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 SWAA2019010728237Flap · delaminatedRT WING OUTBOARD TRAILING EDGE FLAP DELAMINATED AT INBOARD LOWER CORNER. REPAIRED FLAP PER SRM.SDR A6WA2018121746244Skin · gougedRH FLAP IB LOWER SKIN HAS NUMEROUS SMALL GOUGES. REPLACEDSDR SWAA2022022401256Flap · delaminatedL/H WING O/B AFT FLAP IS DELAM ON TRAILING EDGE I/B CORNER / REPAIRED L/H WING O/B AFT FLAP I/B CORNER IAW SRM 51-70-10-2R-0 REV 66 PER SRM 57-53-01-2R-4 PAR B REV 66SDR ABXA20181212141Rib · gougedGOUGE ON THE INTERNAL SPICE RIB OF THE LEFT OUTBOARD FLAP AT OTEF STATION 83.73. THE RIB WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR REXA2018121201240Skin · chafedRT IB FLAP VANE L/E CHAFED IN 3 LOCATIONS. REMOVED AND REPLACED 3 EA RT INBOARD FLAP VANE L/E SKINS IAW SRM 51-42-10.SDR DALA2018121437210Ballscrew · corroded(AIRCRAFT 6703, L/P 0862121) RII: CORROSION ON OUTBD BUSHING BALL NUT ON OUTBD BALLSCREW OF RH WING INBD FLAP. OUTBD BUSHING BALL NUT ON OUTBD BALLSCREW OF RH WING INBD FLAP WAS REPLACED AND TESTED PER B 757-200 AMM 27-51-21.SDR FDEA201812113488Rib · crackedX-RAY INSPECTION OF THE RIGHT WING CENTER FLAP TOP SKIN AND RIB FLANGES FOUND AFT RIB 20 FLANGE CRACKED. REPAIRED THE RIGHT WING CENTER FLAP CRACKED RIB UPPER FLANGE AT RIB20, STR.2.8 TO REAR SPAR PER EA 6-5750-T0344016 P1 & DRAWING A57960307. EA TITLE: WINGS SDR FDEA201812113487Rib · crackedX-RAY INSPECTION OF THE RIGHT WING CENTER FLAP TOP SKIN AND RIB FLANGES FOUND AFT RIB 26 FLANGE CRACKED. REPAIRED THE RIGHT WING CENTER FLAP CRACKED RIB UPPER FLANGE AT RIB26, STR.2.7 TO REAR SPAR PER EA 6-5750-T0344016 P1 & DRAWING A57960307. EA TITLE: WINGS SDR FDEA201812113486Rib · crackedX-RAY INSPECTION OF THE LEFT WING CENTER FLAP TOP SKIN AND RIB FLANGES FOUND AFT RIB 27 FLANGE CRACKED. REPAIRED THE LEFT WING CENTER FLAP CRACKED RIB UPPER FLANGE AT RIB27, STR.2.8 TO REAR SPAR PER EA 6-5750-T0344015 P1 & DRAWING A57960307. EA TITLE: WINGS - SDR SWAA2018121127565Skin · delaminatedLT WING OUTBOARD AFT FLAP DELAMINATED ON LOWER SURFACE INBOARD LOWER CORNER. R&R AFT FLAP PER AMM.SDR SWIA2019012945462Vane · damagedREPLACE LT INBOARD FLAP CENTER VANE CAP. (C-CHECK) RO:01/25/2019 REPLACED LT IB FLAP CENTER VANE CAP WITH NEW P/N 601R14303-51 IAW REO.SDR AALA2018121209031Strut · corrodedCORROSION FOUND ON THE LEFT WING TRAILING EDGE FLAP INTERCONNECTING STRUT. REPLACED THE INTERCONNECTING STRUT IAW AMM 27-51-44-400-001-A.SDR AALA201812119004Bracket · wornRIGHT WING INBOARD INTERCONNECTING STRUT ATTACHMENT BRACKET WORN. REPLACED THE BRACKET IAW SRM 51-72-11.SDR SWAA2019010728137Flap · delaminatedLT WING