Boeing 727-2A1
Service difficulty reports · 502
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = '7272A1' 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 aircraft_model_key = '7272A1' 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 C8GA20090132Tab · delaminatedWHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT THE RT IB AILERON TAB PREVIOUS REPAIR IS DELAMINATED. CUT OUT DAMAGED AREA DIM 5" X 9", FABRICATED REPAIR FILLER FROM 2024 T3 .012" DIM 5" X 9" AND DOUBLER FROM 2024 T3 .012" DIM. 6" X 12". INSTALLED REPAISDR C8GA20090131Skin · canningWHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT THE RT FUSELAGE SKIN AT BS 670 STRINGER 26R HAS OIL CANNING. CUT OUT DAMAGED AREA DIM 2.250" X 2.750", FABRICATED REPAIR DOUBLER FROM 2024 T3 .080 DIM 10.375 X 7.250" AND FILLER FROM 2024 T3 .071" DIM. 10.3SDR C8GA20090130Skin · delaminatedWHILE IN HEAVY MX IT WAS NOTED THAT THE LT WING INBD AFT FLAP IS CRACKED AT EDGE WBL 124. REMOVED DAMAGED SKIN AND CORE DIM 7" X 1.5", FABRICATED REPAIR CORE DIM 7" X .5" FROM 5052-44-3/16 AND 2 EA DOUBLER'S FROM 2024 T3 .016" DIM 5" X 3", 8.5" X 3". HOT BONSDR C8GA20090129Skin · delaminatedWHILE IN HEAVY MX IT WAS NOTED THAT THE LT WING INBD FLAP IS DELAMINATED ON THE LWR T/E. REMOVED DAMAGE AREA, FABRICATED DOUBLER. HOT BONDED REPAIR, NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.SDR C8GA20090128Skin · delaminatedWHILE IN HEAVY MX IT WAS NOTED THAT THE LT WING INBD FOREFLAP IS DELAMINATED ON THE LWR SURFACE NEAR THE INBD END. REMOVED LT INBD FOREFLAP, REMOVED DAMAGE AREA DIM 5" DIA. CIRCLE. FABRICATED DOUBLER FROM 2024 T3 .016". HOT BONDED REPAIR, NO OTHER DEFECTS WESDR C8GA20090127Skin · delaminatedWHILE IN HEAVY MX IT WAS NOTED THAT LT WING OTBD MID-FLAP HAS AN AREA OF DELAMINATION ON THE T/E OTBD END. REMOVED DAMAGED AREA, FABRICATED FILLER AND DOUBLER. INSTALLED HOT BOND REPAIR. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.SDR C8GA20090126Skin · delaminatedWHILE IN HEAVY MX IT WAS NOTED THAT THE LT WING OTBD MID-FLAP HAS AREA OF DELAMINATION ON T/E ON OTBD END. REMOVED DAMAGED AREA, FABRICATED FILLER AND DOUBLER. INSTALLED HOT BOND REPAIR. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.SDR C8GA20090125Stringer · gougedWHILE IN HEAVY MX IT WAS NOTED THAT STRINGER 22L AT STA 1180 HAS A GOUGE ON THE UPPER FLANGE. REMOVED EXISTING STRINGER SPLICE AND FABRICATED NEW STRINGER AND SPLICE. INSTALLED REPAIR, NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.SDR C8GA20090124Skin · damagedWHILE IN HEAVY MX IT WAS NOTED THAT NR 1 AND NR 3 PYLON UPPER SURFACE FASTENERS G AND H ARE PULLED THRU THE PANEL AT ENGINE STA 146 BBL 68. REMOVED PANELS AND FABRICATED NEW PANELS. INSTALLED NEW PANELS. NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SESDR C8GA20090123Skin · misrepairedWHILE IN HEAVY MX IT WAS NOTED THAT THE EXISTING EXTERNAL REPAIR LOCATED AT BS 1179 BETWEEN STR. 20L-23R IS NON-COMPLIANT WITH SRM. THE EXISTING REPAIR WAS REMOVED, HFEC WAS PERFORMED WITH NO DEFECTS. FABRICATED DOUBLER FROM 2024 T3 .071" DIM 18.3" X 11.3", SDR C8GA20090122Skin · misrepairedWHILE IN HEAVY MX IT WAS NOTED THAT THE EXISTING EXTERNAL REPAIR LOCATED AT BS 720A +12 BETWEEN STR. 27L-27R IS NON-COMPLIANT WITH SRM. EXISTING REPAIR WAS REMOVED, HFEC WAS PERFORMED WITH NO DEFECTS. FABRICATED DOUBLER FROM 2024 T3 .100 INCH DIM 30.25 INCH SDR C8GA20090121Skin · delaminatedWHILE IN HEAVY MX IT WAS NOTED THAT THE NR 11 SPOILER OTBD END T/E IS DELAMINATED. DAMAGED AREA WAS REMOVED. FABRICATED REPAIR FILLER, AND REPAIR DOUBLER, INSTALLED BOND