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 FDEA2019111542951Carriage · damagedLEFT HAND WING - OUTBOARD FLAP ASSEMBLY OUTBOARD CARRIAGE SPINNER BUSHING REMOVED (REFERENCE: SNRM # N00764) FOUND BORE CENTER SURFACE DAMAGED DAMAGED AT LEFT HAND WING - OUTBOARD FLAP ASSEMBLY OUTBOARD CARRIAGE SPINNER BORE CENTER SURFACE LOCAL BLEND CARRSDR SWIA2020010947601Vane · chafedLH INBD FLAP VANE OTBD CAP CHAFE, FLAGGED (C-CHECK) RO 01/07/2020 CHAFE ON L/H INBD FLAP VANE CAP€”OTBD SIDE FOUND TO BE OUT OF LIMITS REF. CRJ200 SRM, REMOVED OUT OF LIMITS VANE CAP REF. CRJ200 SRM, LOCATED, DRILLED FULL SIZE AND COUNTERSUNK ALL HOLES COMMOSDR SWIA2020010947600Vane · chafedLH INBD FLAP VANE MIDDLE CAP CHAFE, FLAGGED (C-CHECK) RO 01/07/2020 REMOVED AND REPLACED CHAFED LH INBD FLAP VANE MIDDLE CAP WITH NEW (P/N 601R14303-51S) WITH NEW FASTENERS, REF BOMBARDIER DWG AND CRJ200 SRM. / SKYCARD COMPLIED WITH IN ITS ENTIRITY.SDR A6WA2019112047022Structure · damagedR/H O/B FLAP T/E DAMAGED 14" O/B FROM I/B CORNER. DAMAGE WAS INDUCED DURING MAINTENANCE. AIRCRAFT REMOVED FROM SERVICE REPAIRED DAMAGE ON R/H O/B FLAP T/E AT APPROX 14" O/B FROM I/B CORNER WITH A REPAIR DOUBLER THAT MEASURES 5.6" X 3.1" REF CRJ 200 SRM 57-53SDR HALA2019111400483Vane · dentedFOUND A DENT L-1/2 " W 1/4 " D 0.006 " WITH A CRACK 9/32 " LONG AT THE CENTER OF THE DENT DAMAGE LOCATED ON L/H AFT MOVEABLE VANE 15 1/2 " FROM INBOARD EDGE 12 3/16 " FROM TRAILING EDGE UNDER SIDE OF VANE. // PERFORMED COIN TAP TEST AROUND THE AFFECTED AREA NOSDR SWIA2019122747411Panel · chafedLEFT INBD FLAP PANEL 584JB IS CHAFFED AT ACTUATOR NOTCH . REPAIRED THE LT INBD FLAP PANEL.SDR SWIA2019122747409Panel · chafedLEFT INBD FLAP PANEL 584MB IS CHAFED AT THE ACTUATOR NOTCH. REPAIRED LT INBD FLAP PANEL IAW EA934, CURED AND FINISHED.SDR FDEA2019111522935Nut Plate · damagedLT I/B FLAP INBOARD HOIST FITTING HAS 2 EACH NUT PLATES STRIPPED OUT. REMOVED AND REPLACED 2 EA NUT PLATES ON LT I/B FLAP I/B HOIST FITTING IAW DWG ARC2369 AND SRM 51-31-01 VOL II. SKIN SPLICE REPAIR IAW SRM 57-10-00 FIG 86 VOL I. RSC TRACKING ON EA T8-5750SDR IPXA2019112769431Doubler · damagedINSPECTION TYPE:2CR/H WING I/B FLAP HAS DAMAGED REPAIR DOUBLER AT STA. XIFH=165.3 AND AFT OF YIFH=34.5.REPAIRED DAMAGED R/H I/B FLAP UPPER SKIN AT STA. XIFH=165.3 AND AFT OF YIFH=34.5 IAW VT-SAA EA 011-5753-01-A7954 REV. I/R AND UPS EO MD11-5750-74734-A. (MAJOSDR IPXA2019112219239Skin · damagedINSPECTION TYPE:2CR/H I/B FLAP T/E WEDGE UPPER SKIN HAS REPAIR AT STA. XIFH=171.3 AND 6.5 INCHES FROM EDGE NOT ON REPAIR MAPREPAIRED R/H I/B FLAP T/E WEDGE UPPER SKIN AT STA. XIFH-=171.3 AND 6.5 INCHES FROM EDGE IAW SRM 57-00-01 REPAIR 1 FIG. 201. (MAJOR)SDR AALA201911139020Flap Track · wornAIRCRAFT IN BASE MAINTENANCE: LEFT WING INBOARD TRAILING EDGE FLAP TRACK #1 WORN. REPLACED FLAP TRACK PER AMM 57-54-21.SDR SWIA2020010947552Bolt · corrodedL/H WING OUTBROAD #3 FLAP OUTBROAD AND INBROAD HINGE BOX ATTACHING HARDWARE