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 SWIA202054998Hinge Fitting · chafedRIGHT WING FLAP HINGE BOX HAS CHAFING DAMAGE ON CENTER MOUNT FITTING. C-CHECK RO 12/30/2020. REPAIRED RT WING FLAP HINGE BOX CENTER MOUNT FITTING, IAW REO. MAJOR REPAIR TASK & FORM M337 COMPLETED AND ATTACHED. NO MEASURABLE WEIGHT CHANGE. REFER TO CONTINUSDR SWIA202054997Hinge Fitting · gougedRT INBOARD FLAP, OUTBOARD/AFT HINGE BOX ATTACH FITTING GOUGED APPROXIMATELY .5" LONG. C-CHECK RO 12/30/2020. REPAIRED IAW REO. MAJOR REPAIR TASK & FORM M337 COMPLETED AND ATTACHED. NO MEASUREABLE WEIGHT CHANGE. REFER TO CONTINUE CARD FOR WORK. PERFORMEDSDR FDEA202011192910Skin · delaminatedDISBOND UPPER SURFACE RIGHT INBOARD MAIN FLAP REPAIRD UPPER SURFACE OF RT INBOARD MAIN FLAP, IAW B757 SRM 51-70-10-2R REP 2 AND 57-50-01 01-2R REP 1.SDR EE4Y2020111911950Skin · crackedRT WING TRAILING EDGE AT WBL 204, FLAP LEADING EDGE SKIN WITH CRACK. NOTE: IT WAS REPAIRED, AS PER B737-400 SRM INSTRUCTIONS (REF: JOB: A1J185 NRI: 6-54).SDR SWAA2021081231739Wedge · delaminatedL/H WING I/B MAIN FLAP HAS 3 AREAS OF DELAMINATION ON UPPER SURFACE TRAILING EDGE / R/R L/H I/B WEDGE PANEL IAW SRM 51-40-02 POS: L/HSDR SWIA202055484Vane · wornRT WING INBOARD FLAP VANE HAS 3 EA WEAR MARKS ALONG LEADING EDGE, AREAS MARKED. C-CHECK RO 1/16/2021. REMOVED 3 EA WEAR MARKS ON RT WING INBOARD FLAP VANE LEADING EDGE, REF REO 601R-57-52-004, REV -D, DATED 2012-12-19. ALL 3 EA LOCATIONS ARE OUT OF LIMITS, SDR SWIA202055402Vane · wornLT WING INBOARD FLAP VANE HAS 3 EA WEAR MARKS ALONG LEADING EDGE, AREA MARKED. C-CHECK RO 1/16/2021. INSTALLED LT WING INBOARD FLAP (OUTBOARD) VANE, REF CRJ200 SRM 51-42-13 AND DWG 601R14303 REV J. COMPLIED WITH 51-900-1003-SKY AND SEE CONTINUATION CARD FORSDR SWIA202055929Panel · chafedCHAFFING ON THE RIGHT HAND WING INBOARD FLAP PANEL 684ET. (C-CHECK) RO 2/1/2021 BLENDED CHAFFED AREA ON PANEL 684ET REF CRJ900 SRM 51-12-00-001-001-A01.FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED PANEL AND REPLACED WITH NEW PANEL P/N:CC670-14027-3 AND BOMBASDR SWIA202055928Skin · chafedCHAFFING ON THE RIGHT HAND WING INBOARD FLAP PANEL 684EB. (C-CHECK) RO 2/1/2021 REMOVED CHAFFING ON THE RH WING INBD FLAP PANEL 684EB. FOUND REWORKED AREA TO BE OUT OF LIMITS, REMOVED DAMAGED PANEL AND REPLACED WITH NEW PANEL P/N:CC670-14177-2. SEE CONTINUSDR SWIA202055925Skin · chafedCHAFFING ON THE RIGHT HAND WING INBOARD FLAP PANEL 684GB. (C-CHECK) RO 2/1/2021 REPLACED PANEL 684GB