REPAIR. NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.SDR C8GA20090120Skin · delaminatedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE NR 12 SPOILER I/B END IS DELAMINATED. DAMAGED AREA WAS REMOVED. FABRICATED REPAIR FILLER, AND REPAIR DOUBLER, INSTALLED HOT BOND REPAIR. NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE.SDR C8GA20090119Skin · misrepairedWHILE IN HEAVY MX IT WAS NOTED THAT THE EXISTING EXTERNAL REPAIR LOCATED AT BS 720B +11 BETWEEN STRINGERS 26R-28R IS NON-COMPLIANT WITH SRM. REMOVED EXISTING REPAIR, PERFORMED HFEC INSPECTION WITH NO DEFECTS. FABRICATED AND INSTALLED TIPPLER FROM 2024 T3 .07SDR C8GA20090118Skin · misrepairedWHILE IN HEAVY MX IT WAS NOTED THAT THE EXISTING EXTERNAL REPAIR LOCATED AT THE LOWER FWD CORNER ON THE R2 DOOR CUTOUT IS NON-COMPLIANT WITH SRM. REMOVED EXISTING REPAIR, PERFORMED HFEC INSP WITH NO DEFECTS. FABRICATED AND INSTALLED TIPPLER FROM 2024 T3 .071SDR C8GA20090117Skin · misrepairedWHILE IN HEAVY MX IT WAS NOTED THAT THE EXISTING EXTERNAL REPAIR LOCATED AT R2 DOOR CUTOUT IS NON-COMPLIANT WITH SRM. REMOVED EXISTING REPAIR, PERFORMED HFEC INSP WITH NO DEFECTS. FABRICATED AND INSTALLED TIPPLER FROM 2024T3 .100" DIM 20" X 21, DOUBLER FROM 2SDR C8GA20090116Skin · misrepairedWHILE IN HEAVY MX IT WAS NOTED THAT THE EXISTING EXTERNAL REPAIR LOCATED AT BS 1188 STRINGER 21L - 22L IS NON-COMPLIANT WITH SRM. REMOVED EXISTING REPAIR, PERFORMED HFEC INSPECTION WITH NO DEFECTS. FABRICATED AND INSTALLED NEW DOUBLER FROM 2024 T3 .071" DIM SDR C8GA20090115Skin · misrepairedWHILE IN HEAVY MX IT WAS NOTED THAT THE EXISTING EXTERNAL REPAIR LOCATED AT BS 297 STRINGER 22R -24R IS NON-COMPLIANT WITH SRM. REMOVED EXISTING REPAIR, PERFORMED HFEC INSP WITH NO DEFECTS. FABRICATED AND INSTALLED NEW FILLER FROM 2024 T3 .040" DIM 17.750" XSDR C8GA20090114Skin · misrepairedWHILE IN HEAVY MX IT WAS NOTED THAT THE EXISTING EXTERNAL REPAIR LOCATED AT BS 342 STRINGER 23R -25R IS NON-COMPLIANT WITH SRM. REMOVED EXISTING REPAIR, PERFORMED HFEC INSP WITH NO DEFECTS. FABRICATED AND INSTALLED NEW FILLER FROM 2024 T3 DIM 20.5" X 11" ANDSDR C8GA20090113Skin · misrepairedWHILE IN HEAVY MX IT WAS NOTED THAT THE EXISTING EXTERNAL REPAIR LOCATED AT BS 1090 STRINGER 17R -19R IS NON-COMPLIANT WITH SRM. REMOVED EXISTING REPAIR, PERFORMED HFEC INSP WITH NO DEFECTS. FABRICATED AND INSTALLED NEW DOUBLER REPAIR FROM 2024 T3 .063" DIM.SDR C8GA20090112Stringer · damagedWHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT STR 27L AT BS 997 IS DAMAGED. REMOVED DAMAGED STRINGER AT 27L FROM BS 980 TO 1008. FABRICATED AND INSTALLED NEW SECTION OF STRINGER PN BAC1498-145 7075 T6. NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNEDSDR C8GA20090111Structure · corrodedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE RT VERTICAL STAB HINGE PIN BEARING HOLE IS PITTED. REMOVED PITTING FROM THE LT BEARING HOLE BY REAMING AND INSTALLED REPAIR SLEEVE PN 69-65750-5. NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVISDR C8GA20090110Intercostal · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE INTERCOSTAL LOCATED AT STA. 950 IS CRACKED BELOW STR. 20 R. REMOVED AND REPLACED CRACKED INTERCOSTAL AT BS 950. NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE.SDR C8GA20090109Stringer · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT STRINGER 27 RIGHT AT BS. 720D HAS CORROSION. DAMAGED ARE WAS REMOVED DIM 48.5". LOCATED AND INSTALLED NEW STRINGER. NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE.SDR C8GA20090106Doubler · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE L1 DOOR LOWER