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 ASAA0842945Skin · dentedRIGHT WING TRAILING EDGE I/B AFT FLAP LOWER SURFACE IS DENTED AT WBL 82.25. PREPPED DAMAGED AREA, CUT TO FIT AND INSTALLED PREPREG GLASS IAW B737 400 SRM 51 70 02 REPAIR 2.SDR ASAA0842943Skin · dentedRIGHT WING TRAILING EDGE I/B AFT FLAP LOWER SURFACE DENTED AT WBL 77. PREPPED DAMAGED AREA, CUT TO FIT AND INSTALLED PREPREG GLASS IAW B737 400 SRM 51 70 10 REPAIR 2.SDR MALA080078Skin · chafedHOLE CHAFED IN RT FLAP LEADING EDGE AT WS 225.4 FROM CONTACT WITH AILERON CABLE DAMPER BLOCK. REPAIRED CHAFE DAMAGE BY WET LAYUP REPAIR IAW MESABA EO NR S51031 AND APPLICABLE SECTIONS OF SAAB 340 SRM CH 51-70.SDR ASAA0842894Skin · dentedRIGHT I/B FORE FLAP LOWER SURFACE HAS SEVERAL DENTS AT WBL 73 95. PREPPED AREA, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW B737 400 SRM 51 70 10 REPAIR 2.SDR 08FDEA01610Skin · dentedLEFT WING INBOARD FLAP LOWER SURFACE CENTER LOWER SEGMENT FOUND DENT. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG 17 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR DHL2008760508Fitting · chafedREMOVED AND REPLACED DAMAGED FITTING AT LT INBOARD AFT FLAP AT LWBL 124.2, P/N 65-89086-1, PER B727 SRM 51-30-2 AND 51-30-5.SDR 08FDEA01603Skin · dentedLEFT WING INBD FLAP HAS TWO DENTS LOCATED 65 1/2 INCH AND 61 1/2 INCH OUTBD END AND 14 INCH AND 16 1/4 INCH FROM THE T/E THAT HAVE BEEN FOUND OUT OF LIMITS ON N/R N00417, LABELED D/E ON N/R N00417. FABRICARED DOUBLER & FILLER IAW SRM 57-50-00 FIG 205 PG 219. SDR 08FDEA01601Flap · dentedLEFT WING INBD FLAP HAS TWO DENTS LOCATED 55" AND 57 1/4 " FROM THE INBD ENDAND 7 3/4 " & 5" FROM THE T / E THAT HAVE BEEN FOUND OUT OF LIMITS ON N/R N00417. LABELED A & B ON N/R N00417. FABRICATED DOUBLER IAW SRM 57-50-00; FIG 205; PG 219. LOCATED &SDR 2008UALA02485Flap · delaminatedRT INBOARD TRAILING EDGE FLAP HAS APPROX 10 IN DELAMINATION ON INBOARD TRAILING EDGE. REPAIRED TRAILING EDGE REF SRM 51-70-10 P201 REPAIR 1. ACFT OK FOR SERVICE.SDR 2008UALA02443Skin · chafedRT WING INBD FLAP UPPER SURFACE CHAFED IN AREA OF PREVIOUS REPAIR ON INBD TOP SIDE OF FLAP. ACCOMPLISHED MAJOR REPAIR, REMOVED PREVIOUS REPAIR AND REPLACED WITH PERMANENT REPAIR.SDR 08FDEA01604Skin · dentedLEFT WING FLAP HAS A DENT LOCATED 62 INCHES FROM THE OUTBD END AND 26 INCHES FROM THE T/E THAT HAVE BEEN FOUND TO BE OUT OF LIMITS ON N/R N00417. FABRICATED DOUBLER IAW SRM 57-50-00. LOCATED & DRILLED IAW SRM 57-50-00. ALODINED IAW SRM 51-21-10. PRIMED IAW SDR 08FDEA01562Rub Strip · damagedRIGHT WING INBD FLAP UPPER SKIN RUB STRIP IS WORN. REMOVED & REPLACED THE CHAFE / RUB STRIP IAW SRM 57-50-00.SDR 08FDEA01543Structure · wornFOUND ON LT INBOARD FLAP DURING ACCOMPLISHMENT OF SB