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 EVGR20181119001Flap Track · brokenTHE LEFT INBOARD FLAP TRACK WAS FOUND TO BE CRACKED (BROKEN) AT THE AFT END DURING THE POST FLIGHT INSPECTION. THIS WAS THE FIRST FLIGHT AFTER A 50 HOUR INSPECTION AND ROUTINE SERVICING. THE CRACK WAS NOT EVIDENT DURING THE PREFLIGHT INSPECTION. THE PILOTS (SDR AALA201811109010Strut · corrodedTHE AIRCRAFT IS IN BASE MAINTENANCE. CORROSION FOUND ON LEFT HAND WING TRAILING EDGE FLAP INTERCONNECTING STRUT, INBOARD FLAP. REPLACED LEFT HAND WING TRAILING EDGE FLAP INTERCONNECTING STRUT PER AMM 27-51-400-001-A AND PERFORMED ADJUSTMENT AND OPERATIONAL TESSDR AALA2018111209009Strut · corrodedCORROSION FOUND ON THE RIGHT WING TRAILING EDGE INTERCONNECTING STRUT, INBOARD FLAP. REPLACED THE STRUT IAW AMM 27-51-44-400-001-A, AND PERFORMED OPERATIONAL TEST OF THE FLAPS SYSTEM.SDR FDEA201811073128Skin · delaminatedLT OTBD FLAP UPPER SKIN INBD END SHOWS EVIDENCE OF POSSIBLE DELAMINATION. REPAIRED LT OTBD FLAP UPPER SKIN INBD END DELAMINATION IAW SRM 51-70-17-OG PARA 3G AND EA T F-5750-T0343415 P1 FLAP SKIN REPAIR.SDR FDEA201811073125Hinge Bracket · corrodedRIGHT HAND WING INBOARD FLAP OUTBOARD AFT (FLAP SIDE) HINGE PIVOT INBOARD HOLE BORE CORROSION. HOLE BORE (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. BUSHING FABRICATED AND INSTALLED AS PER CMM 57-52-03 AND EA 1-5750-130949C PART5 STEP 2SDR FDEA201811073124Hinge Bracket · corrodedRIGHT HAND WING INBOARD FLAP OUTBOARD AFT (FLAP SIDE) HINGE PIVOT OUTBOARD HOLE BORE CORROSION. HOLE BORE (HOLE B AND A) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-52-03 AND EA 1-5750-130949CSDR FDEA201811073123Hinge Bracket · corrodedLEFT HAND WING INBOARD FLAP OUTBOARD AFT (FLAP SIDE) HINGE PIVOT OUTBOARD HOLE BORE CORROSION. HOLE BORE (HOLE B AND A) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-52-03 AND EA 1-5750-130946C PASDR FDEA201811073122Hinge Bracket · corrodedLEFT HAND WING INBOARD FLAP OUTBOARD AFT (FLAP SIDE) HINGE PIVOT INBOARD HOLE BORE CORROSION. HOLE BORE (HOLE G AND F) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-52-03. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-52-03 AND EA 1-5750-130946C PARSDR DALA2018111200329Cover · missingRIGHT WING NR 2 FLAP FAIRING AFT HINGE COVER MISSING. COVERED AREA WITH SPEED TAPE PER CDL 57-00-07.SDR A6WA2018110946140Plate · crackedFLAP PANEL 684AB HAS 2 CRACKED ATTACH PLATES. REPLACED ATTACH PLATED IAW CRJ200 SRM 51-42-06.SDR DALA2018110706497Fastener · missingLEFT WING TRAILING FLAP & VANE BRACKET HARDWARE MISSING (3RD BRACKET FROM INBD). INSTALLED NEW HARDWARE IAW AMM 27-51-00. SDR REPORTED DUE TO POSSIBILITY THAT THE MISSING HARDWARE MAY HAVE DEPARTED THE AIRCRAFT DURING FLIGHT. (LP4755522)SDR