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 C8GA20090040Skin · debondedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE RT INBD AFT FLAP APPROX 30 INCHES FROM THE INBD END UPPER SURFACE IS DIS-BONDED. DAMAGED AREA REMOVED DIM 6.0 INCHES BY 2.5 INCHES. FABRICATED FILLER DIM 6 INCH BY 2.5 INCH AND DOUBLER DIM 9.5 INCH BY 4 INCH SDR C8GA20090039Skin · debondedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE RT INBD AFT FLAP LOWER SURFACE OTBD END DIS-BONDED. DAMAGED AREA REMOVED DIM 3.5 INCH BY 2 INCH. FABRICATED DOUBLER FROM 2024 T3 .016 INCH HOT BONDED REPAIR. NO OTHER DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SDR C8GA20090029Structure · delaminatedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THE LT OUTBOARD AFT FLAP AT WBL. 485 IS DELAMINATED. REMOVED DAMAGED AREA DIM 5.5 INCHES BY 22 INCHES. FABRICATED REPAIR FILLER FROM 2024 T3 .016 INCH DIM 5.5 INCH BY 22 INCH AND DOUBLER FROM 2024SDR C8GA20090028Skin · delaminatedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THE LT OUTBOARD AFT AT WBL 445 IS DELAMINATED. REMOVED DAMAGED AREA DIM 5.5 INCH BY 6.5 INCH. FABRICATED REPAIR FILLER AND DOUBLER FROM 2024 T3 .016 INCH AND HOT BONDED REPAIR. NO OTHER DEFECTS WSDR FDEA200902050461Skin · damagedRT INBOARD FLAP UPPER SURFACE FOUND DEEP SCRATCH 4 INCHES LONG AND DEEP MAX .078 INCHES ON UPPER SKIN, DAMAGE IS "NON/FLIGHT AIRCRAFT STRIKE DAMAGE". REPAIRED SKIN IAW SRM 57-10-00 FIG 85 1-4 VOL I.SDR ASAA0944458Skin · dentedRT WING I/B MID FLAP HAS A DENT 10 INCHES FROM I/B END AND 18 INCHES FROM T/E. REMOVED DAMAGED SECTION OF SKIN, FABRICATED REPAIR DOUBLER, FILLER AND INSTALLED REPAIR IAW B737 400 SRM 57 53 01.SDR ASAA0944457Skin · dentedLT WING O/B MID FLAP HAS A DENT AT THE UPPER SURFACE 117 INCHES FROM O/B END. PREPPED DENT DAMAGE, FABRICATED EXTERNAL REPAIR DOUBLER AND BONDED REPAIR DOUBLER.SDR ASAA0944456Skin · dentedLT WING O/B MID FLAP HAS A DENT AT THE UPPER SURFACE 75 INCHES FROM O/B END. PREPPED DENT DAMAGE, FABRICATED EXTERNAL REPAIR DOUBLER AND BONDED REPAIR DOUBLER.SDR ASAA0944455Skin · dentedLT WING O/B MID FLAP HAS A DENT AT THE UPPER SURFACE 81 INCHES FROM OB END. PREPPED DENT DAMAGE, FABRICATED EXTERNAL REPAIR DOUBLER AND BONDED REPAIR DOUBLER.SDR UIEA200900016Fairing · damagedNR 6 CANOE DAMAGED. PREPARED CLEANED, AND REPAIRED DAMAGE TO CANOE IAW SRM 51-70-07-06-01.SDR UPS09554578Roller · gougedINSPECTION TYPE:C3 LT WING I/B FLAP O/B FWD FLAP TRACK ROLLER IS GOUGED AT UPPER EDGE. BLENDED & TREATED IAW ER 09-1282 DATED 2-3-09.SDR ASAA0944353Skin · dentedLT WING IB AFT FLAP HAS DENT UPPER SURFACE 7.5 INCHES FROM OB END. FABBED REPAIR PARTS AND INSTALLED IAW SRM 51 70 10.SDR SWAA090842Skin · peelingDURING SCHEDULED MV1 CHECK, FOUND LT WING I/B AFT FLAP SKIN PEELING OFF. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWIA200920946Skin · crackedC-CHECK, LEFT NACELLE FLAP HAS CRACKS ON OUTBOARD SKIN. REPLACED LEFT NACELLE FLAP.SDR FDEA200902030431Vane · delaminatedLEFT WING, INBOARD FLAP VANE LOWER SURFACE INBOARD SIDE FOUND DELAMINATION. REMOVED AND REPLACED AS PER AMM 27-50-22-4. ADJUSTMENT CARRIED OUT AS PER AMM 27-50-22-5 FOUND SATISFACTORY.SDR IPXA09855951Skin · chafedINSPECTION TYPE:SV SS#852-W4-20, REPAIR DOUBLER HAS CHAFING DAMAGE, RT INBD FLAP UPPER SKIN