JASC 5753
Service difficulty reports · 31,515
Reports filed under 5753 · Trailing Edge Flaps, 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 = '5753' 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 = '5753' 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 SWAA102928Flap · delaminatedDURING SCHEDULED 16Y CHECK, FOUND RT WING T/E OUTBOARD FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR SWAA102898Flap · corrodedDURING SCHEDULED 16Y CHECK, FOUND RT WING OB/ FORE FLAP CORRODED. REMOVED AND REPLACED FORE FLAP PER MM.SDR SWAA102892Skin · delaminatedDURING SCHEDULED 16Y CHECK, FOUND LT WING O/B FORE FLAP END UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR SWAA102891Skin · delaminatedDURING SCHEDULED 16Y CHECK, FOUND RT WING O/B FORE FLAP END UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR UIEA201000186ASkin · crackedEO 4457A250: MX FOUND THE LT - OTBD MID FLAP LOWER SURFACE WITH A CRACK AND DELAMINATION MEASURING 6.56 FT LONG. DAMAGE IS BEYOND THE SRM LIMITS IAW THE SRM 57-53-01, FIG 101. (ALLOWABLE DAMAGE GENERAL). PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WOSDR HALA2010051800226Structure · corrodedRT INBD T/E MAIN FLAP HAS CORROSION ON UPPER REAR CHORD 18 INCHES OTBD FROM INBD END. UPPER REAR CHORD REPLACED IAW SRM 51-40-02,DWR 0634T210. REV 83.SDR SWIA201024240Flap · crackedRIGHT WING NACELLE FLAP CRACKED ON OUTBOARD SIDE. (C CHECK) REPAIRED PER SRM.SDR SWAA102883Flap · delaminatedDURING SCHEDULED 16Y CHECK, FOUND LT WING FORE FLAP O/B END DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR 2010FA0000538Rib · crackedDURING AN ANNUAL INSP, (1) NOSE RIB WAS FOUND CRACKED IN THE RT FLAP. IT IS THE RIB LOCATED DIRECTLY BENEATH THE ATTACH BRACKET MOUNTED ON THE SKIN.SDR IPXA10560354Skin · chafedINSPECTION TYPE:C2, LT WING OTBD FWD FLAP LWR EDGE OF BULL NOSE IS CHAFED FROM INBD END TO 18 INCHES OTBD WHERE FLAP MAKES CONTACT WITH WING T/E PANEL. REPAIRED IAW ATS ER 10-2910.SDR IPXA10560137Wedge · delaminatedINSPECTION TYPE:C2, RT WING INBD MID FLAP PREVIOUS REPAIR ON UPPER T/E JUST OTBD OF AFT FLAP IS DELAMINATED. REPLACED T/E WEDGE IAW SRM51-40-02-0G AND 51-40-05-0G.SDR IPXA10B59885Skin · damagedLT INBD AFT FLAP LOWER SKIN DAMAGED LOCATION OF DAMAGES NOTED IN EO B7 B747-5700-37548-A. REPAIRED IAW EO B747-5700-37548-B REF LOG PAGE 383520/1/2.SDR IPXA10159887Wedge · damaged.725 HOLE LOCATED RT INNER FLAP T/E WEDGE. REPAIRED IAW EO A300-5750-33456-B.SDR UIEA201000186Flap · brokenDURING APPROACH, CREW SELECTED 25 DEGREE FLAPS AND LOUD THUMP FELT AND HEARD. ACFT ROLLED SLIGHTLY, CREW CORRECTED AND LANDING WAS UNEVENTFULL. ON POST-FLT WALKAROUND, FOUND LARGE SECTION OF RIGHT WING T/E, INBD FOREFLAP, OTBD END MISSSING (APPROX 12 FT.)SEPSDR IPXA10B59876Skin · damagedLT INBD AFT FLAP L/E SKIN DAMAGED. REPAIRED LT INBD AFT FLAP IAW SRM 51-70-07 AND EO B747-5750-37683-A AN D AMM 51-24-11-7.SDR A6WA201040357Lug · gougedLT INBD FLAP AFT LUG FOR INBD HINGE ARM HAS DEEP GOUGE SCRATCH ON INBD SIDE. REPAIRED LT INBD FLAP AFT INBD LUG IAW REO 601R-57-52-1536.SDR AALA20100514TUL04Vane · gougedLEFT NUMBER 5 FLAP VANE IS GOUGED. BLENDED OUT MINOR SCRATCHES AND APPLIED HOT BOND REPAIR PER SRM 51-70-02.SDR AALA20100514TUL03Vane · gougedRIGHT WING FLAP VANES NUMBER 5 FLAP VANE HAS DEEP GOUGES IN UPPER SIDE. INSTALLED HOT BOND REPAIR PER SRM 51-70-2.SDR IPXA10M60180Vane · chafedINSPECTION TYPE:4C, LT WING OTBD FLAP VANE OTBD LOWER EDGE HAS CONTACT DAMAGE. REPAIRED FLAP VANE REF SRM 57-50-80 REPAIR 2 PARAGRAPH 2.A.