Q2SA20181105404Flap · gougedAIRCRAFT GROUNDED. FLAP 2 BY STATION 235 HAS DEEP GOUGE BY MOUNT BRACKET LT INBD FORE FLAP. SEE EA180602 IR FOR REPAIR PROCESS AND SHOP FOR ANY ADDITIONAL WORK STEPS COMPLETED.SDR Q2SA2019022700011Structure · gougedFLAP 2 BY STATION 235 HAS DEEP GOUGE BY MOUNT BRACKET L/H INBD FORE FLAP.SDR FOTR20181105009Flap · corrodedLT O/B MAIN FLAP HAS INTERNAL CORROSION ON FWD LOWER FLANGE AND AROUND FASTENER HOLES APPX WBL493.SDR SWAA2022022578524None · delaminatedSUPPLEMENTAL INFORMATION: R/H WING; I/B MAIN FLAP O/B LOWER SKIN IS SEPARATED; 23.5' W X 10.0' D / REMOVED AND REPLACED R/H I/B T/E FLAP WEDGE MPN 113A2500-14 ATAG WN5499 IAW BOEING DWG 113A2100 REV B737-700 SRM 51-40-02SDR IPXA2018110235612Skin · damagedFLAP SKIN FOUND GOUGES & CHAFES, PREVIOUSLY BLEND LOCATION. REPAIRED IAW SRM 51-70-10 IAW EO B757-5750-70453-ASDR V0XD20181107001Skin · dentedLH I/B FLAP BOTTOM SURFACE HAS A DENT AT W.S. 38.00 CORRECTIVE ACTION: REPAIRED L/H I/B FLAP BOTTOM SURFACE AT W.S. 38.00 IAW CRJ 700 SRM 57-52-01 REPAIR IV, 51-25-06, 51-21-11, 51-25-16, AND CRJ700 NDTM PART 1 51-20-006.SDR SWAA2018110226436Repair · damagedLT WING OUTBOARD AFT FLAP INBOARD EDGE DAMAGED TO PREVIOUS REPAIR. R&R AFT FLAP PER AMM.SDR FDEA201810313068Rib · crackedRT WING CENTER FLAP RIB 26 HAS TWO CRACKS AT TOP SKIN ATTACHMENT, 6TH FASTENER AND 12TH FASTENER FWD OF REAR SPAR. REPAIRED 2 CRACKS BETWEEN STR 2.7 AND 2.8 IAW SRM 57-50-00, FIG 201, SEE RSC TRACKING EA 6-5750-T0343180 PT1, WRI 57502376. REPAIR IS CLASSIFIED SDR FDEA201810313066Skin · corrodedBULGING SKIN AT LT INBD FLAP LOWER SURFACE MID AREA 22" INBD OF FLAP HINGE ARM. CORROSION FOUND TO BE BEYOND LIMITS AT BULGING SKIN AT LT INBD FLAP LOWER SURFACE MID AREA 22" INBD OF FLAP HINGE ARM IAW SRM 57-00-01 FIG 1A. REMOVED AND REPLACED LOWER SKIN AND SDR 39LA20181030178Channel · corrodedDURING REPAIR ACTIONS TO THE RT INBD FLAP PIVOT CONTROL POINT, THE CHANNEL ATTACHED TO THE SUPPORT BOX WAS FOUND TO BE CORRODED. REF SRM FIG 2-24 POS 3 DWG 212-11157 NHA LINK BRACKET I AND II. ASSEMBLY OF A TECHNICAL DATA PACKAGE IS CURRRENTLY IN WORK. ONCE TSDR 39LA20181030177Fitting · wornDURING INSPECTION, DANAGE WAS NOTED TO THE RT INBD FLAP PIVOT CONTROL POINT. THE LT AND RT FITTING PLATES WERE FOUND WORN BEYOND LIMITS AT THE BOLT HOLES. REF SRM FIG 2-24 POS 7 DWG 212-11157 NHA LINK BRACKET I AND II. ASSEMBLY OF A TECHNICAL DATA PACKAGE IS SDR SWAA2018110526447Flap · delaminatedLT WING OUTBOARD AFT FLAP DELAMINATED ON LOWER INBOARD CORNER. REPAIRED AFT FLAP PER EA.SDR SWAA2018103126371Flap · delaminatedLT WING OUTBOARD AFT FLAP DELAMINATED AT INBOARD TRAILING EDGE. REPAIRED AFT FLAP PER SRM.SDR IPXA2018102985426Skin · dentedRIGHT OTBD AFT FLAP LOWER SURFACE WAS DENTED. REPAIRED IAW EO