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 IPXA10659124Wedge · delaminatedINSPECTION TYPE:C, RT WING OTBD T/E FLAP, T/E WEDGE LWR SURFACE MID AREA DELAMINATION . COMPOSITE WET LAY UP REPAIR CARRIED OUT IAW SRM 51-70-06 PAR 5A (1) FIG 9. REV 46.SDR IPXA10159127Skin · misrepairedINSPECTION TYPE:3C, REPAIR SURVEY 149-W4-01 RT WING OUTER FLAP L/E INBD SKIN FLUSH REPAIR DOES NOT CORRELATE TO THE SRM REPAIR 57-50-00, FIG 208 DO TO A BLIND FASTENER INSTALLED AT SPLICE IN LIEU OF SOLIDS. R & R IAW SRM 57-50-00 FIG 208 AND IAW EO A300-5750-SDR FDEA201003311040Rib · damagedRT INBD FLAP, OUTBD WEDGE, 5TH RIB FROM INBD IS DAMAGED. REMOVED RIB REF SRM 51-35-01, VOL II. FABBED REPAIR DOUBLER FOR WEB REF SRM 57-00-01, FIG 4, VOL I. FABBED NEW "T" CAP REF DAC DWG ARC 2468, REV "D". FABBED SKIN SHIM REF SRM 57-00-01, FIG 85, VOL SDR SWAA101833Skin · delaminatedDURING SCHEDULED 22Y CHECK, FOUND RT WING T/E INBOARD FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FLAP PER SRM.SDR SWAA101820Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING T/E AFT FLAP DELAMINATED AT OUTBOARD EDGE. REMOVED AND REPLACED FLAP PER MM.SDR UALA2010032901045Flap · damagedRIGHT O/B FLAP DAMAGED. REPAIR ACP'D ON C CHECK PACKAGE. TEST FLIGHT SUCCESSFUL FOR FLAP CHANGE.SDR SWAA101787Rib · crackedDURING SCHEDULED 10Y CHECK, FOUND LT WING I/B AFT FLAP L/E RIB CRACKED. REMOVED AND REPLACED RIB PER AAR EA.SDR FDEA201003271021Skin · damagedRT WING OTBD FORE FLAP, INBD L/E WBL 309 TO WBL 314 HAS 2 DEEP GOUGES FROM CONTACT WITH SPOILER PULLEY BOLTS. GOUGES OUT OF LIMITS IAW SRM 57-50-2 ,CUT OUT 2 DAMAGED AREAS DIMS .5" EACH IAW SRM 57-50-4, FABRICATED DOUBLER REPAIR USING 2024T-3 .050 DIMS 7" XSDR 2010FA0000305Skin · damaged( SPUY) DURING ROUTINE C-CHECK INSPECTION, LT WING INBD FLAP - AFT UPPER SURFACE SKIN PANEL SHOWS SCRATCHES AND (05EA) DENTS (STA XW 1.000 - 91.000).SDR 2010FA0000304Skin · dented( SPUY) DURING ROUTINE C-CHECK INSPECTION, RT WING INBD FLAP - FWD UPPER SURFACE SKIN PANEL SHOWS DENTS ( STA XW 104.000-122.000)SDR 2010FA0000303Skin · dented( SPUY) DURING ROUTINE C-CHECK INSPECTION, RT WING OTBD FLAP - AFT LOWER SURFACE SKIN PANEL SHOWS INTERM REPAIR AND DENT ( STA XF375.00-415.00).SDR FDEA201003261013Spar Cap · crackedRT WING INBD FLAP; INBD FLAP WEDGE UPPER INBD L/E CORNER "T" CAP IS CRACKED. REMOVED SPAR CAP REF SRM 51-35-01, VOL II. FABBED NEW SPAR CAP REF DAC DWG ARC 2450, REV "K". ALODINED AND PRIMED SPAR CAP REF SRM 51-21-01, VOL II. SPAR CAP AND SKIN REF SRM 51-71SDR SWIA201024104Skin · crackedLEFT NACELLE FLAP CRACKED LOWER SURFACE, NEAR OUTBOARD HINGE ARM. (C CHECK) INSTALLED DOUBLER PER SRM.SDR IPXA10159117Skin · gougedINSPECTION TYPE:3/C, GOUGED AREA TOP OF CTR FLAP LT WING 72 IN FROM INBD