(2)(A)SDR IPXA10160145Skin · misrepairedINSPECTION TYPE:5YR, REPAIR SURVEY SEQ 164-W3-02 LOCATED BETWEEN RIBS 13 & 15, STGR 2.6 & 2.8 DOES NOT CORRELATE WITH SRM. LT CTR FLAP. REPAIRED LT CTR FLAP REF STA EA 300-5753-01-A2322 IR AND EO A300-5750-37987-A.SDR IPXA10560390Fitting · gougedINSPECTION TYPE:C1, RT WING INBD AFT FLAP IB ROLLER BEARING RIB FITTING LWR FWD EDGE IS GOUGED. REPAIRED RIB FITTING IAW ER NR 10-2789.SDR SWAA102773Flap · puncturedDURING SCHEDULED 12Y CHECK, FOUND RT WING O/B FLAP L/E PUNCTURED. REMOVED AND REPLACED FLAP PER SRM.SDR SWAA102755Flap Track · corrodedDURING SCHEDULED 16Y CHECK, FOUND LT WING NR 2 FLAP TRACK CORRODED AT MOUNT PAD. REMOVED AND REPLACED FLAP TRACK PER MM.SDR SWAA102751Skin · delaminatedDURING SCHEDULED HC1 CHECK, FOUND RT WING O/B AFT FLAP I/B END UPPER SKIN DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR IPXA10160120Skin · misrepairedINSPECTION TYPE:5 YR, REPAIR SURVEY SEQ 164-W3-01 ON LT WING , INBD FLAP LOWER SURFACE OF T/E DOES NOT CORRELATE WITH SRM REPAIRED IAW EA 300-5750-A2316 REV I/R AND UPS EO A300-5750-37927-A.SDR SWAA102738Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR IPXA10659893Fairing · delaminatedINSPECTION TYPE:C, LT WING OTBD T/E FLAP MID L/E FAIRING INBD AREA DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05 PAR 5C, FIG 2.SDR SWAA102698Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING TRAILING EDGE I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA102696Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING TRAILING EDGE I/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA102684Wedge · delaminatedDURING SCHEDULED 14Y CHECK, FOUND LT WING I/B TRAILING EDGE MID FLAP TRAILING EDGE WEDGE DELAMINATED. REMOVED AND REPLACED WEDGE PER MM.SDR DALA109705803Skin · puncturedDURING L-CHECK, FOUND PUNCTURE IN INBD MAIN FLAP LOWER SURFACE AT STA 130. REPAIRED IAW SRM 57-53-01, SRM 51-70-07, SRM 51-70-17.SDR 2010F00106Bracket · out of toleranceDURING ACCOMPLISHMENT OF S/B 777-27A0071, THE FOLLOWING DEFECTS WERE FOUND DUE TO POOR MACHINING DURING FACTORY BUILD. NR 1 T/E FLAP DRIVE ARM ASSY FWD JOINT 1A AND WING SUPPORT BRACKET MACHINED BEYOND S/B LIMITS. NR 2 T/E FLAP DRIVE ARM ASSY AFT JOINT 2B MASDR DLM88101166Guide Vane · nickedNICKS ON INNER SURFACE AT RT WING INBD FLAP OTBD GUIDE VANE. REPAIRED IAW SRM 57-04.SDR IPXA10M60303Skin · delaminatedINSPECTION TYPE:4C, LT WING OTBD FLAP T/E INBD LOWER SURFACE, TAP TESTED AREA HAS DEAD SPOT, POSSIBLE DELAMINATION. REMOVED DAMGE, FABRICATED AND INSTALLED REPAIR PLYS IAW STA SA EA 011-5750-01-A2343 I/R AND UPS EO MD11-5750-38061-A.SDR IPXA10M59920Vane · damagedINSPECTION TYPE:4C, RT OTBD FLAP VANE DAMAGED AT EDGE OTBD END. FABRICATED AND INSTALLED REPAIR REF SRM 57-50-80. REPAIR 2 FIG 201 AND SRM 51-62-01.SDR IPXA10659901Skin · delaminatedINSPECTION TYPE:C, LT WING INBD AFT FLAP UPPER SURFACE INBD AREA FOUND DELAM. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R REPAIR 4, FIG 201 SH.1.SDR IPXA10659846Fairing · delaminatedINSPECTION TYPE:C, LT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATION. FIBERGLASS FABRIC PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05 PAR 5A (1) FIG 5.SDR USAA2010051090937Skin · delaminatedPHX - RON - DELAMINATION ON LEFT INBOARD AFT FLAP AT AF STA 78.3 UPPER & LOWER SURFACES. REPAIRED LEFT INBOARD AFT FLAP AT AF STA 78.3 UPPER & LOWER SURFACES IAW B757 SRM 51-70-04.SDR P5CA2010050701636Wedge · damagedFOUND LEFT I/B AFT FLAP T/E WEDGE WITH TEAR / GROUND DAMAGE WITH A DIMENSION OF 7 X 11 X 1.5 INCHES. FLAP TIME LIMITED REPAIR PER EO 4457A248 WITH FAA 8110-3 DATED 07 MAY 2010. INSTALLED EXTERNAL DOUBLER WITH REPEAT INSPECTION AT EVERY 10 FC AND PERMANENT RESDR IPXA10659916Fairing · delaminatedINSPECTION TYPE:C, LT WING OTBD T/E FLAP MID L/E FAIRING OTBD AREA DELAMINAION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05 PAR 5C, FIG 2.SDR UIEA201000155Skin · damagedON WALK AROUND INSP FOUND DAMAGE ON LT MID FLAP L/E (INBD FLAP). "EO 4457A247: DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS BY INSTALLING AN EXTERNAL REPAIR DOUBLER; SCHEDULE REPEAT INSPECTIONS AT EVERY 15 FC ASDR UALA2010050601534Skin · damagedLT WING OTBD T/E FLAP, AFT FLAP HAS LOOSE SHEET METAL REPAIR ON UPPER SURFACE AFT OF NR 3 SPOILER. AFT INBD CORNER HAS BECOME DISBONDED. WILL REQUIRE METAL BOND REPAIR. STARTNG REPAIR AFTER CONSULTING WITH EG ON ETCHING PRIMER TO BE USED AS MATERIAL LISTED SDR MALA100064Skin · dentedDURING HEAVY CHECK THE LT INBD FLAP PN 601R14002-1, SN SB/RJ/1013 WAS FOUND TO HAVE A DENT IN THE LOWER SKIN AT WS 68.138, 19.125" FROM THE T/E AND MEASURES 1.313" X 1.125" X 0.055" DEEP. DENT ON LT INBD FLAP WITHIN LIMITS TO REPAIR IAW SRM 57-52-00, PERFORMEDSDR SWIA201024638Flap · crackedRIGHT NACELLE FLAP IS CHAFED AND CRACKED. (C-CHECK) REPAIRED PER SRM.SDR IPXA10659767Fitting · crackedINSPECTION TYPE:C, RT WING INBD FLAP INBD HINGE FTG FLANGE AREA FOUND CRACKED. RT WING INBD MAIN FLAP HINGE FTG AT IFS179.75 REPAIRED IAW SRM 57-53-02-2R1, FIG 201, ORG MATL IS 7075T73 FORGING, CRK LENGTH AT INBD FLANGE IS 0.875" AND OTBD FLANGE IS 1" DAMAGEDSDR SWAA102596Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR IPXA10659766Fitting · crackedINSPECTION TYPE:C, LT WING INBD MAIN FLAP INBD HINGE FTG FLANGE FOUND CRACKED. LT WING INBD MAIN FLAP HINGE FTG AT IFS179.75 REPAIRED IAW SRM 57-53-02-2R1 FIG 201, ORG MATL IS 7075T73 FORGING, CRK LENGTH AT INBD FLANGE IS 1.25", OTBD FLANGE IS 1.25" DAMAGED SDR DHLA201000016Skin · damagedACCOMPLISHED PERMANENT MAJOR REPAIR AT WING STA XFS 392.5, IAW EVA 857-00329 REV 1 AND DWG NR D85700329-001-D REV "A" APPROVED BY 8110-3 SIGNED DERT-510080-CE DTD 5-7-10. TRAX W/O 9269, N/R 005717 FOR DETAILS. ACFT WAS GROUNDED.SDR SWAA102569Flap · delaminatedDURING SCHEDULED MV2 CHECK FOUND, RT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR AALA20100501TUL03Flap · damagedDEEP GROVE- TRAILING EDGE OF INBOARD FLAP AT THE OUTBOARD CANOE AREA. INSTALLED DOUBLER WITH HOT BOND PER SRM 51-70-10-2R-2.
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