P/N CC670-14178-1 DUE TO OUT OF LIMITS CHAFFING IN REF CRJ900 SRM 57-52-01-101-001-A01. ORDERED AND RECEIVED NEW SERVICEABLE PANEL. SEE CONTINUATION CARD FSDR SWIA202055483Skin · dentedLT OUTBOARD FLAP, LOWER SKIN HAS A DENT, INBOARD OF THE CENTER HINGE ARM, MARKED. C-CHECK RO 1/16/2021. DENT ON LT OUTBOARD FLAP, LOWER SKIN MEASURES 1.30" X 1.30" WITH A DEPTH OF .036". DENT IS IN CLOSE PROXIMITY TO FASTENERS AND CHEM MILL. DENTED AREA ISSDR SWIA202054498Skin · chafedLEFT INBOARD FLAP VANE LEADING EDGE CHAFED AT INBOARD .018" OUT OF LIMIT REQUIRES REPLACEMENT. C-CHECK RO 12/04/2020. REMOVED LT INBOARD FLAP LEADING EDGE INBOARD PANEL AND INSTALLED A NEW PANEL, IAW CRJ 200 SRM.SDR IPXA2020111662460Skin · damagedINSPECTION TYPE: N/A LT WING INBOARD FLAP UPPER SKIN DAMAGE. REPAIRED PER EO A300-5750-78068-B.SDR IPXA2020111662459Skin · dentedINSPECTION TYPE: N/A LT WING OUTBOARD TRAILING EDGE FLAP LOWER SKIN DENTED. REPAIRED PER EO B767-5750-78220-B REPAIRED ON N/R'S 662344 AND 662346.SDR SCNA20201201378Cover Plate · corrodedMAIN INBOARD MAIN FLAP COVER PLATE AND STRAP HAVE CORROSION AROUND FASTENER HOLES. REMOVED AND REPLACED RT MAIN FLAP INBOARD COVER PLATE, IAW SRM 51-40-08-0G-0 PAR 5 AND DWG 113A2001 REV H.SDR GTIA2020111635448Skin · chafedLT WING OUTBOARD FLAP INBOARD EDGE CHAFED, DUE TO CHAFING BETWEEN LT WING ICS CONNECTOR SHIELD AND OUTBOARD FLAP INBOARD EDGE. RAF 2649075-01 CREATED SEE LTPR NRI 5001024994-0020 FOR CORRECTIVE ACTION. REVIEWED LTPR NR 5001024994-0020 LT WING OUTBOARD FLAP ISDR FDEA202011142846Bracket · corrodedLEFT HAND WING FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT HOLE BORE, FOUND CORROSION. CORROSION AT LEFT HAND WING FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT HOLE BORE (HOLE G AND F). REWORKED AND FOUND EXCEED LIMIT, AS PER MD-11 CMM 57-52-0SDR FDEA202011142845Bracket · corrodedLEFT HAND WING FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT HOLE BORE, FOUND CORROSION. CORROSION AT LEFT HAND WING-FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT HOLE BORE (HOLE B AND A) REWORKED AND FOUND EXCEED LIMIT, AS PER MD-11 CMM 57-52-0SDR FDEA202011142844Bracket · corrodedRIGHT HAND WING-FLAP SIDE INBOARD FLAP OUTBOARD HINGE INBOARD PIVOT HOLE BORE FOUND CORROSION (G AND F HOLES). REWORKED AND FOUND EXCEED LIMIT, AS PER MD-11 CMM 57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED, AS PER MD-11 CMM 57-52-03 AND SDR FDEA202011142843Bracket · corrodedRIGHT HAND WING-FLAP SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD PIVOT HOLE BORE FOUND CORROSION (B AND A HOLES). REWORKED AND FOUND EXCEED LIMIT, AS PER MD-11 CMM 57-52-03. OVERSIZED BUSHING FABRICATED BY MACHINING AND INSTALLED, AS PER MD-11 CMM 57-52-03 ANDSDR IPXA2020111462363Skin · delaminatedINSPECTION TYPE: SEG RT WING OUTBOARD FLAP UPPER SURFACE DISBOND ON THE TRAILING EDGE. REPAIRED IAW SRM B757 51-70-07-OG, PER SRM 57-53-01-2R-1 250 DEGREES AT 90 MINS.SDR IPXA2020111462362Skin · delaminatedINSPECTION TYPE: SEG RT WING OUTBOARD UPPER SURFACE DISBOND ON THE TRAILING EDGE. REPAIRED IAW SRM B757 B757 51-70-07-OG, PER SRM 57-53-01-2R-1 250 DEGREES AT 90 MINUTES.SDR IPXA2020111462365Skin · delaminatedINSPECTION TYPE: SEG RT WING OUTBOARD FLAP UPPER SURFACE DISBONDED ON THE TRAILING EDGE. REPAIRED IAW SRM B757 51-70-07-OG, PER SRM 57-53-01-2R-1 250 DEGREES AT 90 MINS.SDR IPXA2020111462364Skin · delaminatedINSPECTION TYPE: SEG RT WING OUTBOARD UPPER SURFACE DISBOND ON THE TRAILING EDGE. REPAIRED IAW SRM B757 51-70-07-OG, PER SRM 57-53-01-2R-1 250 DEGREES AT 90 MINS.SDR SWIA202054977Bushing · dentedLT INBOARD FLAP HAS 2 DENTS/GOUGES. ONE MEASURES .5" X .5" AND IS LOCATED BETWEEN WS 68.138 & WS 79.062 BELOW LOWER INTERCOSTAL. THE SECOND MEASURES 1" X 1" BETWEEN WS 68.138 & WS 79.062 ABOVE TOP INTERCOSTAL. BOTH DENTS HAVE BEEN DETERMINED TO BE OUT OF LISDR SWAA2021072833035Fairing · crackedCRACK FLAP TRACK FAIRING 543BB ON PRELOAD PAD AT LT WING / REPLACED PRELOAD ON FLAP TRACK FAIRING 543BB AT LT WING IAW B737-700 SRM 51-40-02 AND PERFORMED ADJUSTMENT CHECK IAW B737-700 AMM 27-51-28-820- 802 AND ADJUSTMENT IS OKSDR SCNA20201117324Fairing · damagedNR 1 FLAP AFT FAIRING HAS DAMAGE ON INNER SKIN. REPAIRED NR 1 FLAP AFT FAIRING INNER SKIN, IAW ER 20-03509 REV IR AND SC EA 57-0055.SDR SCNA20201117298Skin · damagedLT OUTBOARD FLAP LEADING EDGE PANEL 567AT DAMAGED. LT OUTBOARD FLAP LEADING EDGE PANEL 567AT FOUND TO BE OUT OF LIMITS, IAW SRM 57-53-01-1A-3 RECEIVED NEW FLAP LEAD EDGE. LOCATED, DRILLED, TOP COATED IAW SRM 51-40-05-0G-0 AMM 51-21-99-300-801.SDR SCNA20201117297Fairing · damagedLT WING NR 3 FLAP AFT FAIRING HAS DAMAGE ON INNER SKIN. REPAIRED LT WING NR 3 FLAP AFT FAIRING INNER SKIN, IAW ER 20-0352 REV IR AND SC EA 57-0054.SDR IPXA2020111062235Link · gougedINSPECTION TYPE: A300 LT MID FLAP OUTBOARD LINK CUTOUT HAS A DEEP GOUGE. REPAIRED AREA IAW EA 300-5753-27-A2514/UPS EO A300-5750-78403.SDR SWAA2021071329560Skin · debondedDEBONDED OB AFT