END. REPAIRED IAW EO A300-5750-37276-A, AND EA 300-5730-01-A223 5 I/R.SDR FDEA201003251006Skin · damagedRT WING, INBD FLAP, LOWER SURFACE, OTBD WEDGE SECTION, JUST BELOW THE OUTBD HINGE FAIRING, APPROX 14 INCHES FROM THE T/E AT STA XW 273.000 HAS SKIN DAMAGE/ PUNCTURE 9" H X 10" W. REMOVED DAMAGED SKIN IAW MD/DC10-10 SRM 51-31-01, VOL II. FABRICATED NEW SKINSDR AALA20100323TUL01Vane · gougedRIGHT WING, WEAR AREA INTO LEADING EDGE OF FLAP VANE, ABOVE INBOARD FLAP TRACK, FOR OUTBOARD FLAP. DID HOT BOND REPAIR PER SRM 51-70-02.SDR SWAA101704Flap · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REMOVED AND REPLACED FORE FLAP ASSY PER MM.SDR RU3A1012Flap Track · corrodedDURING ROUTINE INSPECTION DISCOVERED SEVERE CORROSION ON INBOARD FLAP TRACK (RIGHT WING INBOARD FLAP).SDR ASAA1047569Skin · dentedLEFT O/B FORE FLAP LOWER SKIN HAS CLUSTER OF DENTS. REPAIRED DENT DAMAGE.SDR IPXA10M58902Skin · dentedRT WING INBD FLAP DENT/ PUNCTURE ON LWR SKIN. REPAIRED IAW EO 5750-37012-C.SDR IPXA10558972Skin · chafedINSP TYPE:C4, RT WING INBD FLAP T/E LOWER SURFACE CORNER IS CHAFED. WBL 230 FOUND TO BE OUT OF LIMITS (ON CUSTOMER CARD 849231), REPAIRED IAW SRM 51-70-10-2R, REPAIR 4.SDR USAA2010031890608Flap · delaminatedPHX - B03 - MAJOR REPAIR - DELAMINATION ON LEFT OUTBOARD AFT FLAP BY INBOARD WEDGE. REPLACED LEFT OUTBOARD AFT FLAP IAW JOB CARD R3M27034.SDR IPXA10558896Skin · dentedLT INBD MAIN FLAP LOWER SKIN DENT ON LOWER SURFACE ( 2 EA ) DENTS ARE 8" APART, CENTER TO CENTER. REPAIRED IAW E0 B757-5750-36440-B.SDR AALA20100319TUL01Flap · gougedRIGHT WING, OUTBOARD MID FLAP, MOST INBOARD BULL-NOSE IS GOUGED AT HINGE FAIRING AREA. BLENDED GOUGED AREA AND DYE CHECKED, NO CRACKS FOUND, PER ESO 80559. ALODINED BLENDED AREA, FLUSH FILLED, PRIMED, FABRICATED AND INSTALLED REPAIR DOUBLER, PER EA MD80-57-0SDR FDEA201003190932Wedge · crackedRT WING INBD FLAP AT RIB 25A; TAIL IS CRACKED. REPAIRED RT WING INBD FLAP AT RIB 25A TAIL BY FABRICATING AND BONDING CORE, SKIN, DOUBLER AND BRACKET IAW EA 6-5750-136629 TITLE "WINGS - RT INBD FLAP T/E WEDGE AT RIB 25A".SDR UALA2010031900922Bolt · wrong partREPLACE RIGHT WING NR 2 FLAP ACTUATOR ON ACCT OF CHRONIC LOCKED FLAPS PER CH8644. INSTALLED NR 2 RT WING FLAP ACTUATOR FROM STEP C (3) OF MM. INSTALLED CORRECT LENGTH BOLTS.SDR FDEA201003180881Skin · crackedLT OTBD FOREFLAP, CARRIAGE ATTACH FITTING WBL 348 AREA, CUTOUT, SKIN FWD OF FITTING CRACKED. TRIMMED OUT DAMAGED AREA (DIM: .2500"X.2500") IAW SRM 51-10-1. FABRICATED REPAIR DOUBLER FROM 2024-T3, .063", PO NR 9009353, DIM: 6"X4" IAW SRM 57-50-2, FIG 4. TREATESDR FDEA201003180879Attach Fitting · crackedRT INBD FOREFLAP, CARRIAGE ATTACH FITTING WBL 224, SKIN FWD OF FITTING CRACKED.SDR SWIA201024032Skin · crackedRIGHT NACELLE FLAP LOWER SKIN CRACKED. (C CHECK) REPLACED FLAP PER AMM.SDR ASAA1047562Wedge · delaminatedRIGHT I/B MIDFLAP WEDGE LOWER SURFACE DELAMINATED 1 INCH FROM T/E 44 INCHES FROM I/B END. REPAIRED DAMAGED AREA.SDR SWAA101613Flap · wornDURING SCHEDULED SPV CHECK, FOUND RT WING I/B MID FLAP WORN. REPAIRED MID FLAP PER SRM.SDR SWAA101623Flap · puncturedDURING SCHEDULED HC2 CHECK, FOUND RT WING I/B AFT FLAP