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 UALA2009061501698Skin · chafedLEFT WING, INBOARD FLAP OUTBOARD UPPER SKIN HAS CHAFING MARKS BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED: FABRICATED AND INSTALLED 2 EACH REPAIR DOUBLERS. ACP'D RIG CHECK OF NR 5 SPOILER TO FLAP CLEARANCE AND ADJUSTED.SDR ASAA0946084Skin · delaminatedLEFT O/B AFT FLAP LOWER SURFACE HAS DELAMINATION ON I/B END. REMOVED DAMAGED AREA, FABBED FILLER AND DOUBLER AND BONDED REPAIR IAW B737 400 SRM 51 70 10 REF 4.SDR ASAA0945985Wedge · dentedLEFT I/B TRAILING EDGE WEDGE LOWER SURFACE HAS CLUSTERS OF DENTS. PREPPED DAMAGED AREAS, FABRICATED, TREATED, PRIMED AND BONDED REPAIR DOUBLER IAW SRM.SDR CALA2009061500311Attach Bracket · damagedFWD I/B MOUNT BRACKET FOR PANEL 572HB IS BROKEN OFF ON LEFT WING I/B FLAP. REPAIRED DAMAGED AREA OF FLAP AT ATTACH BRACKET REF ECRA 5752-0 1395 INTERIM REPAIR. ISSUED DIP FOR PERMANENT REPAIR WITHIN 24 MONTHS HS CTL 94487. ACCOMPLISH A PERMANENT REPAIR WITHSDR SWAA093846Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP PER MM.SDR IPXA09M56433Skin · misrepairedINSPECTION TYPE:1C REPAIR SURVEY SEQ 273-W4-01 RT WING INBOARD FLAP UPPER SKIN BETWEEN STA XIFH165.300 TO XIFH183.300 EXTERNAL DOUBLER DOES NOT CORRELATE WITH SRM. REMOVED REPAIR DOUBLER ON RT WING INBOARD FLAP UPPER SKIN AT STA XIFH16 5.300 TO XIFH183.300. SDR ASAA0995936Seal · wornRIGHT I/B MAIN FLAP ANGLE SEAL LOCATED BELOW I/B AFT FLAP PROGRAM TRACK IS WORN. REMOVED AND REPLACED FLAP ANGLE.SDR SWAA093836Flap · delaminatedDURING SCHEDULED CV CHECK, FOUND RT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA093807Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING I/B FORE FLAP UPPER SKIN DELAMINATED AT O/B EDGE. REMOVED AND REPLACED FORE FLAP PER MM.SDR HALA2009060900030Spar · corrodedMODERATE CORROSION ON REAR SPAR LWR TANG AT XRS 267 (AREA O/B FLAP ACT FITTING). ACCOMPLISHED PERMANENT REPAIR PER BOEING MSSG. NR HWI 09-0047-08B AND DRWG NR J060271.SDR FDEA200906091965Skin · gougedRT INBD FLAP UPPER SURFACE HAS 2 EA DENTS--1. 48 INCHES FROM INBD, 16 " FROM L/E, 2" X 1.5" X .043" 2. 47" FROM INBD, 27" FROM L/E, 1" X 1" X .031" REPAIRED 2 EA GOUGES IAW SRM 57-50-00, FIG 206 SHEET 1.SDR C8GA20090181Skin · delaminatedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE RT WING INBD MID-FLAP UPPER T/E IS DELAMINATED. DAMAGED AREA WAS REMOVED DIM 12.5 INCH X 4 INCH. FABRICATED REPAIR FILLER FROM 2024 T3 .016 INCH DIM 12.5 INCH X 4 INCH AND DOUBLER FROM 2024 T3 .020 INCHSDR C8GA20090153Skin · crackedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE LT OTBD FOREFLAP IS CRACKED AT INBD ATTACK CUTOUT. STOP DRILLED CRACK, PERFORMED HFEC INSP FOR CRACK CONTAINMENT NO FURTHER CRACKS. FABRICATED REPAIR DOUBLER FROM 2024 T3 .063 INCH DIM 6.5 INCH X 7 INCHSDR C8GA20090145Skin · delaminatedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE LEFT WING I/B FOREFLAP UPPER GUIDE PLATE ON TOP IS CRACKED. DAMAGED CHAFE STRIP WAS REMOVED, FABRICATED CHAFE STRIP DIA 3" X 11" FROM 301 1/4 HD .016". INSTALLED BONDED REPAIR, NO OTHER DESDR C8GA20090144Skin · delaminatedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE RIGHT WING I/B MID FLAP UPPER TRAILING EDGE DELAMINATED IN TWO AREAS. DAMAGED AREAS WERE REMOVED APPROX 4" X 3", FABRICATED FILLER FROM 2024 