FLAP UPPER SKIN I/B EDGE AT RT WING / REPAIRED O/B AFT FLAP UPPER SKIN I/B EDGE AT RT WING AS PER B737-700 SRM 57-53-01-2R-16 REPAIR 16 AND B737-700 SRM 51-70-10-2R-0 REPAIR GENERAL. THIS IS AN INTERIM REPAIR. FOR INSPECTIONS REQUIREMENTS SEE TSDR SWIA202054343Vane · chafedLT INBOARD FLAP VANE TRAILING EDGE MID UPPER SIDE HAS CHAFING DAMAGE. C-CHECK RO 11/23/2020. REMOVED THE CHAFE DAMAGE FROM THE LT INBOARD FLAP VANE UPPER TRAILING EDGE SKIN, REF CRJ200 SRM, FOUND TO BE OUT OF LIMITS. RECEIVED AND COMPLIED WITH ALL STEPS OF SDR SWIA202054313Vane · chafedRT INBOARD FLAP VANE LEADING EDGE INBOARD SIDE HAS CHAFING DAMAGE. C-CHECK RO 11/23/2020. REMOVED CHAFE DAMAGE FROM RT INBOARD FLAP VANE LEADING EDGE, INBOARD SIDE, REF CRJ200 SRM. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW RT INBOARD FLAP VANE CSDR SWIA202054312Vane · chafedLT INBOARD FLAP VANE LEADING EDGE OUTBOARD SIDE HAS CHAFING DAMAGE. C-CHECK RO 11/23/2020. REMOVED CHAFE DAMAGE ON LT INBOARD FLAP VANE LEADING EDGE OUTBOARD SIDE, REF CRJ200 SRM. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW VANE CAP AT LT INBOARD SDR IPXA2020112262659Beam · crackedINSPECTION TYPE: 2C RT OUTBOARD FLAP INBOARD HINGE FAIRING BEAM CRACK. REMOVED AND REPLACED CRACKED BEAM AT RT OUTBOARD FLAP INBOARD HINGE, IAW SRM 51-35-01,51-33-01 AND DWG ARC2151. (MINOR)SDR IPXA2020112262661Bracket · corrodedINSPECTION TYPE: 2C RT WING OUTBOARD FLAP INBOARD HINGE LUG HOLES CORRODED. REPAIRED RT OUTBPARD FLAP INBOARD HINGE CORRODED LUG HOLES, IAW VT-SAA EA 011-5740-01-A8716 REV I/R AND UPS EO MD11-5750-78565-A. (MINOR).SDR SCNA20201117328Panel · damagedRT WING INBOARD FLAP PANEL 653ET HAS DAMAGED HONEYCOMB ON LOWER SURFACE. REPAIRED DAMAGE TO HONEYCOMB ON LOWER (INNER) SURFACE OF RT WING INBOARD FLAP PANEL 653ET, PER SRM 51-70-10-2R-4.SDR SCNA20201116284Fairing · damagedLT WING FLAP TRACK FAIRING 542BB (3) HAS GOUGE ON FWD EDGE. REPAIRED DAMAGE TO LT WING FLAP TRACK FAIRING 542BB, IAW SRM 51-70-04 AND EA 57-0052 (ER# 20-03440 RV IR).SDR SCNA20201116283Fairing · damagedLT WING FLAP TRACK FAIRING 542BB (3) HAS INTERIOR DAMAGE 47" FROM FWD EDGE. REPAIRED LT WING FLAPTRACK FAIRING 542BB INTERIOR 47" FROM FWD EDGE, IAW SRM 51-70-04, EA 57-0052 ER 20-03440 RV IR.SDR SCNA20201116281Fairing · damagedRT WING FLAP TRACK FAIRING 642BB (6) HAS INTERIOR DAMAGE 49" FROM FWD EDGE. REPAIRED INTERIOR DAMAGE 49" FROM FWD EDGE ON RT WING FLAP TRACK FAIRING 642BB(6), IAW SRM 51-70-04-2R-1 + ER NR 20-03442 REV