CORRODED (C-CHECK) RO 01/06/2020 REMOVED AND REPLACED LH OB #3 HINGE. NEW HARDWARE INCLUDED AS ASSMBELY IAW CRJ200 AMM. / TW: STS-2550 DUE:25NOV2020SDR SWIA2020010947551Bolt · corrodedL/H WING OUTBROAD #4 FLAP OUTBROAD AND INBROAD HINGE BOX ATTACHING HARDWARE CORRODED (C-CHECK) RO 01/06/2020 REMOVED AND REPLACED L/H O/B FLAP O/B HINGE BOX ASSEMBLY IAW CRJ 200 AMM. T.W. #STS2250 CAL DUE DATE 25NOV 20. REF.19877644SDR SWIA2019123147532Vane · chafed*RH INBD FLAP VANE CHAFFED INBD END (C-CHECK) RO 12/27/2019 REMOVED CHAFFED RH INBD FLAP VANE CAP AND INSTALLED NEW RH INBD FLAP VANE CAP REF CRJ 200 SRM AND DWG. SEE CONTINUE CARD FOR DETAILS.SDR AALA201911109014Skin · debondedAIRCRAFT WAS NOT GROUNDED: RIGHT WING OUTBOARD FLAP TRAILING EDGE DISBONDED INBOARD OF THE #3 TRACK FAIRING. **SUPPLEMENTAL REPORT: REPAIRED FLAP PER SRM 57-53-00-283-013 AND 51-77-13-911-004.** (CLOSED)SDR SWAA2022022447701Flap · delaminatedLEFT OUTBOARD AFT FLAP LOWER SURFACE HAS LARGE AREA OF DELAMINATION AT INBOARD END / REMOVED AND INSTALLED NEW LEFT WING; OUTBOARD AFT FLAP. IAW AMM 27-51-22-000-801; AMM 27-51-22-400-801. ADJUSTMENT GOOD. ATAG # WT1094 POS L/H TAB / GRB NO. 1046165 P/N OFF 11SDR FDEA201911082910Support · corrodedLEFT WING - OUTBOARD FLAP VANE NUMBER 4 SUPPORT FITTING ECCENTRIC HOLE FOUND CORRODED. CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER 4 SUPPORT FITTING ECCENTRIC HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 SDR FDEA201911082909Support · corrodedLEFT WING - OUTBOARD FLAP VANE NUMBER 3 SUPPORT FITTING ECCENTRIC HOLE FOUND CORRODED. CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER 3 SUPPORT FITTING ECCENTRIC HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 SDR FDEA201911082908Support · corrodedLEFT WING - OUTBOARD FLAP VANE NUMBER 2 SUPPORT FITTING ECCENTRIC HOLE FOUND CORRODED. CORROSION AT LEFT WING - OUTBOARD FLAP VANE NUMBER 2 SUPPORT FITTING ECCENTRIC HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5 SDR FDEA201911082911Support · corrodedRIGHT WING - OUTBOARD FLAP VANE NUMBER 1 SUPPORT FITTING ECCENTRIC HOLE FOUND CORRODED. CORROSION AT RIGHT WING - OUTBOARD FLAP VANE NUMBER 1 SUPPORT FITTING ECCENTRIC HOLE REWORKED BY MACHINING AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR SDR FDEA201911082906Rib · crackedRH WING - MID FLAP RIB21 AFT AREA FOUND CRACK ON X-RAY INSPECTION. RH WING - MID FLAP RIB21 UPPER FLANGE CRACK BETWEEN STGR2.7 AND STGR2.8 . REPAIRED THE CRACKED RIB FLANGE PER A300-600F SRM57-50-00-201 FIG.201. TRACKING EA:6-5750-T0350993 HAS BEEN ISSUED SDR A6WA2019112147027Fitting · chafedR/H WING O/B FOREFLAP / AFT FLAP FITTING WORN DUE TO SEIZED ROLLER.AT FZ 189.57. AIRCRAFT REMOVED FROM SERVICE BLENDED CHAFE DAMAGE AREA ON R/H WING O/B FLAP O/B FOREFLAP FITTING AND AFT FLAP FITTING IN AN AREA OF 4.2"L X .20"W X .005"D WITHIN LIMITS REF ASASDR DALA2019111206569Skin · scratchedFOUND OUT SCRATCH ON LH WING I/B FWD FLAP TRAILING EDGE