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 IPXA09M55646Wedge · damagedINSPECTION TYPE:3C RIGHT WING I/B FLAP T/E WEDGE HAS A HOLE AT MID T/E. REMOVED DAMAGE, FILLED CUTOUT, AND APPLIED FIBERGLASS PILES IAW MD-11 SRM 57-20-00 PARA 3 FIG 2.SDR IPXA09855424Structure · misrepairedINSPECTION TYPE:SV SEQ 814-W3-27, LT WING DOUBLER I/B FLAP I/B CLOSE-OUT RIB LOWER T/E DOES NOT CORRELATE TO SRM REPAIR. FABRICATED REPAIR PARTS IAW REO-G12645 REV IR.SDR IXXA09SMN013SSkin · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING OUTBOARD FLAP UPPER SKIN CRACKED AT STATION XF 210.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PART. INSTALLED SDR IXXA09SMN011SSkin · scratchedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING INBOARD FLAP UPPER SURFACE SCRATCHED AT STATION XW 120.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, BONDED DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. SDR IXXA09SMN010SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING INBOARD FLAP UPPER SKIN HAS IMPROPER REPAIR AT STATION XW 105.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTSDR ASAA0944272Flap Track · corrodedFOUND LT IB MIDFLAP CENTER FORE FLAP TRACK CORRODED. R&R LT IB MIDFLAP CENTER FORE FLAP TRACK.SDR UPS09554470Skin · damagedINSPECTION TYPE:C2 RT WING I/B FWD FLAP T/E UPPER SURFACE I/B OF AFT FLAP HAS A LIGHTNING STRIKE. REPAIRED PER SRM 51-70-10-2R2 REV 73 SEP 2008.SDR USAA2009012790196Skin · delaminatedCLT - C2 - MAJOR REPAIR - LEFT OUTBOARD FORE FLAP LOWER SURFACE DELAMINATED 4 INCHES OUTBOARD FROM INBOARD EDGE. REPLACED LEFT OUTBOARD FORE FLAP IAW US AIRWAYS JOB CARD 03C30727009/004.SDR FDEA200901210299Hinge Bracket · corrodedRT WING, OTBD FLAP OTBD FWD HINGE AFT LOWER ATTACH HOLES FWD AND AFT FACE FOUND WITH CORROSION. REPAIRED AS PER E.A. 1-5750-127739, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR SWAA090458Flap · delaminatedDURING SCHEDULED 14Y CHECK, FOUND LT WING O/B FORE FLAP DELAMINATED I/B AFT EDGE. REMOVED AND REPLACED FORE FLAP PER MM.SDR FDEA200901210289Stiffener · crackedRIGHT WING FLAP FAIRING 633 CB FWD CENTER STIFFENER ANGLE IS CRACKED. REMOVED STIFFENER IAW A310-200 SRM 51-40-21; PG 22. INSTALLED A NEW STIFFENER IAW A310-200 SRM 51-40-21; PG 9; PARAGRAPH B. THE STIFFENER WAS FABRICATED ON N/R N01416 23416.SDR FDEA200901200280Skin · misrepairedLEFT INBOARD FLAP UPPER SURFACE FOUND WITH EXISTING DOUBLER REPAIR AT OUTBOARD SEGMENT. EXISTING DOUBLER REPAIR AT LT INBOARD FLAP UPPER SURFACE OUTBOARD SEGMENT EVALUATED AND FOUND NOT CARRIED OUT IN ACCORDANCE WITH SRM 57-10-00 FIG 38 VOL I. EXISTING REPSDR UPS09554469Skin · dentedINSPECTION TYPE:C2 LT WING O/B AFT FLAP LWR SURFACE T/E HAS DISBONDED DENT 13.5 INCHES O/B OF I/B END, AND 12 INCHES FWD OF AFT EDGE. REPAIR PER SRM 57-53-2R-1, SRM 51-70-04 FIG 5.SDR UPS09554468Skin · dentedINSPECTION TYPE:C2 LT WING O/B AFT FLAP LWR SURFACE T/E HAS DISBONDED DENT 27.5 INCHES I/B OF O/B END, AND 8.5 INCHES FWD OF T/E. REPAIR PER SRM 57-53-2R-1, SRM 51-70-04 FIG 5.SDR ASAA0944267Skin · damagedRT OB MID FLAP SKIN DAMAGED AT IB END AT EXHAUST GATE CONTROL ROD CUTOUT AREA. REPAIRED RT OB MID FLAP.SDR USAA2009022390424Spindle · corrodedPHL - RON - MAJOR REPAIR - LEFT WING OUTBOARD FLAP INBOARD SPINDLE SHOWING CORROSION FRONT OF FITTING. REPLACED LEFT WING OUTBOARD FLAP INBOARD SPINDLE IAW B737AMM 27-51-44-4 (WBL 254).SDR FDEA200901190261Structure · delaminatedRIGHT WING INBOARD FLAP VANE LOWER SURFACE FOUND WITH DELAMINATION.SDR FDEA200901190250Web · crackedLEFT WING FLAP FAIRING 533 CB HAS A CRACKED WEB. REMOVED AND REPLACED WEB IAW A310-200 SRM 51-40-21; PG 7. THE WEBS WERE FABRICATED ON N/R N01426/23426 AND N/R N01427/23427.SDR ASAA0944277Skin · dentedDENT ON LT IB FLAP. REPAIRED DENTS ON LT IB AFT FLAP LOWER SURFACE IAW B737 400 SRM 51 70 10.SDR SWAA090422Skin · delaminatedDURING SCHEDULED MV2 CHECK, FOUND LT WING O/B AFT FLAP LOWER SKIN DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR ASAA0944312Doubler · delaminatedLT WING OB AFT FLAP TRAILING EDGE REPAIR DOUBLER IS DELAMINATED AT IB CORNER. REPAIR LT OB AFT FLAP IB DAMAGE IAW B737 400 SRM 51 70 10 REPAIR 4.SDR CA090120001Flap Track · crackedPILOT SELECTED FLAPS DOWN THEN NOTICED A ASYMMETRICAL FLAP CONDITION, FLAPS WERE SELECTED UP WHICH RESULTED IN THE CIRCUIT BREAKER POPPING. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THAT THE LEFT OUTBOARD FLAP, INBOARD TRACK HAD FRACTURED NEAR THE SDR ASAA0944332Skin · dentedLT WING OB FORE FLAP HAS A DENT UPPER SURFACE 95" FROM OB END. REPAIRED DENT DAMAGE IAW B737 400 SRM 51 70 10 REPAIR 2.SDR Q2SA746009Panel · detachedON TOP OF CLIMB-OUT, CREW EXPERIENCED AIRFRAME VIBRATION, SUBSEQUENTLY PERFORMING FUEL DUMP (30,000 LBS) AND AIR TURN BACK TO KMIA. ON INSPECTION AFTER LANDING, FORE AND MID-FLAP DAMAGE WAS FOUND ON RIGHT WING, RESULTING FROM RIGHT WING FLIGHT PANEL HAVING DESDR ASAA0944383Skin · dentedLT WING OB MID FLAP HAS A DENT AT UPPER SURFACE 119 INCHES FROM OB END. REMOVED DAMAGED SKINS AT 117" AND 119" FROM OB END. FABRICATED DOUBLERS INSTALLED REPAIR DOUBLERS IAW B737 400 SRM 51 70 10.SDR ASAA0944382Skin · dentedLT WING OB MID FLAP HAS A DENT AT UPPER SURFACE 81 INCHES FROM OB END. REMOVED DAMAGE AT 75" AND 81" FROM OB END. FABRICATED DOUBLERS AND BONDED REPAIR DOUBLERS IAW B737 400 SRM 51 70 10.SDR SWAA090339Wedge · delaminatedDURING SCHEDULED 16Y CHECK, FOUND LT WING INBD MIDFLAP WEDGE DELAMINATED AT OTBD END. REPAIRED WEDGE PER SRM.SDR ASAA0944467Skin · dentedRT WING IB FOREFLAP LOWER SURFACE HAS AREAS OF MULTIPLE SMALL DENTS IN LINE WITH NR 3 AND NR 4 TIRES. REMOVED PREVIOUS REPAIRS FABRICATED REPAIR DOUBLER AND BONDED REPAIR DOUBLER IAW B737 400 SRM 51 70 10 REP 4.SDR UPS09554357Skin · delaminatedTOP SKIN INBD EDGE AFT INBD FLAP DELAM, REPAIRED IAW EO B757-5750-31869-A.SDR SWAA090311Skin · puncturedDURING SCHEDULED 20Y CHECK, FOUND LT WING INBD MID-FLAP T/E WEDGE SKIN PUNCTURED. REPAIRED MID FLAP PER SRM.SDR ASAA0944203Flap Track · corrodedNR 7 FLAP TRACK AFT MOUNT SURFACE CORRODED. R&R FLAP TRACK.SDR IPXA09855414Doubler · gougedINSPECTION TYPE:SV SEQ 814-W3-13 LEFT O/B FLAP UPPER SKIN REPAIR DOUBLER GOUGED STA XF 2 11 8 INCHES FWD OF FLAP FRONT SPAR. FABRICATED REPAIR DOUBLER IAW DC8 SRM 57-02-01 FIG 002Q. INSTALLED REPAIR IAW SRM 51-1-08.SDR IPXA09855187Doubler · gougedINSPECTION TYPE:SV LT OUTBOARD FLAP UPPER SKIN DOUBLER HAS DENT AND SMALL