HINGE PREVENTIVE MODIFICATION IS CRACKED AT THE CUTOUT AREA. EXISTING REPAIR WAS REMOVED, FABRICATED NEW 1 EA DOUBLER DIM 19.1 X 9.8 INCHES FROM 2024 T3 .100 INCH AND 1 EA DOSDR C8GA20090105Doubler · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE L1 DOOR HINGE PREVENTIVE MODIFICATION IS CRACKED AT THE CUTOUT AREA. EXISTING REPAIR WAS REMOVED, FABRICATED NEW 1 EA DOUBLER DIM 19.1 X 9.8 INCHES FROM 2024 T3 .100 INCH AND 1 EA DOUBLER SDR C8GA20090104Vent Line · chafedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE NR 1 FUEL TANK UPPER AFT VENT LINE IS CHAFED AT WS 491. FABRICATED DOUBLER FROM 2024-0 .040 INCH DIM 3 X 4.2 INCHES. INSTALLED REPAIR, NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED SDR C8GA20090103Vent Line · chafedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE NR 1 FUEL TANK UPPER AFT VENT LINE IS CHAFED AT WS 601.5. FABRICATED DOUBLER FROM 2024-0 .040 INCH DIM 3 X 4.2 INCHES. INSTALLED REPAIR, NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNESDR C8GA20090101Splice Plate · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE LOWER FLOORBEAM SPLICE AT BS 640 STR 17L WAS CRACKED. SPLICE PLATE WAS REMOVED AND NEW SPLICE PLATE WAS FABRICATED FROM 2024 T3 .125 DIM 18 X 9 INCHES. INSTALLED NEW SPLICE PLATE, NO OTHESDR C8GA20090100Stringer · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT STRINGER 27R STATION 620 HAS CORROSION AND EXISTING STEEL REPAIR REQUIRES REMOVAL. CUT OUT AND REMOVED DAMAGED SECTION OF STRINGER 19 INCHES LONG FROM STA BS 609-628. INSTALLED NEW STRINGER PSDR C8GA20090099Stringer · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT STRINGER 28R STATION 560 AT FRAME HAS CORROSION. CUT OUT DAMAGED STRINGER FROM STA 552 - 569. FABRICATED NEW 17 INCH LONG STRINGER FROM BAC 1498-146 7075 T62 .080 INCH. INSTALLED REPAIR, NO OSDR C8GA20090096Skin · delaminatedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE RT OUTBOARD MIDFLAP T/E WBL 442 IS DELAMINATED. REMOVED DAMAGED AREA 43 X 3 INCHES, FABRICATED FILLER 43 X 3 INCHES FROM 2024 T3 .016 INCH AND 2 EA DOUBLERS 3 X 3 INCHES FROM 2024 T3 .016. HOT BONDED REPAIR, NSDR C8GA20090095Skin · delaminatedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE RT OTBD MID FLAP TRAILING EDGE DELAMINATED AT WBL 442. REMOVED DAMAGED AREA DIM 43 INCH BY 3 INCH. FABRICATED FILLER 2024 T3 .016 INCH DIM 43 INCH BY 3 INCHES AND 2 EA DOUBLERS 3 INCH BSDR C8GA20090094Skin · delaminatedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE RT INBD AFT FLAP TRAILING EDGE DELAMINATED AT WBL 230. DAMAGED OUTER SKIN WAS REMOVED DIM 23.25 INCH BY 2 INCH AND REMOVED DAMAGED CORE 5 INCH BY 2 INCH. FABRICATED NEW CORE FROM 5052-4-SDR C8GA20090093Skin · damagedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE PREVIOUS REPAIR ON THE NR 8 LEADING EDGE SLAT ABOVE HOOK IS DAMAGED. REMOVED PREVIOUS REPAIR, FABRICATED DOUBLER FROM 2024 T3 .125 INCH DIM 7 INCH BY 3.5 INCH AND INSTALLED REPAIR. NO OTSDR C8GA20090092Skin · damagedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE LEFT WING NR 2 SLAT TRAILING EDGE HAS A SMALL PIECE BROKEN OFF. FABRICATED REPAIR DOUBLER FROM 2024 T3 .125 INCH DIM 4 INCH BY 4 INCH AND INSTALLED REPAIR. NO OTHER DEFECTS NOTED. AIRCRSDR C8GA20090091Skin · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS A CRACK WAS NOTED ON THE LEFT WING NR 2 SLAT LEADING EDGE OTBD HOOK SEAL CAVITY. CUT OUT EXISTING FILLER STRIP DIM 7.25 INCH BY 1 5/8 INCH. PERFORMED HFEC NO CRACKS NOTED. FABRICATED DOUBLER FROM AISI 301 .0SDR C8GA20090090Skin · canningWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE NR 2 LEADING EDGE SLAT OTBD END HAS OIL CANNING. OUTER SKIN DAMAGED AREA WAS CUT OUT DIM 1.25 INCH BY 1.875 INCH, CUT OUT INNER SKIN DAMAGE DIM 4.25 INCH BY 5 INCH. FABRICATED COVER, DOUSDR C8GA20090089Skin · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE LEFT WING HAS A CRACK AT THE OTBD CUTOUT OF THE INBD FITTING FOR THE NR 4 SPOILER PANEL. STOP DRILLED CRACK AND VERIFIED CRACK CONTAINMENT. FABRICATED REPAIR DOUBLER FROM 7075 T6 .071 INCSDR C8GA20090088Panel · delaminatedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE LEFT WING NR 1 SPOILER PANEL IS DELAMINATED ON THE UPPER SURFACE. DAMAGED AREA WAS REMOVED DIM 5 INCHES BY 7 INCHES. FABRICATED FILLER AND DOUBLER AND INSTALLED REPAIR. NO OTHER DEFECTS SDR C8GA20090087Panel · delaminatedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE LEFT WING NR 4 SPOILER PANEL IS DELAMINATED ON THE UPPER SURFACE. DAMAGED AREA WAS REMOVED DIM 4 INCH BY 8.5 INCH. FABRICATED FILLER AND DOUBLER AND INSTALLED REPAIR. NO OTHER DEFECTS WESDR C8GA20090086Skin · bulgedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION A BULGE WAS NOTED AT BS 997 AT STR 27L. DAMAGED AREA WAS REMOVED DIM 1 INCH BY 2.250 INCH, FABRICATED FILLER, FABRICATED DOUBLER AND INSTALLED REPAIR. NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERSDR C8GA20090085Skin · canningWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION A DENT AND OIL CANNING WAS NOTED AT BS 1018 ABOVE STR 22R. DAMAGED AREA WAS REMOVED DIM 4 INCHES BY 2.250 INCHES, FABRICATED FILLER FROM 2024 T3 .063 DIM 4 INCHES BY 2.25 INCHES, FABRICATED DOUBLER FROM 2024 T3SDR C8GA20090084Skin · dentedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION A DENT WAS NOTED AT BS 1030 STR 27R NEAR EXISTING REPAIR. REMOVED PREVIOUS REPAIR AND PERFORMED HFEC NO DEFECTS NOTED. FABRICATED NEW FILLER. FABRICATED NEW DOUBLER AND INSTALLED REPAIR. NO OTHER DEFECTS WESDR C8GA20090083Tee Fitting · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE WING CENTER SECTION UPPER LOBE T-CHORD IS CRACKED AT BS 760.9 RBL 24.75. THE T-CHORD WAS REMOVED AND REPLACED AT STATION 740-850 RBL 24.75. NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURSDR C8GA20090082Tee Fitting · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE WING CENTER SECTION UPPER LOBE TEE IS CRACKED AT BS 760.9 LBL 45.50. THE TEE WAS REMOVED AND REPLACED AT STATION 760.9. NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE.SDR C8GA20090081Skin · delaminatedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE RT STAB INBD ELEVATOR TAB HAS DELAMINATION MARKED. REMOVED DAMAGED AREA AND FABRICATED DOUBLER FROM 2024 T3 .012 INCH DIM 3 INCH BY 1.5 INCH. INSTALLED REPAIR, NO OTHER DEFECTS NOTED. ASDR C8GA20090080Support Angle · corrodedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE SUPPORT ANGLE ON THE RT SIDE SKIN TO BULKHEAD AT BS 740 HAS CORROSION. REMOVED AND REPLACED SUPPORT ANGLE. NO OTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE.SDR C8GA20090079Skin · dentedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE RT INBD AILERON HAS 2 DENTS ON THE UPPER SURFACE. DAMAGED AREA WAS REMOVED DIM 4.5 INCH CIRCLE. FABRICATED DOUBLER. INSTALLED REPAIR, NO OTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SDR C8GA20090078Skin · delaminatedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE RT INBD AILERON TAB WAS DELAMINATED. DAMAGED AREA WAS REMOVED DIM 19.5 INCHES BY 5 INCHES. REMOVED DAMAGED CORE DIM 7.5 INCHES BY 3 INCHES. FABRICATED CORE , FABRICATED FILLER AND DOUBL
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