PANEL LOWER SURFACE AT 80 INCHES TO I/B EDGE. REPAIRED AS PER SRM 57-53-01. (LP 1349225)SDR DALA2019110706468Skin · dented(LOG 1349007) DURING INSPECTION FOUND TWO DENTS ON INBD MAIN FLAP (8'' OF T/E EDGE AND 7'' OF OUTBD EDGE) AT LH WING. REPAIR WAS PERFORMED ON INBD MAIN FLAP (8' OF T/E EDGE AND 7'' OF OUTBD EDGE) AT LH WING PER B737-800 S.R.M. 57-53-01 REPAIR 7 PARAGRAPH 4. ANSDR SWAA2022040658597Skin · debondedRH WING T/E I/B MAIN FLAP LOWER SKIN DISBONDED AT O/B END OF WEDGE. / REPAIRED PER SRM 51-70-10-2R-2.SDR SWIA2019122747394Fairing · crackedLH FLAP STUB FAIRING CRACKED ON LEADING EDGE SIDE (C-CHECK) RO:12/24/2019 REPLACED LH FLAP STUB FAIRING WITH NEW FAIRING. LH FLAP STUB FAIRING IS INSTALLED ON JOB.2755581 OP.96 MX.19844954. SEE CONTINUATION FOR DETAILSSDR SWAA2019112539080Skin · delaminatedL/H WING OUTBOARD AFT FLAP UPPER SURFACE INBOARD CORNER DELAMINATED. / R&R AFT FLAP IAW SRM AND AMM.SDR FDEA201911062895Hinge · corrodedLEFT WING FLAP SIDE OUTBOARD FLAP INBOARD HINGE PIVOT INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT LEFT WING FLAP SIDE OUTBOARD FLAP INBOARD HINGE PIVOT INBOARD LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM57-52-04. OVERSIZED BUSHING FABRICSDR FDEA2019110762896Hinge · corrodedRIGHT WING FLAP SIDE OUTBOARD FLAP INBOARD HINGE PIVOT INBOARD LUG HOLE BORE FOUND CORROSION. CORROSION AT RIGHT WING FLAP SIDE OUTBOARD FLAP INBOARD HINGE PIVOT INBOARD LUG HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM57-52-04. OVERSIZED BUSHING FABRSDR SWIA2019110646716Vane · chafed*L/H I/B FLAP VANE L/E AT O/B ACTUATOR IS CHAFED. (C-CHECK) RO: 11/05/2019 REPLACED LH INBOARD FLAP VANE CAP AT OB ACTUATOR IAW SRM.SDR SWIA2019110646715Vane · chafedL/H I/B FLAP VANE L/E AT CENTER ACTUATOR IS CHAFED. (C-CHECK) RO: 11/05/2019 REPLACED LH INBD FLAP VANE CAP AT CENTER ACTUATOR IAW SRM.SDR AALA201911139011Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING INBOARD TRAILING EDGE FLAP UPPER SKIN AT MFS 91.2. REPLACED FLAP PER TASK CARD 27-94-12.SDR FDEA2019110752854Doubler · gougedR/H OUTBOARD MAIN FLAP L/E DOUBLER IS GOUGED. COMPLIED WITH EA F-5750-T0350465 P1, AND SRM 57-53-01-2R, REP 2, FIG 201.SDR SWAA2019110738669Plate · crackedRH WING TRAILING EDGE FLAP WELL LOWER SIDE WIGGLE PLATE IS CRACKED AT RSS 270. / REPLACED WIGGLE PLATE ASSEMBLY AT TRAILING EDGE FLAP RSS 270 IAW SRM 51-40-02-0G-0 + 51-40-05-0G-0.SDR DALA2019110766470Structure · corroded(LOG 1346947) DURING INSPECTION FOUND CORROSION ON INBD LOWER AREA AT INBD AFT FLAP RH WING, NEAR TO BODY FAIRING. CORROSION LEVEL 2 REPAIR WAS ACCOMPLISHED PER ERA 582646-14 REV. A AND ETI-37-19-344 REV. ORIG.SDR SWIA2019110546705Flap · out of toleranceRH O/B FLAP POP MARKS OUT OF TOLERANCE. (C-CHECK) RO: 11/04/2019 WORK PERFORMED BY VENDOR AVMAX,SDR SWIA2019110546671Spar · damagedDAMAGED SPAR, LH IB FLAP BETWEEN WS 58.505 TO WS 61.506. (C-CHECK) RO: 11/04/2019 REPLACED DAMAGED SPAR/INTERCOSTAL. COMPLIED WITH