T3 .016" DIM. 4" X 3" AND DOUBLER FROM 2024 T3 SDR C8GA20090143Skin · dentedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE RIGHT WING I/B AFT FLAP UPPER EDGE IS DENTED. REMOVED DAMAGE DIM 3/16" X 1.5", APPLIED POTTING COMPOUND, FABRICATED DOUBLER 5" DIA. FROM 2024 T 3 .016" AND INSTALLED HOT BOND REPAIR.SDR C8GA20090141Skin · dented"SUPPLEMENTAL INFORMATION" WHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE RIGHT WING I/B AFT FLAP O/B UPPER EDGE DENTED. DAMAGED AREA WAS REMOVED 1" DIA, FABRICATED DOUBLER 5" DIA FROM 2024 T3 .016. INSTALLED REPAIR, NO OTHER DEFECTS NSDR C8GA20090140Skin · dentedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTION IT WAS NOTED THAT THE RIGHT WING O/B AFT FLAP IS CRACKED AT THE NR 2 TRACK CUTOUT. DAMAGED AREA WAS REMOVED DIM 1" X 1". FABRICATED REPAIR DOUBLER FROM 2024-0 HEAT TREATED TO T4 .050" DIM 8" X 17". INSTALLED RESDR C8GA20090136ASkin · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE RIGHT WING O/B AFT FLAP IS CRACKED AT NR 2 TRACK CUTOUT. CUT OUT DAMAGED AREA DIM 1" X 1". FABRICATED REPAIR DOUBLER FROM 2024 -0 .050". HEAT TREATED TO T4, INSTALLED REPAIR DIM 6" X 5". NSDR ASAA0945950Flap · chafedLT WING O/B FORE FLAP CHAFED O/B CORNER. REMOVED EXISTING DOUBLER, FABRICATED, TREATED, PRIMED AND INSTALLED NEW REPAIR DOUBLER IAW B737 400 SRM 57 53 01 FIG 201.SDR SWAA093742Skin · crackedDURING SCHEDULED 24Y CHECK, FOUND LT WING TRAILING EDGE I/B FORE FLAP LOWER SKIN CRACKED. REPAIRED SKIN PER MM.SDR SWAA093713Flap · delaminatedDURING SCHEDULED SPV CHECK, FOUND RT WING TRAILING EDGE O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR ASAA0945989Flap · dentedRIGHT I/B FORE FLAP DENTED SEVERAL LOCATIONS. PREPPED DAMAGED AREA. FABRICATED, TREATED AND BONDED (3) DOUBLER REPAIRS IAW B737 400 SRM 51 70 10 REPAIR 2.SDR ASAA0945988Skin · delaminatedLEFT I/B AFT FLAP LOWER SURFACE DELAMINATED. REMOVED DAMAGED SKIN & CORE. FABRICATED, TREATED, PRIMED AND BONDED NEW REPAIR DOUBLER AND CORE IAW B737 400 SRM 51 70 10 REPAIR 4.SDR ASAA0945987Flap · dentedRT WING INBOARD AFT FLAP DENTED 1.5 INCHES FROM T/E 34 INCHES FROM INBOARD END. PREPPED DENTED AREA. BONDED REPAIR IAW SRM 51 07 FAR 4.SDR ASAA0945984Flap · chafedRIGHT O/B FLAP I/B LEADING EDGE CHAPPED. REMOVED DAMAGED DOUBLER, FABRICATED, TREATED, PRIMED AND INSTALLED NEW REPAIR DOUBLER IAW B737 400 SRM 52 53 01 FIG 201.SDR ASAA0945982Doubler · chafedLEFT I/B FOREFLAP UPPER SURFACE REPAIR DOUBLER CHAFED JUST ABOVE CENTER TRACK. REMOVED DAMAGED DOUBLER, FABRICATED, TREATED, PRIMED AND BONDED NEW REPAIR IAW SRM.SDR DL757091132Skin · dentedLT WING I/B FLAP FORE FLAP LOWER SKIN SURFACE APROX WS 165 HAS 3 EA SMALL DINGS / COMPLIED WITH ER/A 474949-14 AT SAA SAT ON N/R CARD 132698 DURING HMVSDR A6WA200940307Skin · dentedMWC 136507-52 - DENT FOUND ON LT INBD FLAP LOWER SKIN W/S 65.0 (9.0 X 8.0 X .160 DEEP). LT INBD FLAP LOWER SKIN W/S 65.0. REPAIRED IAW REO 601R-57-52-1447. (K)SDR CA090609003Bracket · cracked(CAN) DURING A SCHEDULED INSP CRACKS WERE FOUND ON THE RT OTBD FLAP INBD TRACK (LOWER ATTACHMENT) BRACKETS. FURTHER INSP REVEALED THAT THE LWR 2 RIVETS ON EACH OF THE FWD ATTACHMENT BRACKETS WERE NO LONGER HOLDING, 3 RIVETS WERE SHEARED AND THE SECOND RIVET FRSDR ASAA0995903Skin · dentedLT WING INBD AFT FLAP HAS DENTS OUT OF