OUTBOARD AFT FLAP DELAMINATED ON LOWER AFT CORNER. REPAIRED AFT FLAP PER WO.SDR SWAA2019010728136Flap · delaminatedRT WING OUTBOARD AFT FLAP DELAMINATED ON LOWER AFT CORNER. REPAIRED AFT FLAP IAW WO.SDR 2018F00160Spar · crackedWHEN CONDUCTING A ROUTINE APPROVED MODIFICATION OF THE RIGHT FLAP WE FOUND THAT THERE WAS A CRACK IN THE AFT INBOARD SPAR (P/N 2625005-18 AT THE BEND RADIUS BETWEEN WS68 AND WS53.5. THE AIRCRAFT HAS A TOTAL TIME OF 3700 HOURS ON IT WHEN THE CRACK WAS DISCOVERSDR SWAA2018121027499Skin · delaminatedLT WING OUTBOARD AFT FLAP DELAMINATED ON UPPER AND LOWER SKINS AT INBOARD AFT CORNER. REPAIRED AFT FLAP IAW EA.SDR SWAA2018121027465Flap · delaminatedLT WING OUTBOARD AFT TRAILING EDGE FLAP DELAMINATED OF UPPER AND LOWER AT INBOARD AFT CORNER. R&R AFT FLAP PER AMM.SDR HKGA20181205004Hinge · crackedDURING AN INSPECTION, THE LT NACELLE FLAP INBOARD HINGE WAS FOUND CRACKED. REMOVED AND REPLACED FLAP ASSEMBLY IAW MM 27-50-03. OPERATIONAL CHECK GOOD.SDR R61A201901110047Rib · corrodedDURING HEAVY CHECK MAINTENANCE FOUND RT OB MAIN FLAP INTERNAL BACKUP RIB ABOVE IB FLAP TRACK IB RIB HAS CORROSION AROUND THE NUTPLATE. REMOVED AND REPLACED FLAP ASSY 170-33001-420 IAW AMM 27-51-07-00/400-801. OPERATIONAL CHECK GOOD.SDR AALA201812139013Strut · wornLEFT WING TRAILING EDGE FLAP INTERCONNECTING STRUT WAS WORN. REPLACED THE INTERCONNECTING STRUT IAW AMM 27-51-44-000-001-A.SDR AALA201812129007Strut · wornRIGHT WING TRAILING EDGE FLAP INTERCONNECTING STRUT WAS WORN. REPLACED THE INTERCONNECTING STRUT IAW AMM 27-51-44-000-001-A.SDR SWAA2022022835695Skin · delaminatedRT WING INBD MAIN FLAP OUTBD AFT T/E WEDGE PANEL LOWER SKIN DELAMINATED 4.800 IN WIDE BY 12 IN LONG AND EXTENDS TO THE T/E EDGE. DELAM STARTS 6.25 IN INBD OF OUTBD EDGE. / C/W EA REPAIR - 57EA -06019 THSI IS A TIME LIMITED REPAIRINSP P44SDR SWAA2018120427323Skin Panel · delaminatedRT WING INBOARD MAIN FLAP OUTBOARD AFT TRAILING EDGE WEDGE PANEL LOWER SKIN DELAMINATED. REPAIRED AFT FLAP PER EA.SDR DALA201812036995Flap · wornDURING FLAP/TRUNNIONS SLIDING PANEL INSPECTION FOUND NEW WEAR IN AD AREA, REPAIR REF ER/A 573428-14ADSDR CALA2018120202477Rivet · shearedFOUND SHEARED RIVET ON NR 6 FLAP TRACK SUPPORT. REMOVED AND REPLACED DAMAGED RIVETS REF SRM 51-40-02.SDR FDEA201811303403Skin · damaged[R/H WING, I/B FLAP HAS DAMAGE ON TOP OF SKIN BY STA. XIFH 155., 2018-11-30] REPAIRED THE R/H WING, I/B FLAP UPPER SURFACE PER SRM 57-10-00 FIG 85 SHEET 4 VOL 1 & TRACKING EA # 8-5710-T0343639, PART 3SDR FDEA201811303399Skin · damaged[RH INBD FLAP DAMAGED ON TOP SIDE OF FLAP., 2018-11-30] REPAIRED DAMAGE ON THE R/H FLAP, UPPER