JASC 5753
Service difficulty reports · 31,513
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 SWAA2018082224512Skin · delaminatedRT WING OUTBOARD AFT FLAP UPPER SKIN DELAMINATED. REPAIRED AFT FLAP PER SRM.SDR SWAA2022021746502Flap · delaminatedR/H WING OUTBOARD AFT FLAP DELAMED AT INBOARD TRAILING EDGE / REMOVED AND REPLACED R/H O/B AFT FLAP PER M/M. REF. 27-51-22. CLEARANCE AND OPS CHECK GOOD.PN OFF: 113A3700-26 SN OFF: S1306-30PN ON: 113A3700-12 SN ON: 000789SDR SWIA2018091245063Guide Plate · chafedLT OUTBOARD FLAP CENTER HINGE ARM INBOARD GUIDE PLATE CHAFED. (C-CHECK) RO: 09/12/2018. REMOVED AND REPLACED WITH NEW INBOARD GUIDE PLATE P/N: 601R14629-111 IAW SRM.SDR FDEA2018082102133Fairing · damagedRIGHT WING FLAP FAIRING 632BB, AFT INNER SURFACE HAD COMPOSITE CHAFED. A SECTION WAS MISSING. BONDED AND REPAIRED THE RT WING FLAP FAIRING IAW SRM 57-20-35, AND EA T 6-5710-T0341633. MAJOR REPAIR.SDR SWAA2018082024446Flap · delaminatedRT WING OUTBOARD AFT FLAP DELAMINATED AT INBOARD TRAILING EDGE. R&R AFT FLAP PER MM.SDR IPXA2018082753204Skin · dentedLEFT WING CENTER FLAP WAS DENTED BETWEEN RIBS 14 AND 15, -10.5 FROM FRONT SPAR AND 79 INCHES FROM FLAP INBD EDGE. REPAIRED THE FLAP IAW REO-G20545, REV IR.SDR FDEA2018082182110Skin · crackedRT CENTER FLAP, RIB 11 HAD TWO CRACKS, AT FIRST AND SECOND STRINGER FWD OF THE REAR SPAR. REPAIRED THE FLAP IAW SRM 57-50-00, FIG 201, AND FIG 205. MAJOR REPAIR.SDR FDEA2018082182106Skin · puncturedSMALL PUNCTURE ON THE UPPER SURFACE SKIN OF THE LT INBOARD MAIN FLAP, IFS 256. REMOVED DAMAGE AND REPAIRED IAW SRM 57-53-01-2R, REPAIR 1, AND 51-70-17-0G.SDR SWAA2022021768712Flap · delaminatedSUPPLEMENTAL INFORMATION: WHILE PERFORMING PHASE I INSPECTION; FOUND ENVIRONMENTAL DELAMINATION OF THE RIGHT OUTBOARD AFT FLAP TRAILING EDGE WEDGE INBOARD BOTTOM CORNER; APPROXIMATELY 1' VERTICAL PLANE AND 2' HORIZONTAL PLANE. / PERMANENTLY REPAIRED DELAMINATISDR ABXA2018082017091Beam · gougedGOUGES ON THE INBOARD FLAP INBOARD TRAILING EDGE BEAM AT WING STATION 344.3. THE BEAM WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR AALA201808249027Fitting · wornRIGHT WING INBOARD FLAP INTERCONNECTING STRUT ATTACH FITTING HAS EXCESSIVE PLAY. REPLACED FITTING IAW SRM 51-72-11 AND AIRBUS DRAWING D57570280.SDR ASOA201808207150Skin · delaminatedRIGHT WING INBOARD FLAP HAD AREAS OF DELAMINATION AT APPROXIMATELY 14 INCHES FROM INBOARD END. REPLACED THE CORE THROUGH THE BOTTOM SKIN.SDR UIEA2018081601718Shim · migratedSHIM MIGRATED AT RIGHT WING OUTBOARD FLAP TO ROAR SPAR, INBOARD FLAP FITTING. APPLIED TORQUE CHECK CHECK AT RIGHT WING O/B FLAP I/B FITTING ATTACHING BOLT IAW SRM 51-40-04. 