LIMITS. REPAIRED OUT OF LIMITS DENTS.SDR ASAA0995902Skin · dentedLT WING INBD AFT FLAP HAS DENTS OUT OF LIMITS. REPAIRED OUT OF LIMITS DENTS.SDR FDEA200906031999Skin · damagedRT WING INBD FLAP UPPER SKIN DENTED AND CRACKED. FABRICATED SKIN REF. EA. 6-5750-127971, ALODINED AND PRIMED SKIN REF. AMM 51-23-10-00.SDR SWAA093613Skin · delaminatedDURING SCHEDULED SPV CHECK, FOUND LT WING I/B FORE FLAP UPPER SURFACE DELAMINATED FROM O/B END. REPAIRED FORE FLAP PER SRM.SDR IPXA09656302Fairing · delaminatedINSPECTION TYPE:6C LT WING O/B TRAILING EDGE FLAP L/E MID FAIRING DELAMINATION (2 PLACES) AT MID AREA. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-05 PAR 5A (1) FIG 5 REV 44.SDR IPXA09656301Flap · delaminatedINSPECTION TYPE:6C LT WING O/B TRAILING EDGE FLAP L/E MID FAIRING DELAMINATION AT O/B AREA. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5 REV 44.SDR IPXA09656300Fairing · delaminatedINSPECTION TYPE:6C LT WING O/B TRAILING EDGE FLAP L/E MID FAIRING DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-05 PAR 5C FIG 2 REV 44.SDR IPXA09656285Fairing · delaminatedINSPECTION TYPE:6C LT WING - I/B MAIN FLAP O/B LEADING EDGE FAIRING DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03 PAR 5A (1) FIG 5, REV 44.SDR IPXA09656297Hinge Fitting · crackedINSPECTION TYPE:6C LT WING I/B MAIN FLAP I/B AFT HINGE FTG UPPER AREA FOUND CRACK. LT WING I/B MAIN FLAP I/B AFT HINGE FTG UPPER AREA REPAIRED AS PER SRM 57-53-02-2R1 FIG 201 REV 44. THIS REPAIR CLASSIFIED AS A MAJOR REPAIR WITH 10134-2007-7075T6511 AS REPAISDR IPXA09656286Fairing · delaminatedINSPECTION TYPE:6C RT WING O/B FLAP MID L/E FAIRING DELAMINATION. COMPOSITE WET LAY UP REPAIR CARRIED OUT AS PER SRM 51-70-03, PARA 5A (1), FIG 5, REV 44.SDR IPXA09656284Hinge Fitting · crackedINSPECTION TYPE:6C RT WING I/B MAIN FLAP I/B AFT HINGE FTG UPPER AREA FOUND CRACKED. RIGHT I/B MID - FLAP INBOARD AFT HINGE FITTING REPAIR PER SRM 57-53-02-2R1 FIG 201 REV 44.SDR SWAA093569Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING I/B AFT FLAP DELAMINATED ON LOWER SURFACE. REMOVED AND REPLACED AFT FLAP PER MM.SDR IPXA09656174Wedge · delaminatedINSPECTION TYPE:N/A LT WING OUTBOARD FLAP T/E WEDGE DELAM. REPAIRED PER EO-B767-5750-30880-B.SDR SWAA093538Flap · delaminatedDURING SCHEDULED OTS CHECK, FOUND LT WING O/B TRAILING EDGE AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA093496Flap · delaminatedLT WING O/B TRAILING EDGE AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR DALA1317530928Skin · dentedMX FOUND THE DENT OUTSIDE OF ALLOWABLE LIMITS ON RT WING TE FLAP. REPAIR IAW ER/A 475220-14.SDR ABXA200905300027Stiffener · corrodedSTIFFENER CORRODED ON RIGHT I/B FLAP FORWARD SPAR INBOARD END. REMOVED & REPLACED STIFFENER IAW B767 SRM 51-40-02.SDR IPXA09156233Doubler · gouged5 YR REPAIR-SURVEY SEQUENCE NR 160-W4-01 HAS DAMAGE TO PREVIOUS REPAIR GOUGED. REMOVED OLD REPAIR, FABRICATED AND INSTALLED NEW DOUBLER IAW A300-600F 57-50-00 PARA 4E FIG. 205.SDR DL757090943Shim · migratedR/W NR 8 FLAP TRACK CORRODED BETWEEN AFT SHIM AND TRACK. SHIM MIGRATED C/W AT SAA - SAT ON N/R 129961 JOB 82868960001.SDR SWAA093492Flap · delaminatedDURING SCHEDULED MV2 CHECK, FOUND RT WING I/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP ASSY PER MM.
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