUS REPAIR, BS 178 S17L. EXTERNAL DOUBLER REPAIR IAW SRM 53-30-01, DEFECT SIZE: 2" BY 7".SDR USAA060067Repair · unknownFOUND PREVIOUS REPAIR L/E 81" O/B OF I/B END. UPDATED SDA AS REQUIRED IAW SRM 55-10-01, DEFECT SIZE: PREVIOUS REPAIR FOR RT HORZIONTAL REMOVABLE L/E 81" O/B OF I/B END, FLUSH PATCH.SDR USAA060068Repair · unknownFOUND SKIN WITH PREVIOUS REPAIR, L/E 38" O/B OF I/B END. MAJOR REPAIR, UPDATED SDA AS REQUIRED SRM 55-10-01. DEFECT SIZE: PREVIOUS REPAIR ON SDA FOR LEFT HORIZONTAL REMOVE L/E 38" O/B OF I/B END FLUSH PATCH.SDR USAA060072Repair · unknownFOUND SKIN WITH PREVIOUS REPAIR, 178 BULKHEAD. UPDATED SDA IAW EO 5300V153 DEFECT SIZE: UNKNOWN.SDR USAA060040Repair · unknownFOUND SKIN WITH PREVIOUS REPAIR STA 179 BETWEEN S16R AND S15R. SDA UPDATED AS REQUIRED IAW EO 5300V157, DEFECT SIZE: 3" BY 5".SDR VNAA0601014Skin · ground damageDURING LOADING A BELTLOADER HIT THE FUSELAGE BELOW THE CARGO DOOR. A 6 X 8 AREA OF SKIN WAS PUNCTURED AND DENTED. MAINTENANCE REPAIRED THE FUSELAGE SKIN IAW BSC EO 601R-53-8134. THE FUSELAGE PRESSURIZATION LEAK CHECK WAS GOOD. THE AIRCRAFT WAS RELEASED FORSDR VNAA0601011Structure · lightning strikeDURING APPROACH THE CREW REPORTED A LIGHTNING STRIKE TO THE FUSELAGE NOSE SECTION AND THE RADAR FAILED. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED EN ROUTE & DETAILED LIGHTNING STRIKE INSPECTIONS. DAMAGE WAS FOUND ON THE RADOME, LT HOSDR 06FDEA0166Repair · noneUPPER FUSELAGE AT APPROXIMATELY STA 1781 - 1821 TOP CROWN FORWARD OF NR 2 INLET LIP FOUND DOUBLER REPAIR. PREVIOUS DOUBLER REPAIR AT UPPER FUSELAGE APPROXIMATELY AT STA 1781- 1821 TOP CROWN FORWARD OF NR 2 INLET LIP EVALUATED AND FOUND REPAIR CARRIED OUT ISDR 06FDEA0184Repair · misinstalledEXISTING REPAIRS 2 AT AFT AIR STAIR CUT OUT FWD CORNERS DO NOT COMPLY WITH FAA DATA. REMOVED RT AND LT REPAIR DOUBLERS IAW SRM 51-30-2. PERFORMED HFEC INSPECTION PER NTM-PT6 51-00-00 TO MARK THE END OF CRACKS. NO CRACKS NOTED BEYOND STOP DRILL. FABRICATED SDR 06FDEA0177Repair · noneMAIN CABIN AT STA 1681 AND 1700 X 19 HAS SEAT TRACK REPAIR. PERFORMED INSPECTION OF REPAIR IAW SRM 53-70-00 FIG 2 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.SDR 06FDEA0171Repair · unknownMAIN CABIN AT STA 939 X 19 HAS SEAT TRACK REPAIR. PERFORMED INSPECTION OF REPAIR IAW SRM 53-70-00 FIG 2 VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P2.SDR 06FDEA0170Repair · unknownINTERNAL FUSELAGE AT STA 1154 X-72 FWD PRESSURE BULKHEAD PANEL REPAIR. PERFORMED INSPECTION OF REPAIR IAW SRM 53-40-00 FIG 4A VOL 1 AND FOUND IN COMPLIANCE WITH CRITERIA REQUEST BY EO 8-5100-7-5001 P1.
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