51-20-12.SDR SRXR201808160016Vane · corrodedFOUND HEAVY CORROSION AND DEEP PITTING ON THE RT INBD FLAP VANE AT THE INNER AND OUTER ATTACH POINT INNER RIBS. REMOVED AND REPLACED THE FLAP VANE IAW AMM 27-50-22.SDR A6WA2018081645979Skin · dentedRIGHT INBOARD FLAP LOWER SKIN HAS AREAS OF DENTS FROM WS 75.0 TO 50.5. REPAIRED RIGHT INBOARD FLAP LOWER SKIN IAW SRM 57-52-00.SDR AALA2018110759038Strut · corrodedCORROSION ON THE RIGHT WING TRAILING EDGE FLAP INTERCONNECTING STRUT TARGET. REPLACED THE INTERCONNECTING STRUT IAW AMM 27-51-44.SDR A6WA2018081445978Skin · chafedLEFT INBOARD FLAP VANE LEADING EDGE CHAFED AT WS 57.0. REPLACED THE FLAP VANE L/E SKIN IAW IAW SRM 51-42-13.SDR REXA20180829732Landing · crackedDURING GVI OF THE LT INBD FLAP VANE, FOUND A CRACKED ACCESS PANEL LANDING. REMOVED AND REPLACED THE ACCESS PANEL LANDING ON THE INBD FLAP VANE IAW SRM 51-42-13.SDR IPXA2018082433184Skin · dentedINSPECTION TYPE:12YRLEFT WING CENTER FLAP LOWER SURFACE HAS NUMEROUS DENTSREPAIRED IAW UPS EO A300-5750-69637-A AND HAECO REO G21541 REV IR BY CUTOUT OF DAMAGE AND INSTALLATION OF REPAIR DOUBLER.SDR Q2SA2018091410394Skin · crackedAIRCRAFT GROUNDED. DURING LINE CHECK, THE LT INBD AFT FLAP [P/N 113W2700-13; S/N 001043] LOWER SKIN PANEL CRACK FOUND. LT INBD AFT FLAP LOWER PANEL [113W2831-15] REPLACED IAW SRM, DRAWING, AND EO 1957A353 PART 3.SDR IPXA2018082743195Skin · dentedLEFT WING CENTER FLAP TRAILING EDGE, LOWER SKIN BETWEEN RIB 17 AND 18, DENTED. REPAIRED THE LT WING FLAP IAW EO A300-5750-69636-A, AND REO G21540 REV IR.SDR A6WA2018081345974Skin · chafedRIGHT INBD FLAP VANE L/E SKIN WAS CHAFED. REPLACED FLAP VANE IAW SRM 51-42-13.SDR A6WA2018081345975Skin · chafedRIGHT INBD FLAP VANE SKIN WAS CHAFED. REPLACED THE FLAP VANE SKIN IAW SRM 51-42-13.SDR SWAA2022022258309Skin · delaminatedL/H OUTBOARD AFT FLAP HAS DELAMINATION ON UPPER SURFACE INBOARD AFT CORNER. / APPLIED REPAIR IAW SRM 57-53-01-2R-4 AND SRM 51-70-10-2R-4.SDR A6WA2018081345973Flap · damagedLT WING TE FLAP DAMAGED. REPAIRED IAW SRM 57-52-00.SDR UIEA2018080701631Flap · damagedLT O/B MID FLAP O/B LE DAMAGED. REPAIRED DAMAGE OF LT O/B MID FLAP O/B LE PER SRM 51-53-01-2R-1 DETAIL IV AND SRM 51-70-07-05-0 PAR 5C.SDR SIMA20180807001Rib · damagedRIGHT OTBD FLAP, OTBD ROLLER BUSHING BORE WAS SCORED. REMOVED AND REPLACED THE RT RIB 19 IAW ERS-EM-57MR-1001 R1.SDR CA180808018Support Beam · cracked(CAN) LT NACELLE, OUTBOARD FLAP TRACK NR 3 SUPPORT BEAM FOUND CRACKED 0.75` ALONG RADIUS APPROXIMATELY 6` FWD OF XN210.00. THE BEAM IS A PRINCIPLE STRUCTURE ELEMENT THAT SUPPORT THE NR 3 FLAP ROLLER TRACK. NO INDICATION OF DEFORMATION OR INDUCED DAMAGE NOTEDSDR DALA2018080704895Trunnion · damagedFOUND THE LEFT INBD FLAP TRUNNION DAMAGED, REPLACED THE TRUNNION FITTING IAW AMDS 2750-6010-LT AND CMM 57-52-21.SDR A6WA2018080645967Skin · dentedLEFT INBD FLAP, LOWER OTBD SKIN PANEL HAD TWO DENTS. REPLACED THE FLAP SKIN PANEL IAW SRM 51-42-13SDR A6WA2018080645966Skin · dentedRIGHT INBD FLAP, LOWER INBD SKIN PANEL HAD MULTIPLE AREAS OF DENTS, DINGS, AND PITS. REPLACED THE FLAP SKIN IAW SRM 51-42-13.SDR SWAA2022022258098Skin · delaminatedL/H OUTBD AFT FLAP DELAMINATING AFT INBD CORNER / REPAIRED L/H O/B AFT FLAP AT I/B CORNER IAW B737 SRM 51-70-10-2R-0 REV 65; AND B737 SRM 51-70-10-2R-4.SDR DALA2018080704904Cover · missingRIGHT WING NR 2 FLAP TRACK LOWER COVER WAS MISSING, REPLACED THE LOWER COVER.SDR KCSA201808031210Support Beam · crackedWING T/E FLAP SUPPORT MECHANISM, 1, 2, & 3 BEAMS. NR 1 POSITION. HAD ONE FASTENER HOLE WITH A CRACK