A300-57-6100 SOME HOLES OVERSIZED. REPAIR PERFORMED BY VERIFICATION OF OVERSIZED HOLES IAW RAS/FOK/040/2008 ISS A, APPROVED BY EA 6-5752-115278.SDR UPS08M52986Fairing · gougedINSPECTION TYPE:C, RT WING IB FLAP ELEPHANT EAR FAIRING FOUND GOUGED AND DENTED. RT WING IB FLAP, IB FAIRING, REMOVED IAW CMM57-52-03 R61. GOUGED AND DENTED AREAS MEASURED, EVALUATED & FOUND OUT OF LIMIT IAW SRM57-00-01 VI R35. DAMAGED SKIN PORTION ON RT WINSDR 08FDEA01628Skin · dentedRT WING INBD FLAP LWR SKIN HAS A NUMBER OF DENTS. MEASURED DEEPEST DENT TO BE D= .028 INCH DEEP AND X= .500" WIDE. FOUND TO BE WITHIN LIMITS PER SRM 57-50-00 PG 101 DEPTH GAUGE NR T8492F. GOUGE BLENDED ORIG MAT .031" REMAINING .021, REMOVED .010" FOUND TO SDR SWAA082224Flap · debondedDURING SCHEDULED 22Y CHECK, FOUND RT WING INBOARD T/E AFT FLAP INBOARD END DISBONDED. REPAIRED FLAP PER SRM.SDR SWAA082175Flap · delaminatedDURING SCHEDULED BRDG CHECK, FOUND RIGHT WING OUTBOARD T/E AFT INBOARD END DELAMINATED. REMOVED AND REPLACED FLAP PER MM.SDR SWAA082172Skin · delaminatedDURING SCHEDULED BRDG CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP INBOARD UPPER AND LOWER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM.SDR 2008UALA02404Structure · gougedRT OB TRAILING EDGE FOREFLAP HAS GOUGE APPROX .020 IN DEEP LOCATED .75IN INBD OF WBL 414.38. REPAIRED THE RIGHT HAND OUTBOARD FORE FLAP LEADING EDGE.
SDR 08FDEA01518Fairing · dentedLEFT WING FLAP FAIRING 535 AT IS DENTED. REPAIR BY REMOVING THE DAMAGE & APPLYING A CORE; CLOSING PLIES AND A FIBERGLASS OVERLAY REPAIR IAW SRM 57-20-35. APPLIED AN ANTI-STATIC COATING IAW SRM 51-23-20. APPLIED PORE FILLER & PRIMER IAW SRM 51-75-10. PREPPED SDR 08FDEA01517Fairing · delaminatedLEFT WING FLAP FAIRING 535 AT IS DELAMINATED. REPAIRED BY REMOVING THE DAMAGE & APPLYING A CORE; CLOSING PLIES AND A FIBERGLASS OVERLAY REPAIR IAW SRM 57-20-35. APPLIED THE ANTI-STATIC COATING IAW SRM 51-23-20. APPLIED PORE FILLER & PRIMER IAW SRM 51-75-1SDR 08FDEA01516Fairing · erodedLEFT WING FLAP FAIRING 534 AB L/E IS ERODED IN 2 AREAS. REMOVED DAMAGE & LAYED UP REPAIR PLIES & STARTED CURE. COMPLETED CURE & SANDED. APPLIED ANTI-STATIC COATING; APPLIED FR PRIMER & APPLIED PAINT.SDR 08FDEA01515Fairing · erodedLEFT WING FLAP FAIRING 535 AB L/E IS ERODED IN 2 AREAS. REMOVED FINISH & DAMAGE AT 2 AREAS TOP & BOTTOM OF THE FAIRING IAW SRM 57-20-35. LAYED UP; BAGGED & CURED REPAIRS IAW SRM 57-20-35. REINSTALLED SEAL PARTIALLY REMOVED TO F.O.M. & RESTORED FINISH IAWSDR 08FDEA01514Panel · erodedLEFT WING FLAP FAIRING 532 BB LEADING EDGE IS ERODED. REMOVED DAMAGE AND REPAIRED BY APPLYING FIBERGLASS WET LAY UP IAW SRM 57-20-35 & E.A. 6-5720-118496.SDR 08FDEA01513Fairing · puncturedLEFT WING FLAP FAIRING 535 BB