XW105 AT FLAP SPAR. REPAIRED PER TIMCO REO-G12768 REV B, AND IPXA EO NR DC8-5750-33483-A.SDR IPXA09855233Rib · misrepairedINSPECTION TYPE:SV SS 852-W4-19, REPAIR DOUBLER HAS 2EA FASTENERS WITH LESS THAN 4D SPACING RT INBOARD FLAP INBOARD RIB XCW 60 14" AND .5" AFT OF FLAP SPAR 2" BELOW UPPER SKIN. REPLACED WEB PER DDWG 5652796 REV H AND DC8 SRM 51-03-00.SDR IPXA09855229Doubler · chafedINSPECTION TYPE:SV SS 852-W4-18, REPAIR DOUBLER CHAFED AT I/B EDGE, RT I/B END LOWER SKIN AT AFT EDGE OF FLAP XCW 60. REPAIRED PER DC8 SRM 51-03-00, AND DDWG 5652796 REV H.SDR SWAA090756Flap · puncturedDURING SCHEDULED SPV CHECK, FOUND LT WING I/B AFT FLAP PUNCTURED. REPAIRED AFT FLAP PER SRM.SDR SWAA090751Flap · crackedDURING SCHEDULED 10Y CHECK, FOUND RT WING O/B T/E AFT FLAP CRACKED. REMOVED AND REPLACED AFT FLAP PER MM.SDR ASAA0944448Rib · crackedDURING INSTALLATION OF ROLLERS ON LT O/B MID FLAP AT CENTER ARM FOUND RIB CRACKED. REMOVED AND REPLACED RIB AT LT O/B MID FLAP IAW B737 400 SRM 51 40 02.SDR UPS09654499Doubler · debondedINSPECTION TYPE:N/A RT WING - I/B AFT FLAP, TRAILING EDGE WEDGE UPPER SKIN, EXISTING REPAIR DOUBLER FOUND DISBOND, REF SURVEY SEQ 304-W4-02. SRM 51-70-10 REPAIR 4 FIG 202 REV 43.SDR SWAA090625Wedge · delaminatedDURING SCHEDULED 26Y CHECK, FOUND RT WING NR 5 SLAT DELAMINATED AT I/B TRAILING EDGE WEDGE. REPAIRED WEDGE PER SRM.SDR FDEA200901290383Structure · crackedCRACK ON LEFT INBD MID FLAP CHORD AT WBL 114. CUT OUT DAMAGED AREA IAW SRM 51-40-3 FIG 1. FABRICATED LOWER SECTION USING EXTRUSION AND SPLICE IAW SRM 51-40-3 FIG 1 AND 57-50-2 FIG 5. INSTALLED REPAIR PARTS IAW SRM 51-30-2.SDR FDEA200901290380Skin · gougedRIGHT WING INBD FORE FLAP IS GOUGED AT OTBD LEADING EDGE IN TWO PLACES. REMOVED PREVIOUS REPAIR IAW SRM 51-30-2. FABRICATED NEW REPAIR PARTS IAW SRM 57-50-2 FIG 3 AND 57-50-4 FIG 1. INSTALLED NEW REPAIR IAW SRM 51-30-2.SDR HNAA2009061900189Bushing · corrodedLT AND RT FLAP TRACK BEAM NR 1 HOLLOW BOLT BUSHING CORRODED. REMOVED AND REPLACED BUSHING IAW MM 57-50-11.SDR UPS09154626Doubler · gougedINSPECTION TYPE:3/C SEQ 144-W3-01 DOUBLER ON LT CENTER FLAP DAMAGED WITH 2 EACH GOUGES AND 3 EACH LOOSE FASTENERS ON UPPER SKIN BETWEEN STR 2.5 AND 2.7, AND RIBS 13-15. REMOVED, FABBED AND INSTALLED REPAIR DOUBLER IAW A300-600, SRM 51-40-00 PG 133, AND 57-50-SDR UPS09154624Doubler · gougedINSPECTION TYPE:3/C SEQ 144-W4-02, I/B FLAP ON RT WING UPPER SKIN DOUBLER GOUGED BETWEEN STR 2.1 AND 2.2, AND RIB 11-16. REMOVED, FABBED AND INSTALLED REPAIR DOUBLER IAW A300-600, SRM 57-50-00 FIG 205, PG 218 AND 51-40-00 PG 5.SDR USAA2009012990221Flap · crackedPHX - PHASE 8 CHECK - MAJOR REPAIR - CRACKED CARBON FIBER ON RIGHT WING OUTBOARD FLAP. REPAIRED RIGHT WING OUTBOARD FLAP IAW A319 SRM 57-53-00.SDR FDEA200901280352Vane · delaminatedRIGHT WING INBOARD FLAP, FLAP VANE LOWER SURFACE FOUND DELAMINATED FROM CENTER VANE TRACK TO OUTBOARD VANE TRACK AREA. REMOVED AND REPLACED AS PER AMM 27-50-22-4. ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-22-5. REPAIR CLASSIFIED AS MINOR PER GMM 6-SDR SWAA090616Flap · delaminatedDURING SCHEDULED 14Y CHECK, FOUND RT WING T/E AT AFT INBOARD FLAP DELAMINATED. REPAIRED FLAP PER SRM.SDR HNAA2009061900191Flap Track · corrodedRT WING FLAP TRACK NR 5 CORRODED. REMOVED AND REPLACED FLAP TRACK IAW MM 57-52-51.SDR HNAA2000906190090Flap Track · corrodedFOUND LT WING NR 4 FLAP TRACK CORRODED. REMOVED AND REPLACE FLAP TRACK IAW 57-50-41.SDR HNAA2000906190091Flap Track · corrodedFOUND LT WING NR 4 FLAP TRACK CORRODED. REMOVED AND REPLACE FLAP TRACK IAW 57-50-41.SDR HNAA2000906190019Flap Track · corrodedFOUND LT WING NR FOUR FLAP TRACK CORRODED. REMOVED AND REPLACE FLAP TRACK IAW 57-50-41.SDR WRLA2009020Structure · crackedDURING C-CHECK INSPECTION IN TPE - CRACK WAS FOUND AT LT WING INBOARD FLAP XIFH230 LOWER TRAILING EDGE L=4 INCHES. REPAIRED CRACK AREA IAW SRM 57-20-00 VOL I FIG 2 REV 40. REF EGAT N/R U05011.SDR UPS09654509Access Panel · debondedINSPECTION TYPE:C LT WING - I/B MAIN FLAP LOWER ACCESS PNL, FOUND DISBOND. SRM 51-70-10 REPAIR 4 FIG 203 REV 43.SDR USAA2009012890205Flap · debondedCLT - Q5 - MAJOR REPAIR - RIGHT OUTBOARD FORE FLAP DISBONDED 30 INCHES FROM OUTBOARD END ON LEADING EDGE. REPLACED RIGHT OUTBOARD FORE FLAP IAW B737 AMM 27-51-37.SDR UPS09654507Doubler · debondedINSPECTION TYPE:C LT WING - I/B AFT FLAP T/E WEDGE UPPER SKIN EXISTING REPAIR DOUBLER FOUND DISBOND, REF SURVEY SEQ 304-W3-08. SRM 51-70-10 REPAIR 4 FIG 202 REV 43.SDR UPS09654647Hinge Fitting · crackedINSPECTION TYPE:C RT WING MAIN FLAP SUPPORT HINGE FITTING FOUND CRACK. RT WING MAIN FLAP SUPPORT HINGE FITTING REPAIRED PER SRM 57-53-02-2R1 FIG 201.SDR UPS09654520Doubler · debondedINSPECTION TYPE:C RT WING - O/B FLAP LOWER FWD ACCESS PNL DOUBLER DISBOND FOUND, REF SURVEY SEQ 304-W4-05. SRM REV 43, 51-70-10, REPAIR 4 FIG 201.SDR UPS09654519Skin · delaminatedINSPECTION TYPE:C LT WING O/B FLAP T/E WEDGE LOWER SKIN EXISTING REPAIR FOUND DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-17 PARA 4A (1).SDR UPS09654508Doubler · debondedINSPECTION TYPE:C LT WING - I/B AFT FLAP T/E WEDGE UPPER SKIN EXISTING REPAIR DOUBLER FOUND TOO CLOSE AND DISBOND, REF SURVEY SEQ 304-W3-06 TO 07. SRM 51-70-10 REPAIR 4 FIG 201 REV 43.SDR UPS09654506Doubler · debondedINSPECTION TYPE:C LT WING - I/B AFT FLAP T/E WEDGE UPPER SKIN, EXISTING REPAIR DOUBLER FOUND DISBOND REF SURVEY SEQ 304-W3-04. SRM 51-70-10, REPAIR 4 FIG 202 REV 43.SDR UPS09654505Doubler · debondedINSPECTION TYPE:C LT WING - I/B AFT FLAP T/E WEDGE UPPER SKIN EXISTING REPAIR DOUBLER FOUND DISBOND, REF SURVEY SEQ 304-W3-09. SRM 51-70-10 REPAIR 4 FIG 201 REV 43.SDR USAA2009012990219Skin · crackedBFM - C1 - MAJOR REPAIR - CRACK IN RIGHT WING INBOARD TRAILING EDGE FLAP UPPER SURFACE. REPAIRED RIGHT WING INBOARD TRAILING EDGE FLAP UPPER SURFACE IAW B737 SRM 57-53-01.SDR SWAA090565Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING O/B AFT FLAP I/B END DELAMINATED. REMOVED AND REPLACED FLAP PER MM.SDR MASA2009012300043Flap · damagedPERMANENT REPAIR TO LT INBD FLAP HOLE DAMAGE.SDR UIEA200900013Skin · damagedLT WING OUTBOARD FLAP, AFT FLAP INBOARD AFT CORNER FROM WBL 502.0 TO 515.0 HAS A GROUND DAMAGED AREA OF 5.5 BY 13.0 INCHES ON COMPOSITE SKIN. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09, FIG 5, SHEET 7 AND 8, 250 DEGREES F CURE PER SRM 51-40-12SDR CNMA20090093Skin · damagedLT OTBD FLAP VANE HAS A SMALL HOLE AT UPPER SKIN ABOVE FLAP OTBD FAIRING. HOLE ON OTBD FLAP VANE REPAIRED WITH EXTERNAL DOUBLER IAW SRM 51-71-00, PAR 16B.
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