P1. RT WING FLAP TRACK FAIR 642BB(6) WILL BE REPLACED WISDR SCNA20201116279Fairing · gougedRT WING MID FLAP FAIRING 642BB (6) HAS GOUGE ON LEADING EDGE. REPAIRED RT WING MID FLAP FAIRING 642BB LEADING EDGE, IAW SRM 51-70-04 AND EA 57-0053 (ER NR 20-03442 RV IR).SDR SWIA202054729Skin · chafedRT INBOARD FLAP LOWER SKIN IS CHAFED AROUND PERIMETER OF INBOARD FAIRING. C-CHECK RO 12/24/2020. REPAIRED RT INBOARD FLAP LOWER SKIN CHAFE BY DOING A SKIN SPLICE REPAIR, IAW CRJ700 SRM. COMPLETED TASK CARD AND ATTACHED FORM M-337. WEIGHT CHANGE +3.83 LBS, SDR 2020F00440Skin · gougedLEFT WING INBOARD FLAP DAMAGE (GOUGE). ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ27564M1 DATED NOVEMBER 4, 2020; 680A-0052 (N514QS) LEFT WING INBOARD FLAP DAMAGE (GOUGE).SDR IPXA2020112362695Skin · crackedINSPECTION TYPE: 2C RT OUTBOARD FLAP HAS A CRACKED FITTING INSIDE PANEL 657HT, HINGE ATTACH FITTING. REMOVED AND REPLACED RT OUTBOARD FLAP, IAW AMM27-50-30-400-802. (MINOR)SDR IPXA2020111762497Skin · dentedINSPECTION TYPE: 4C LT WING INBOARD FLAP UPPER SKIN HAS 2 EA LARGE DENTS 45" FROM TRAILING EDGE AND 77' FROM INBOARD END. REPAIRED DENTED LT WING INBOARD FLAP UPPER SKIN AT STA XIFH 203 AND XIFH 39, IAW MD-11 SRM 57-00-01, REPAIR 1, FIGURE 201. (MAJOR)SDR SCNA20201116282Fairing · damagedLT WING FLAP TRACK FAIRING 543BB (2) HAS INTERIOR DAMAGE 45-51" FROM FWD EDGE. REPAIRED LT WING FLAP TRACK FAIRING 543BB (2) INTERIOR DAMAGE 45-51" FROM FWD EDGE, IAW EA 57-0051 8ND ATS ER 20-03447 REV IR.SDR SWAA2021082627922Bracket · crackedR/H WING AFT FIXED TRAILING EDGE PANEL SEAL BRACKET CRACKED. / REMOVED AND REPLACED R/H AFT FIXED TRAILING EDGE PANEL SEAL BRACKET PER S.I.P.SDR IPXA2020112262657Skin · crackedINSPECTION TYPE: 2C LT OUTBOARD FLAP INBOARD HINGE FITTING CRACK. REMOVED AND REPLACED LT OUTBOARD FLAP ASSEMBLY, IAW AMM 27-50-30-000-802 AND AMM 27-50-30-400-802. (MINOR)SDR SWIA202054128Skin · chafedLT INBOARD FLAP LEADING EDGE PANEL 584GB HAS CHAFE MARK. C-CHECK RO 11/16/2020. REPLACED LT INBOARD FLAP LEADING EDGE PANEL 584GB, REF CRJ700 SRM. INSTALLATION ACCOMPLISHED ON JOB 71028670 OP 7005. SEE CONTINUE CARD FOR DETAILS.SDR SWIA202054731Skin · chafedLT INBOARD FLAP LOWER SKIN IS CHAFED AROUND PERIMETER OF INBOARD HINGE FAIRING. C-CHECK RO 12/24/2020. REPAIRED LT INBOARD FLAP LOWER SKIN CHAFE BY DOING A SKIN SPLICE REPAIR, IAW CRJ700 SRM. COMPLETED TASK CARD AND ATTACHED FORM M-337. WEIGHT CHANGE +3.83
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