PUNCTURED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA101622Flap · puncturedDURING SCHEDULED HC2 CHECK, FOUND LT WING I/B AFT FLAP PUNCTURED. REMOVED AND REPLACED AFT FLAP PER MM.SDR WRLA20100316350Bracket · damagedDURING HARD LANDING INSP FOUND DAMAGE/DENT IN FLAP TRACK BRACKET. PER BOEING REPAIR REF 57-ED-269679, SRE-WLD-10-0001-02B THE BRACKET IS STRUCTURALLY ACCEPTABLE FOR CONT IN SERVICE WITH HFEC INSP EVERY C-CHECK NOT TO EXCEED 24MONTHS.SDR WRLA20100316349Vane · damagedDUE TO HARD LANDING, INSP A PERFORMED AND FOUND LT WING INBOARD FLAP-VANE AFT RT EDGE DAMAGED. DAMAGED SECTION TRIMMED OUT IAW BOEING APPROVAL REF SRE-WLD-10-0001-02B.SDR SWAA101561Flap · corrodedDURING SCHEDULED 20Y CHECK, FOUND LT WING FORE FLAP O/B CORRODED. REMOVED AND REPLACED FORE FLAP PER MM.SDR SWAA101555Skin · delaminatedDURING SCHEDULED 22Y CHECK, FOUND RT WING I/B AFT FLAP LOWER SURFACED DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR SWAA101551Skin · puncturedDURING SCHEDULED SPV CHECK, FOUND LT WING I/B FORE FLAP LOWER SKIN PUNCTURED. REPAIRED FORE FLAP PER SRM.SDR A6WA201040208Fitting · chafedLT OTBD FLAP ALIGNMENT ROLLER FITTING IS CHAFED. BLENDED, ROTOPENNED, TOP COATED AREA IAW REO 601R-57-53-787.SDR A6WA201040209Structure · chafedRT OTBD FLAP INBD EDGE IS CHAFED JUST AFT OF THE ROLLER. BLENDED, ROTO PEENED AND TOP COATED IAW REO 601R-57-53-786.SDR SWAA101510Flap · delaminatedDURING SCHEDULED 14Y CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA101581Flap · delaminatedDURING SCHEDULED MV2 CHECK, FOUND LT WING I/B MID FLAP T/E DELAMINATED. REPAIRED MID FLAP PER SRM.SDR SWAA101506Flap · delaminatedDURING SCHEDULED SPV CHECK, FOUND LT WING I/B FORE FLAP DELAMINATED. REPAIRED FORE FLAP PER SRM.SDR SWAA101505Flap · delaminatedDURING SCHEDULED HC1 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA101435Flap · delaminatedDURING SCHEDULED 14Y CHECK, FOUND RT WING I/B AFT FLAP DELAMINATED ON O/B END. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA101432Flap · chafedDURING SCHEDULED 14Y CHECK, FOUND LT WING O/B MID FLAP L/E CHAFED. REMOVED AND REPLACED MID FLAP PER MM.SDR SWAA101409Flap · delaminatedDURING SCHEDULED 2HC2 CHECK, FOUND LT WING O/B AFT FLAP DELAMINATED. REMOVED AND REPLACED AFT FLAP PER MM.SDR SWAA101393Flap · wornDURING SCHEDULED 14Y CHECK, FOUND LT WING O/B TRAILING EDGE FORE FLAP WORN AREA ON L/E BULLNOSE, AT O/B END. REMOVED AND REPLACED FORE FLAP PER SRM.SDR SWAA101382Flap · delaminatedDURING SCHEDULED 22Y CHECK, FOUND LT WING FORE FLAP T/E DELAMINATED BETWEEN WBL 117 TO WBL 122. REPAIRED FORE FLAP PER SRM.SDR QXEA2010030900163Attach Fitting · damagedRFD - C CHECK - LT OTBD FLAP VANE ATTACH FITTINGS ARE DAMAGED. DAMAGE WAS FOUND TO BE IN LIMITS FOR ATTACH FITTING/BUTE DOOR CAM AT FS 296.07 IAW SRM 57-53-01-101-001-A01. ALLOWED TO HAVE A REMAINING MATERIAL THICKNESS OF .030. CURRENT MATERIAL THICKNESS IS
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