M-337.SDR SWIA2019110546670Rib · damagedDAMAGED RIB LH IB FLAP AT WS 91.338. (C-CHECK) RO: 11/04/2019 REPLACED DAMAGED RIB INSIDE LH I/B FLAP. COMPLIED WITH M-337.SDR SWIA2019110546665Skin · damagedLIGHT SURFACE DAMAGE TO THE LOWER SKIN OF THE IB FLAP, DIRECTLY AFT OF THE LH MLG WHEELS. (C-CHECK) RO: 11/04/2019 WORK PERFORMED BY VENDOR AVMAX.SDR SWIA2019110546664Rib · damagedDAMAGED RIB, LH IB FLAP AT WS 54.848. (C-CHECK) RO: 11/04/2019 WORK PERFORMED BY VENDOR AVMAX.SDR SWIA2019110546663Skin · damagedMINOR SURFACE DAMAGE ON THE BOTTOM SKIN OF THE R/H I/B FLAP, JUST AFT OF THE R/M MLG TIRES. (C-CHECK) RO: 11/04/2019 WORK PERFORMED BY VENDOR AVMAX IAW SRM.SDR SWIA2020010947557Vane · damagedLEFT INBOARD FLAP VANE HAS DAMAGE ON LEADING EDGE (C-CHECK) RO 01/06/2020 REMOVED AND REPLACED LH IB FLAP ASSY IAW CRJ200 AMM / FLAPS RIGGED IAW CRJ200 AMM / OPS CHECK GOOD AT THIS TIME / TW:STS-0252 DUE: 27DEC2019SDR SWIA2020010947556Skin · damagedRIGHT INBOARD FLAP VANE HAS DAMAGE ON LEADING EDGE (C-CHECK) RO 01/06/2020 REMOVED AND REPLACED RH IB FLAP ASSY IAW CRJ200 AMM FLAPS RIGGED IAW CRJ200 AMM OPS CHECK GOOD AT THIS TIME / TW:STS-0252 DUE: 27DEC2019SDR A6WA2019112047024Hinge Fitting · chafedR/H WING O/B FLAP HINGE BOX AT WS 264.00 HAS 2 AREAS OF CHAFING DAMAGE. DAMAGE AREA 1 IS TO THE I/B FLAP HINE ARM FITTING DWG 601R10910 WITH DAMAGE DIMENSIONS OF .20"L X .15"W X .032"D. DAMAGE 2 IS TO THE AFT SIDE PLATE DWG 601R10180 WITH DAMAGE DIMENSIONS OF SDR DALA2019110506409Skin · dented(AIRCRAFT 5640, L/P 1345844) DENT ON INBD MAIN FLAP LWR SKIN MF STA 209 AT RH WING. (AD). CORRECTIVE ACTION: INBD MAIN FLAP LWR SKIN MF STA 209 AT RH WING WAS REPAIRED PER B757-200 SRM 57-53-01 REPAIR 1 DETAIL I AND SRM 51-70-10 REPAIR 2 PAR. 4.SDR SWIA2019110446655Skin · dentedRH INBOARD FLAP LOWER SKIN HAS A DENT AT INBOARD AFT BAY. (C-CHECK) RO: 11/3/2019 R/H INBOARD FLAP LOWER SKIN AT INBOARD AFT BAY OUT OF LIMITS. FLUSH REPAIR ACCOPLISHED.SDR SWIA2019110446650Fairing · chafedRH FLAP STUB FAIRING IS CHAFED. (C-CHECK) RO: 11/3/2019 REMOVED THE RH FLAP STUB FAIRING AND FOUND OUT OF LIMITS. RECEIVED NEW FLAP STUB FAIRING, LOCATED AND DRILLED NEW PART. INSTALLED A NEW RH FLAP STUB FAIRING IAW AMM.SDR SWIA2019110446649Fairing · chafedLH FLAP STUB FAIRING IS CHAFED. (C-CHECK) RO: 11/3/2019 REMOVED THE LH FLAP STUB FAIRING AND FOUND OUT OF LIMITS. RECEIVED NEW FLAP STUB FAIRING, LOCATED AND DRILLED NEW PART. INSTALLED A NEW LH FLAP STUB FAIRING REF IAW AMM.SDR SWIA2019110446648Guide Plate · chafedFLAP HINGE FAIRING 592BB GUIDE PLATE CHAFED. (C-CHECK) RO: 11/3/2019 ORIGINAL GUIDE PLATE THICKNESS .045, CHAFE DAMAGE .017, REMAINING THICKNESS .028 FOUND TO BE OUT OF LIMITS IAW SRM.SDR SWIA2019110446636Skin · chafed* LEFT INBD FLAP VANE INBD LEADING EDGE IS CHAFFED. (C-CHECK) RO: 11/1/2019 LH INBD FLAP VANE INBD LEADING EDGE IS FOUND TO BE OUT OF LIMITS AND REPLACED WITH NEW.
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