GOUGE XF 345, 9 INCHES FWD OF FLAP FRONT SPAR SS 752-W3-19. REPAIRED PER TIMCO REO-G12585 REV B, AND UPS EO DC8-5720-32341-A.SDR UPS09554612Flap · damagedINSPECTION TYPE:N/A LEFT I/B AFT T/E FLAP DAMAGED ON I/B SIDE DURING EXTENSION OF FLAPS. REMOVED AND REPLACED LT I/B FLAP.SDR UPS09854411Doubler · gougedINSPECTION TYPE:SV SEQ 814-W3-13 LT OUTBOARD FLAP UPPER SKIN REPAIR DOUBLER GOUGED STA XF2118 FWD OF FLAP FRONT SPAR. REPAIRED PER 57-02-01 FIG 2Q.SDR SWAA090287Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING I/B AFT FLAP DELAMINATED AT O/B END. R&R FLAP PER MM.SDR SWAA090252Skin · delaminatedDURING SCHEDULED 6Y CHECK, FOUND LT WING OTBD FLAP T/E DELAMINATED AT UPPER INBD SURFACE. REPAIRED FLAP PER SRM.SDR IPXA09855479Doubler · gougedINSPECTION TYPE:SV SS 814-W4-02 RT O/B FLAP STA XF213 REPAIR DOUBLER, GOUGED. REPAIR ACCOMPLISHED PER TIMCO REO G12583 REV B, DATED 03/26/2009 AND US EO DC8-5720-32905-A, DATED 03/27/2009.SDR IPXA09854904Web · misrepairedINSPECTION TYPE:SV RT INBOARD FLAP XCW 64 REPAIR DOUBLER SURVEY SEQ NO 814-W4-01 MINIMUM FASTENER EDGE DISTANCE LESS THAN 1.5D. REPLACE WEB 51-01-20D.SDR ASAA0944307Skin · delaminatedRT IB FLAP OUTER SKIN PANEL HAS 2 AREAS OF DELAMINATION. REPAIRED RT IB OUTER SKIN DAMAGE ON FLAP IAW B737 400 SRM 51 70 10 REPAIR 3 PG 201.SDR ASAA0944278Skin · dentedLT AFT IB TE FLAP UPPER SURFACE DENTED APPROX 3" IB OF OB EDGE 9" FWD OF AFT EDGE. REPAIRED LT AFT IB TE FLAP UPPER SURFACE IAW SRM 51-70-10.SDR ASAA0944191Skin · dentedLT OB FORE FLAP HAS A DENT FROM CHAFING OB OF NR 1 FORE FLAP TRACK. R&R EXISTING REPAIR DOUBLER REQUIRES REPAIR FASTENER INSPECTIONS AT EVERY C CHECK.SDR FDEA200901110146Bracket · corrodedRIGHT WING INBOARD FLAP OUTBOARD AFT HINGE OUTBOARD PIVOT BORE FOUND WITH CORROSION. REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-52-03. NEW BUSHING FABRICATED AND INSTALLED AS PER E.A. 1-5750-127721. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA200901110143Bracket · corrodedLEFT WING INBOARD FLAP OUTBOARD AFT HINGE INBOARD PIVOT BORE FOUND WITH CORROSION. INBOARD PIVOT BORE AT LT WING INBOARD FLAP OUTBOARD AFT HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-52-03. NEW BUSHING FABRICATED AND INSTALLED AS PER E.A. 1-575SDR SWAA090179Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING INBOARD FORE FLAP LOWER SKIN DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR SWAA090174Wedge · debondedDURING SCHEDULED 20Y CHECK, FOUND RT WING INBD MID FLAP T/E WEDGE DISBONDED. REPAIRED WEDGE PER SRM.SDR UPS09554334Skin · chafedINSPECTION TYPE: C2 RT WING IB T/E MAIN FLAP LWR L/E SURFACE IS CHAFED 85INCHES FROM IB END. REMOVED DAMAGE FROM AREA IAW EO NR757-5750-31831-A.SDR UPS09854309Skin · chafedINSPECTION TYPE:B CHAFING TO RT OUTBOARD FLAP UPPER SKIN AT FLAP STATION XF213 TO XF208. ACCOMPLISH REPAIR PER EO DC8-5750-31844.SDR SWAA090129Flap · delaminatedDURING SCHEDULED 24Y CHECK, FOUND LT WING OTBD FORE FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.SDR SWAA090127Flap · delaminatedDURING SCHEDULED MV2 CHECK, FOUND RT WING OTBD T/E FLAP DELAMINATED AT INBD END. REMOVED AND REPLACED FLAP PER MM.
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