IS PUNCTURED ON THE FWD LOWER SECTION. REMOVED DAMAGE & APPLIED A WET LAY-UP IAW SRM 57-20-35.SDR 08FDEA01512Fairing · dentedLEFT WING FLAP FAIRING 534 BB IS DENTED ON THE LOWER FWD SECTION. REMOVED DAMAGE AND APPLIED A WET LAY-UP IAW SRM 57-20-35 & RESTORED FINISH IAW SRM 57-75-10 & AMM 51-23-10-0.SDR 08FDEA01511Fairing · puncturedLEFT WING FLAP FAIRING 533BB FWD SECTION IS PUNCTURED INTERNALLY. REMOVED DAMAGE FROM PANEL; FABRICATED REPLACEMENT CORE PLUG; POTTED CORE & STARTED CURE; COMPLETED CURE & SANDED; LAYED UP REPAIR PLYS UNDER VAC BAG & STARTED CURE; COMPLETED CURE & LSDR 08FDEA01509Rub Strip · chafedLEFT WING INBD FLAP UPPER SURFACE CHAFING PLATE IS PEELING AND WORN. REMOVED &B REPLACED THE CHAFE STRIPS IAW SRM 57-50-00; PARA 3-G; FIG 207.SDR 08FDEA01508Rub Strip · delaminatedRIGHT WING FLAP UPPER SKIN RUB STRIP IS DELAMINATED AT 3 SPOTS. REMOVED & REPLACED THE CHAFE / RUB STRIP IAW SRM 57-50-00; PARA 3-G FIG 207.SDR 08FDEA01501Fairing · delaminatedRIGHT WING FLAP FAIRING 636 AB LEFT SIDE UPPER POINT IS DELAMINATED. REMOVED FINISH AND DAMAGE IAW SRM 57-20-35. LAYED UP & CURED REPAIR PLYS IAW SRM 57-20-35 PAPAGRAPHS 5; G-M. APPLIED FINISH IAW SRM 51-75-10.SDR 08FDEA01499Fairing · dentedLEFT WING FLAP FAIRING 536 AB RIGHT SIDE HAS A DENT. REPAIRED THE DENT BY REMOVING THE DAMAGED AREA, POTTING THE CORE, APPLYING A WET LAY UP REPAIR AND REFINISHING THE AREA IAW SRM 57-20-35.SDR UPS08852277Frame · crackedINSPECTION TYPE:C3 LT OUTBD FLAP LE SUPPORT FRAME CRACKED IN LOWER ATTACH ANGLE RADIUS INBD FROM STA 340 HINGE. FABRICATED AND REPLACED LT OUTBD FLAP LE ATTACH ANGLE INBD OF STA 34 0 IAW DWG 5655752, SRM 51-01-24, SRM 51-01-24, SRM 51-01-20D.SDR SWAA082143Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING INBOARD FOREFLAP UPPER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM.SDR UPS08852194Skin · wornINSPECTION TYPE:C3 DOUBLER LOOSE, WORN AND NUMEROUS SCREWS PULLING THROUGH ALONG BOTTOM EDGE OF LEFT OUTBOARD FLAP L/E BETWEEN 219 AND 340. REPAIRED BOTTOM EDGE OF OUTBOARD FLAP L/E AT STA 219 AND 340 IAW SRM 57-07 -01-0, SRM 57-02-00-0 FIG 002, SRM 57-01-08 SDR 2008UALA02304Structure · damagedRT INBD FWD FLAP LWR SURFACE HAS 1-2 INCH HOLE FROM EMBEDDED ROCK 1 FOOT FROM INBD EDGE AND 6 INCH FROM TRAILING EDGE. FOUND FOD DAMAGE. REPLACED INBOARD FORE FLAP PER MM 27-51-07. ACFT OK FOR SERVICE.SDR SWAA082126Carriage · wornDURING SCHEDULED MV2 CHECK, FOUND LT WING NR 2 MID FLAP CARRIAGE ASSY BEARING SUPPORT WORN. REMOVED AND REPLACED FLAP CARRIAGE PER MM.SDR SWAA082125Carriage · wornDURING SCHEDULED MV2 CHECK, FOUND LT WING NR 1 MID FLAP CARRIAGE ASSY BEARING SUPPORT WORN. REMOVED AND REPLACED FLAP CARRIAGE PER MM.SDR SWAA082127Carriage · wornDURING SCHEDULED MV2 CHECK, FOUND LT WING NR 7 MID FLAP CARRIAGE ASSY BEARING SUPPORT WORN. REMOVED AND REPLACED FLAP CARRIAGE PER MM.SDR IXXA08SMN175SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT OUTBOARD FLAP TRAILING EDGE LOWER SKIN IMPROPER REPAIR AT STATION XF 370.000 - 404.