INDICATION.SDR KCSA201808031209Structure · corrodedCORROSION ON LOWER SURFACE OF RT INBD MAIN FLAP JUST AFT OF OUTBOARD HINGE ASSYSDR AALA201808176004Fitting · corrodedLEFT WING OUTBOARD FLAP, THE CENTER HINGE WAS MISSING SEALANT AND CORRODED BETWEEN LOWER STUDS AND FORWARD HINGE FITTING. REPLACED STUDS AND FITTING PER AMM 57-40-01-201.SDR FDEA2018080311869Skin · dentedRT I/B FLAP I/B LOWER SURFACE AT STA XIFH 157 FOUND DENTED. REPAIR CARRIED OUT AT RT I/B FLAP LOWER SURFACE AT STA XIFH 133.90 AND XIFH 159.300 AS PER SRM 57-50-01-2R FIG 201 REPAIR 1 AND EA 1-5750-T0341437 PART 1.SDR A6WA2018080645956Skin · dentedRIGHT INBOARD FLAP LOWER OTBD SKIN PANEL WAS DENTED. REMOVED AND REPLACED THE SKIN IAW SRM 51-42-13.SDR FXGA201807311816Skin · chafedCHAFED SKIN ON RT FLAP UPPER SKIN AT W/STA 370R. THE RIGHT HAND FLAP UPPER SKIN WAS FOUND CHAFED ON THE LEADING EDGE SECTION AT W/STA 370R. REMOVE DAMAGE IN A RACE TRACK SHAPE AND REPAIR PER A&B OHM FIGURE 13-47A. USE NAS1097AD RIVETS INSTEAD OF AN426AD RIVSDR IPXA2018081543823Skin · gougedLEFT WING, OTBD FLAP LE SKIN WAS GOUGED ON A PREVIOUS REPAIR. REPAIRED IAW SRM 57-50-00, P.231, STEP H.SDR SWAA2022021763478Flap · delaminatedRIGHT WING INBD MAIN FLAP WEDGE IS DELAMINATED. / REMOVED AND REPLACED RT INBD FLAP WEDGE PANEL PER SRM 51-40-02SDR A6WA2018073045955Skin Panel · damagedLT INBD FLAP LOWER INBD SKIN PANEL HAS MULTIPLE AREAS WITH DAMAGE. REPLACED LT INBD FLAP LOWER INBD SKIN PANEL IAW SRM 51-42-13.SDR SWAA2018082024350Fairing · crackedLT WING NR 1 (544AB) FORWARD FLAP TRACK FAIRING CRACKED ON INNER SURFACE. R&R FAIRING PER SRM.SDR DALA2018082765250Plate · missingRIGHT WING, INBD FLAP HINGE FAIRING WAS MSSING A PLATE. INSTALLED THE HINGE FAIRING PLATE IAW SECTION III, ERA 570416-14. OK FOR SERVICE.SDR IPXA2018081032594Web · crackedLEFT OTBD FLAP FAIRING LOWER FWD WEB WAS CRACKED. REMOVED, FABRICATED AND REPLACED THE FLAP FAIRING WEB IAW DWG ARC2152, AND SRM 51-31-01.SDR DALA2018072704723Ballscrew · corrodedCORROSION ON BALLSCREW NUT OF INBD FLAP OUTBD BALLSCREW AT LT WING. OUTBD BALLSCREW OF INBD T/E FLAP WAS REPLACED WITH A SERVICEABLE PART AND WAS INSTALLED WITH 2751-2538 STEP 13.SDR SWAA2022021611210Flap · delaminatedLT WING O/B AFT FLAP I/B LWR END T/E IS DISBANDED. / LT WING O/B AFT FLAP WAS REPLACED AND NEW UNIT WAS INSTALLED ON A/C ON CARD # T822335SDR SWAA2022021611240Flap · delaminatedRT WING O/B AFT FLAP I/B END AT T/E IS DISBANDED. / RIGHT WING O/B AFT FLAP I/B END DELAMINATION WAS REPAIRED ON ATS WORK ORDER 508604. FLAP WAS REMOVED AND REINSTALLED ON AIRCRAFT ON CARD # T822371SDR DALA2018072704721Bushing · corrodedCORROSION ON INBD BUSHING/GIMBAL ON INBD FLAP OUTBD BALLSCREW AT LT WING. INBD BUSHING/GIMBAL ON INBD FLAP OUTBD BALLSCREW AT LT WING WAS REPLACED AND APLICABILITY WAS VERIFIED WITH IPC 27-51-11-01 ITEM 25.SDR DALA2018072704722Ballscrew · corrodedDURING INSPECT RT IB BALLSCREW FROM INBD FLAP, CORROSION WAS FOUND ON BALL NUT ID. BALLSCREW FROM INBD FLAP RT WAS REPLACED AND INSTALLED PER AMM 27-51-11-424-020 PAR (E).
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