B747-5750-69080-B.SDR ASOA201810255289Skin · gougedRT INBOARD FLAP UPPER SKIN GOUGED. REPAIRED PER REO 601R87-52-2266 REV- DATED 2018-10-23.SDR FDEA2018102653011Flap · gougedAIRCRAFT DAMAGE-RT I/B FLAP HAS A PUNCTURE ON LOWER SURFACE AFT OF AFT TRUNNION FAIRING. REPAIRED RT I/B FLAP PUNCTURE ON LOWER SURFACE AFT OF AFT TRUNNION FAIRING IAW SRM 51-70-17-OG PARA 3G & FIG 5 AND EA WORK CARD T F-5750-T0343144 P1. WING-FLIGHT SURFACES-SDR COEA2018112348801Hinge · corrodedWO 188750 NR 500042 HEAVY CHECK COE/MINOR REPAIR: LH WING LOWER TRAILING EDGE DROP DOWN PANEL 531AB MIDDLE HINGE SUPPORT ATTACH PLATE HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED HINGE WITH OEM PART.SDR COEA2018112347801Hinge · corrodedWO 188750 NR 500041 HEAVY CHECK COE/MINOR REPAIR: LH WING LOWER TRAILING EDGE DROP DOWN PANEL 531AB INBOARD HINGE SUPPORT ATTACH PLATE HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED HINGE WITH OEM PART.SDR DALA2018102506268Doubler · wornWEAR ON UPPER DOUBLER OF RT WING OUTBOARD FLAP INBOARD VANE. RT WING OUTBD FLAP INBD VANE WAS REPAIRED PER SRM 57-03D. PAR 11.SDR R61A2018111641143Bushing · corrodedDURING HEAVY CHECK MAINTENANCE FOUND LH WING #2 FLAP CARRIAGE SUPPORT FWD HARDWARE HAS RUST. REMOVED AND REPLACED CARRIAGE SUPPORT HARDWARE IAW EMB AMM 27-51-08.SDR AALA201811059017Skin · debondedAIRCRAFT IN BASE MAINTENANCE: RIGHT WING OUTBOARD TRAILING EDGE FLAP SKIN DEBONDED BETWEEN RIB 14 AND RIB 16. REPAIRED FLAP PER SRM 57-53-00-300-017.SDR FDEA201810232977Bolt · looseRT WING, NR 7 & NR 8 FLAP TRACKS LOOSE AT AFT ATTACH POINTS. REPLACED NR 7 & NR 8 FLAP TRACK, AFT ATTACH BOLTS IAW AMM 27-51-15SDR FDEA201810232976Bolt · looseLT WING, NR 1 & NR 2 FLAP TRACKS LOOSE AT AFT ATTACH POINTS. REPLACED NR 1 & NR 2 FLAP TRACK, AFT ATTACH BOLTS IAW AMM 27-51-15.SDR DALA2018102200313Cover · missingLEFT WING NR 2 FIXED FLAP TRACK FAIRING MISSING ACCESS COVER ON THE OUTBOARD SIDE. DEFERRED PER CDL 57-00-07. REPLACED ACCESS COVER.SDR FDEA201810222968Web · damagedLT INBD FLAP SKIN PANEL DAMAGED. REPLACED -3 WEB ASSY WITH A -23 WEB ASSY IAW PRODUCTION DWG ARC2305. COMPLIED WITH EA1-5730-T0343042.SDR SWAA2018110526490Flap · corrodedLT WING INBOARD AFT FLAP CORRODED ALONG THE TRAILING EDGE. R&R AFT FLAP IAW AMM.SDR AALA201901029040Skin · corrodedCORROSION ON THE LEFT WING OUTBOARD TRAILING EDGE FLAP LOWER SKIN. REPLACED LT WING TE FLAP IAW AMM 27-50-00.SDR SWIA2018110245220Skin · dentedA DENT WAS FOUND ON THE RT INBD FLAP LOWER SKIN. REPAIRED THE SKIN IAW SRM 57-52-00.SDR IPXA2018110235578Skin · dentedDENT FOUND ON THE LT WING INBD AFT FLAP LOWER SKIN, NEAR WBL 296. REPAIRED IAW SRM 57-53-01-2R-1, REPAIR 1, SRM 51-70-10-2R-4, AND SRM 51-70-10, REPAIR GENERAL, REV 83.01.SDR FDEA201810192952Support Fitting · corrodedLEFT HAND OUTBOARD FLAP VANE HORN FITTING "D" MOUNT HOLE CORRODED. CORROSION AT LEFT HAND OUTBOARD FLAP VANE HORN FITTING "D" MOUNT HOLE REWORKD BY MACHINING AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R REPAIR 5 FIGURE 201. OVERSIZED SLOT BUSHING FABRICATED BSDR FDEA201810192951Support Fitting · corrodedLEFT HAND OUTBOARD FLAP VANE HORN FITTING "F" MOUNT HOLE CORRODED. CORROSION AT LEFT HAND OUTBOARD FLAP VANE HORN FITTING "F" MOUNT HOLE REWORKD BY MACHINING AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R REPAIR 5 FIGURE 201. OVERSIZED SLOT BUSHING FABRICATED BSDR FDEA201810192950Support Fitting · corrodedLEFT HAND OUTBOARD FLAP VANE HORN FITTING "C" MOUNT HOLE CORRODED. CORROSION AT LEFT HAND OUTBOARD FLAP VANE HORN FITTING "C" MOUNT HOLE REWORKD BY MACHINING AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R REPAIR 5 FIGURE 201. OVERSIZED SLOT BUSHING FABRICATED BSDR FDEA201810192949Support Fitting · corrodedLEFT HAND OUTBOARD FLAP VANE HORN FITTING "E" MOUNT HOLE CORRODED. CORROSION AT LEFT HAND OUTBOARD FLAP VANE HORN FITTING "E" MOUNT HOLE REWORKD BY MACHINING AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R REPAIR 5 FIGURE 201. OVERSIZED SLOT BUSHING FABRICATED BSDR FDEA201810192948Support Fitting · corrodedLEFT HAND OUTBOARD FLAP VANE HORN FITTING "B" MOUNT HOLE CORRODED. CORROSION AT LEFT HAND OUTBOARD FLAP VANE HORN FITTING "B" MOUNT HOLE REWORKD BY MACHINING AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R REPAIR 5 FIGURE 201. OVERSIZED SLOT BUSHING FABRICATED BSDR SWAA2018112727139Skin · corrodedRT WING OUTBOARD AFT TRAILING EDGE FLAP UPPER SKIN CORRODED AT AFT INBOARD CORNER. REPAIRED AFT FLAP IAW SRM & AMM.SDR FDEA201810182938Idler Link · corrodedLEFT WING INBOARD FLAP INBOARD IDLER LINK HOLE BORE CORROSION. CORROSION AT LEFT HAND WING INBOARD FLAP INBOARD IDLER LINK HOLE BORE REWORKED AS PER COMPONENT MAINTENANCE MANUAL 57-52-03 AND FOUND EXCEED LIMIT AS PER DRAWING ARC2761 REV K. REPLACEMENT BUSHING SDR SWAA2022022369509Flap · delaminatedLEFT WING OUTBOARD AFT FLAP; HAS A LARGE DELAMINATION ON THE INBOARD UPPER SURFACE. / REMOVED AND REPLACES L/H O/B TRAILING AFT FLAP PER M/M 27-51-21. TAG NO: 472864 PN ON: 113A3700-19 SN ON: 001344 PN OFF: SN OFF: 000147SDR IPXA2018102935468Support Bracket · crackedRIGHT OTBD FLAP, INBD FWD HINGE FAIRING CENTER PANEL SUPPORT BRACKET WAS CRACKED. REMOVED, FABRICATED, AND REPLACED THE SUPPORT BRACKET IAW DWG ARC0504, AND SRM 51-33-01. MINOR.SDR LR7A2018102301471Skin · warpedWHILE PERFORMING OTHER MAINTENANCE TO THE LT OUTBOARD FLAP, FOUND THE TRAILING EDGE UPPER SURFACE WARPED AND CHAFED AT OWFS0L. / REPAIRED IAW SMP583 SRM, FIG. 51-140-12. NR 2003.
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