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, AND DOUBLER. BONDED PARTS ASSDR IXXA08SMN174SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT HAND INBOARD FLAP UPPER SKIN HAS DENTS BETWEEN STATION XW 104.000 TO STATION XW 115.000.REMOVED FASTNERS AS NEEDED TO PERFORM REPAIR.REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, AND BONDED DOUBLER. BONDED PARTS AS NSDR EIA2008018Structure · damagedAIRCRAFT TOOK BIRDSTRIKE OUT OF JFK, ON BIRDSTRIKE INSP AT DOV FOUND RT OUTBOARD FOREFLAP LEADING EDGE DAMAGE. REMOVED AND REPLACED RIGHT WING OUTBOARD FOREFLAP ASSY IAW MM 27-51-05SDR SWAA082100Skin · debondedDURING SCHEDULED SPV CHECK, FOUND LT WING INBOARD T/E AFT FLAP LOWER SURFACE DISBONDED. REMOVED AND REPLACED FLAP PER MM.SDR QXEA200800408Flap · chafedPDX C4 CHECK RT O/B FLAP HAS A CHAFFED AREA AT THE O/B END APPROX 10" FROM THE TRAILING END. BLENDED ARE OF CHAFE, FOUND OUT OF LIMITS IAW -8 200 SRM 57-50-16. HFEC INSP. IAW -8 200 NDTM PT 6, 51-00-01. NO CRACKS NOTED. UT THICKNESS CHECK IAW -8 200 NDTM PSDR IXXA08SMN158SSkin · wornDURING ROUTINE C CHECK INSPECTION; FOUND LEFT INBOARD FLAP UPPER SKIN WORN AT STATION XW 104.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASDR IXXA08SMN152SSkin · dentedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING INBOARD FLAP UPPER SKIN DENTED AT STATION XW 104.000 TO 115.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN, BONDED DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. SDR IXXA08SMN124SSkin · misrepairedDURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP UPPER PART WITH IMPROPER REPAIR AT STATION XW -2.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. SDR KNNA20080009Skin · delaminatedDELAMINATION OF LEFT WING INBOARD AFT FLAP TRAILING EDGE WAS ORIGINALLY FOUND TO BE WITHIN LIMITS SO SPEED TAPE WAS APPLIED AS A TEMPORARY REPAIR AND THEN PLACED ON CARRY OVER. THE FLAP WAS MONITORED UNTIL THE CONDITION DETERIORATED BEYOND LIMITS SO IT WAS RESDR UIEA200800156Panel · delaminatedNR 1 KNEE CAP PANEL UNDER SURFACE DELAMINATED. REPAIRED PER EO NR 4757A431 AND SRM 51-40-14 AND 51-40-15.SDR 08FDEA01425Skin · looseRT WING OUTBD FLAP NR 80 FASTENERS LOOSE ON LOWER SKIN. REPAIR AREA IAW SRM 57-20-00 FIG.11 VOL.I.SDR UIEA200800157Flap · perforatedLEFT INBOARD FOREFLAP PERFORATED APPROX 12 INCH INBOARD FROM IT'S OUTBOARD EDGE APPROX WS 1178. REPAIR CARRIED OUT IAW EO NR 4757A432.
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