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 IPXA2019053042647Skin · dentedINSPECTION TYPE:12YR L/W I/B FLAP LOWER SURFACE BETWEEN RIBS 15, 17 STR 1.2-2.9 MULTIPLE DENTS. REPAIRED PER SRM 57-50-00 AND EO A300-5750-72562.SDR FDEA201904290962Support Fitting · corrodedLEFT WING - OUTBOARD FLAP VANE NUMBER.5 SUPPORT FITTING ECCENTRIC HOLE FOUND CORROSION. CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER. 5 SUPPORT FITTING ECCENTRIC HOLE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R REPAIR 5 FIGURE 201.OVERSIZED ECSDR FDEA201904290961Support Fitting · corrodedLEFT WING - OUTBOARD FLAP VANE NUMBER.4 SUPPORT FITTING ECCENTRIC HOLE FOUND CORROSION. CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER. 4 SUPPORT FITTING ECCENTRIC HOLE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R REPAIR 5 FIGURE 201.OVERSIZED ECSDR FDEA201904290960Support Fitting · corrodedLEFT WING - OUTBOARD FLAP VANE NUMBER.2 SUPPORT FITTING ECCENTRIC HOLE FOUND CORROSION. CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER. 2 SUPPORT FITTING ECCENTRIC HOLE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R REPAIR 5 FIGURE 201. OVERSIZED ESDR FDEA201904290959Support Fitting · corrodedRIGHT WING - OUTBOARD FLAP VANE NUMBER.4 SUPPORT FITTING ECCENTRIC HOLE FOUND CORROSION. CORROSION AT RIGHT WING - OUTBOARD FLAP VANE NUMBER. 4 SUPPORT FITTING ECCENTRIC HOLE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R REPAIR 5 FIGURE 201. OVERSIZEDSDR FDEA201904290958Support Fitting · corrodedRIGHT WING - OUTBOARD FLAP VANE NUMBER. 2 SUPPORT FITTING ECCENTRIC HOLE FOUND CORROSION. CORROSION AT RIGHT WING - OUTBOARD FLAP VANE NUMBER. 2 SUPPORT FITTING ECCENTRIC HOLE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R REPAIR 5 FIGURE 201. OVERSIZESDR FDEA201904290957Hinge · corrodedRIGHT WING - FLAP SIDE OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - FLAP SIDE OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04. OVERSIZED BUSHING FASDR IPXA2019051442123Flap · dentedINSPECTION TYPE:12YR RT WING T/E I/B FLAP LOWER T/E IS DENTED OUT OF LIMITS. REPAIRED PER SRM 57-50-00.SDR FDEA201904290956Hinge · corrodedLEFT WING - FLAP SIDE OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - FLAP SIDE OUTBOARD FLAP INBOARD HINGE INBOARD PIVOT LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-04. OVERSIZED BUSHING FASDR LR7A2019042901506Stiffener · crackedDURING SCHEDULED C-13 CHECK UNDER JOB CARD HC5711, FOUND THE CENTER WING AFT SPAR FLAP TRACK VERTICAL STIFFENER AT CWS192L CRACKED AT THE LOWER FITTING RADIUS, FS597, WL256. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SRM, CH. 51-60 & 51-70. NR# 2060.SDR LR7A2019043091494Skin · crackedDURING SCHEDULED B-2 CHECK UNDER JOB CARD HB2703, FOUND THE RH OUTBOARD FLAP UPPER TRAILING EDGE SKIN CRACKED AT OWFS266R, 6.8" FWD OF THE TRAILING EDGE. / REPAIRED IAW LOCKHEED SMP583 SRM, FIG. 51-140-12. NR# 1918873.SDR LR7A2019043091493Skin · crackedDURING SCHEDULED B-2 CHECK UNDER JOB CARD HB2703, FOUND THE LH INBOARD FLAP LOWER SKIN CRACKED AT CWS131L, 6" FORWARD OF THE TRAILING EDGE. / REPAIRED IAW LOCKHEED SMP583 SRM, FIG. 51-140-12. NR# 1916825.SDR FDEA201904280945Doubler · wornEXISTING REPAIR ON RH I/B FLAP UPPER SKIN BETWEEN RIB1C AND RIB3 STGR2.1 AND STGR2.2 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON RH I/B FLAP UPPER SKIN BETWEEN RIB1C AND RIB3 STGR2.1 AND STGR2.2 WAS EVALUATED AND FOUND IN CONFORMITY WITH TD FOK/1SDR FDEA201904270938Hinge Bracket · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE (G AND F HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. OVERSSDR FDEA201904270937Hinge Bracket · corrodedRIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE FOUND CORROSION CORROSION AT RIGHT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE (A AND B HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. OVESDR FDEA201904270936Hinge Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE FOUND CORROSION CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT LUG HOLE BORE (A AND B HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. OVERSSDR FDEA201904270935Hinge Bracket · corrodedLEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING - FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT LUG HOLE BORE (G AND F HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57- 52-03. OVERSDR K11A2019061991705Structure · corrodedR/W T/E FLAP, L/E TOP STA XFLS 127 TO XFLS 187SDR REXA2019042600678Vane · chafedRIGHT INBOARD FLAP VANE IS CHAFFED IN 3 LOCATIONS ON LEADING EDGE. REMOVED 3 DAMAGED SECTIONS OF THE RIGHT INBOARD FLAP VALVE LEADING EDGE ALL INSTALLED 3 NEW SECTIONS. IAW SRM 51-42-10 AND SRM 57-52-00.SDR WVER20190624919Skin · dentedL/H INBD FLAP-LOWER SKIN IS DENTED AT FLS 34.5SDR IPXA2019051141995Vane · damagedINSPECTION TYPE:4C RT I/B FLAP VANE IS DAMAGED. REPAIRED DAMAGED R/H I/B FLAP VANE IAW 011-5753-01-A7757 REV. I/R AND EO MD11-5750-72551-A. (MINOR)SDR IPXA2019042654430Skin · dentedINSPECTION TYPE:C1C3DENT ON L/H WING INBD AFT FLAP LOWER SKIN (P/N: 65B02078-505) NEAR WBL 215.REPAIR I.A.W. 747-400SF SRM 57-53-01-2R-1, 51-70-10-2R-2, 51-70-10-2R GENERAL REV.44.00SDR IPXA2019042654429Skin · dentedINSPECTION TYPE:C1C3DENT ON R/H WING INBD AFT FLAP LOWER SKIN (P/N: 65B02078-506) NEAR WBL 181.REPAIR I.A.W. 747-400SF SRM 57-53-01-2R-1, 51-70-10-2R-2, 51-70-10-2R GENERAL REV.44.00SDR 2019FA0000274Flap Track · wornFLAP TRACKS WORNSDR 2019FA0000273Flap Track · wornFLAP TRACKS WORNSDR 2019FA0000270Support Bracket · chafedFLAP LEADING EDGE CHAFING AND SUPPORT BRACKET WEARSDR DALA2019042402599Skin · corrodedCORROSION LEVEL: 2. CORROSION INTERNAL AREA RIB21 TO RIB22 TRAILING EDGE ON RH WING (1E/A). EVALUATED REWORK INTERNAL AREA RIB 21 TO RIB 22 TRAILING EDGE ON RH WING AND FOUND WITHIN LIMITS AS PER A319 SRM 57-21-11- 283-013 STEP 2 ITEM A, FIGURE 1, SHEET 1, THRSDR DALA2020022001270Skin · punctured(AIRCRAFT 6819, L/P 5694578) LEFT TRAILING FLAP INBOARD DAMAGED 1 PUNCTURE. CORRECTIVE ACTION: PERMANENT REPAIR WAS PERFORMED PER B757-200 SRM 51-70-05-06 PAR.5 ON REFERENCE OF B757-200 SRM 57-53-01-2R-1. DETAIL II TABLE II.SDR FDEA201904220879Fitting · corrodedLEFT HAND WING OUTBOARD FLAP VANE HORN FITTING "E" ECCENTRIC HOLE BORE CORROSION. CORROSION AT LEFT HAND WING OUTBOARD FLAP VANE HORN FITTING "E" ECCENTRIC HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201(SHEETSDR FDEA201904220878Fitting · corrodedLEFT HAND WING OUTBOARD FLAP VANE HORN FITTING "B" ECCENTRIC HOLE BORE CORROSION. CORROSION AT LEFT HAND WING OUTBOARD FLAP VANE HORN FITTING "B" ECCENTRIC HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 FIGURE 201(SHEET 1SDR UIEA2019042603985Skin · corrodedLHW O/B MID FLAP I/B UPPER WING PNL SUPPORT UPR CHORD AWAY FROM I/B EDGE 5" AND 13" FOUND CORROSION(<P>LHW O/B MID FLAP I/B UPPER WING UPR CHORD CORROSION REMOVED IAW SRM 51-10-02 AND RE-PROTECTED IAW SRM 51-20-01 AND CHECKED WITHIN SRM 57-30-02 ALLOWABLE LIMISDR UIEA2019042603987Skin · corrodedLHW I/B MID FLAP O/B L/E FAIRING BULGED AT I/B AFT CORNER AREAS(<P>LHW I/B T/E MID FLAP SPAR N0.1 UPPER CHORD CORROSION AREAS REPAIRED IAW RL-57-53-13492 REV.A<BR /></P>)SDR UIEA2019042604024Spar Web · corrodedLHW I/B MID FLAP T/E PNL # 577JT AFT REAR SPAR WEB FOUND CORROSION CRACK AND DE-LAMINATED.(<P>LHW I/B MID FLAP T/E PNL # 577 JT AFT REAR SPAR NO.3 WEB REPLACED AND INSTALLED IAW RL-57-50-13520 REV.A.<BR /></P>)SDR UIEA2019042604047Skin · corrodedLHW O/B MID FLAP I/B UPPER SURFACE AWAY FROM I/B EDGE 74" FOUND BULGED.(<P>LHW O/B MID FLAP I/B UPPER SURFACE FROM I/B EDGE 74" BULGED AREAS CORROSION REMOVED IAW SRM 51-10-02 AND RE-PROTECTED IAW SRM 51-20-01 AND CHECKED WITHIN SRM 57-30-02 ALLOWABLE LIMITS. SDR CALA2019042200636Seal · missingPDA 3 RIGHT WING NR 6 T/E FLAP CANOE OUTBD SIDE CENTER SEAL COMPLETELY MISSING. INSTALLED NEW SEAL REF SRM 51-40-02.SDR CALA2019042200638Seal · missingPDA 3 RT WING UPPER FLAP SEAL MISSING. REF GAP1.SDR IPXA2019042241297Skin · dentedLEFT I/B MAIN FLAP LWR SKIN DENT AND DISBOND REPAIR. LINKED TO D-663694REPAIRED IAW E.O. B757-5750-71256-DSDR DALA201904222542Cover · detachedPDA PART DEPARTED AIRCRAFT; A/C 3265 LOG 4556722. #7 HINGE PIN FLAP TRACK MOVABLE FAIRING PIVOT COVER MISSING, REPLACED #7 RT WING FLAP FAIRING HINGE PIN COVERSDR DALA2019042292552Hinge Fitting · corrodedTHE I/B LUG FACE OF RH FLAP O/B IDLER HINGE IS CORRODED. MAINTENANCE REMOVED ALL OF THE CORROSION AND FABRICATED AN OVERSIZED BUSHING AND WASHER TO FILL THE VOID CAUSED BY THE REMOVED CORROSION. COMPLIED WITH FINAL ER/A 577251-14 REV. 0. (LP #1037065)SDR DALA2019042202539Cover · missingPDA PART DEPARTED AIRCRAFT. A/C 3101 CLOSED LOG 4002230. FLT/CHK 1496. 1 FLAP TRACK MOVEABLE FAIRING PIVOT COVER MISSING. INSTALLED REPLACEMENT COVER PER A319 AMM 27-50-00.SDR DALA201904212536Skin · damagedDURING M CHECK INSPECTION, 3EA DEBONDED DAMAGES WERE FOUND ON TRAILING EDGE OF THE RH FLAP ASSY-O/B BETWEEN RIB 18-19. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLER PER SRM 51-77-13-911-004 AND ER/A 577044-14. LP 1038111.SDR DALA2019041802519Skin · debondedLEFT WING O/B FLAP L/E FOUND DISBONDING AS MARK. REPAIRED PER SRM 57-53-01.SDR SWAA2022022445693Flap · delaminatedRT WING O/B AFT FLAP LOWER SURFACE I/B LOWER CORNER HAS DELAMINATION / REPAIRED RT WING O/B AFT FLAP LOWER SURFACE I/B LOWER CORNER I.A.W 737 SRM 57-53-01-2R-4 & I.A.W 737 SRM 51-70-10-2R-4; DAMAGE WAS PAST ALLOWABLE LIMITS I.A.W 737 SRM 57-53-01-1A-4 PARA 4A(SDR FDEA201904170827Hinge Bracket · corrodedLEFT HAND WING - INBOARD FLAP OUTBOARD AFT HINGE ( FLAP SIDE) PIVOT INBOARD HOLE BORE CORROSION CORROSION AT LEFT HAND WING INBOARD FLAP OUTBOARD AFT HINGE ( FLAP SIDE) PIVOT INBOARD HOLE BORE (G AND F HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03.SDR FDEA201904170826Hinge Bracket · corrodedLEFT HAND WING - INBOARD FLAP OUTBOARD AFT HINGE ( FLAP SIDE) PIVOT OUTBOARD HOLE BORE CORROSION CORROSION AT LEFT HAND WING INBOARD FLAP OUTBOARD AFT HINGE ( FLAP SIDE) PIVOT OUTBOARD HOLE BORE (A AND B HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-0SDR FDEA201904170825Hinge Bracket · corrodedRIGHT HAND WING - INBOARD FLAP OUTBOARD AFT HINGE ( FLAP SIDE) PIVOT OUTBOARD HOLE BORE CORROSION CORROSION AT RIGHT HAND WING INBOARD FLAP OUTBOARD AFT HINGE ( FLAP SIDE) PIVOT OUTBOARD HOLE BORE (A AND B HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52SDR SWAA2022030760886Wedge · debondedINBOARD AFT CORNER OF OUTBOARD AFT TRAILING EDGE FLAP DISBONDED. AREA MEASURES 1/2' WIDE FROM TRAILING EDGE AND 2 3/4' LONG FROM INBOARD EDGE / REPAIRED FLAP TE WEDGE PER SRM 51-70-10-2R-1 (PERMANENT) CL #56256SDR SWAA2022022460887Flap · debondedRIGHT WING I/B AFT CORNER OF OUTBOARD FLAP IS DISBONDED .AREA MEASURES 1.343 ' LONG FROM I/B EDGE AND .718' WIDE FROM TRAILING EDGE. / RH OUTBD AFT FLAP WAS R&R'D ON ACTION LOG PG 0126212SDR SWAA2022022446334Flap · delaminatedLH WING O/B AFT FLAP HAS DELAM ON INBOARD END AT TRAILING EDGE / EVALUATED; PREPPED; CLEANED AND REPAIRED DELAM DAMAGE ON L/H WING O/B AFT FLAP AT I/B - T/E IAW B737 SRM 57-53-01-2R-14 + SRM 51-70-10-2R-0; REV 66.SDR SWAA2019042231845Skin · debondedLH WING I/B AFT CORNER OF OUTBOARD FLAP IS DISBONDED. PERFORMED TEMP. REPAIR TO L/H INBOARD AFT CORNER PER SRM 57-53-01 1A-4. MAKE A DETAILED INSPECTION OF THE DAMAGED AND SPEED TAPE AT A DAILY INTERVAL. ALSO PERFORM A DAILY DETAILED ON THE SURROUNDING FASTNER
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