SURFACE PER SRM 57-10-00 FIG 85 SHEET 4 VOL1 & TRACKING EA # 8-5710-T0343639, PART 2SDR FDEA201811303397Skin · gouged[R/H WING I/B FLAP...TOP FWD SURFACE..APPROX C/L....WEAR MARK/GOUGE ON FLAP SKIN... REFERENCE...SNRM #203, 2018-11-30] REPAIRED THE DAMAGE PER SRM 57-10-00 FIG 85 SHEET 4 VOL 1 & R.S.C. TRACKING EA # 8-5710-T0343639, PART 1SDR SWAA2022022402998None · delaminatedSUPPLEMENTAL INFORMATION: LEFT OUTBOARD AFT FLAP HAS SMALL AREA OF DELAM AT THE LOWER INBOARD TRAILING EDGE CORNER / REPAIRED LH O/B AFT FLAP I/B CORNER DELAMINATION IAW SRM 57-53-01-2R-4 REV 66; SRM 51-70-10-R-4 REV. 66; AND SRM 51-70-10-2R-0 REV 66SDR SWAA2018121027449Flap · delaminatedRT WING OUTBOARD AFT FLAP DELAMINATED AT THE LOWER INBOARD TRAILING EDGE CORNER. REPAIRED AFT FLAP IAW SRM.SDR DALA2018112906902Skin · corrodedLH WING I/B FLAP MAIN FLAP UPPER SURFACE FOUND BULGE SKIN. REPAIRED BULGE AREA SRM 57-53-01 AND 51-70-17. (LP 0844807)SDR SCNA20181128125Flap · damagedBOTTOM OUTBOARD FLAP AT CANOE 7 OUTBOARD SIDE HAS WEAR AND MISSING PAINT FROM CANOE FLAP SURFACE. WEAR WAS FOUND TO BE ON RIGHT OUTBOARD AFT FLAP LOWER SURFACE ON A PREVIOUS REPAIR DOUBLER THAT IS WORN THROUGH DOUBLER IN THE CRITICAL AREA. DAMAGE IS OUT OF LIMSDR ASOA201812145337Skin · dentedREF: CO# 7496618 JOB# 7749661 OP# 28: DENT ON L/H INBOARD FLAP, LOWER SURFACE APPROX. 3.50" FROM INBOARD EDGE AND 1.00" FROM TRAILING EDGE. .500" IN DIAMETER, .020" DEEP. C/A: REPAIRED DAMAGE I.A.W. BOMBARDIER CRJ200 SRM 57-20-00, REPAIR #3 - INBOARD FLAP ASDR DALA2018112606869Strut · corrodedCORROSION INTERCONNECTING STRUT ON FLAP ON LEFT HAND WING. REPLACED IAW AMM 27-51-44-400-011-4.SDR DALA2019021501063Flap · damagedLEFT OUTBOARD FLAP HAS DAMAGE NEAR THE CORNER OUTBOARD AFT END. C/W ERA 573336-14.SDR DALA2018112766857Skin · worn(AIRCRAFT 6802, L/P 0837742) INITIAL INSPECTION. WORN UPPER SKIN ON INBD MAIN FLAP MF STA 295 AT LH WING. SUMMARY OF NRC 00258: PERMANET REPAIR ON UPPER SKIN ON INBD MAIN FLAP WAS ACCOMPLISHED PER ERA 573186-14 REV. ORG SECTION I.SDR DALA2018112636777Skin · delaminatedFOUND OUT O/B FLAP SKIN DELAMINATION AT TRAILING EDGE BETWEEN 13FT AND 14 FT TO HE FLAP I/B EDGE. REPAIRE PER SRM 57-53-01 (LP 0837599)SDR FDEA201811233358Skin · damagedRT I/B FLAP LOWER SKIN IS DAMAGED 47.75" FWD OF TE AND 22.875 I/B OF INNER EDGE. REPAIRED RT FLAP LOWER SKIN PER EA NR 6-5750-T03443692 P1.SDR AALA201811269021Track · looseRIGHT WING OUTBOARD FLAP DEFLECTION CONTROL TRACK CAME LOOSE. THE AIRCRAFT WAS GROUNDED. CONNECTED FLAP DEFLECTION CONTROL TRACK IAW AMM 27-51-23-101.SDR DALA2018112406754Cover · missingDURING INSPECTION, FOUND LEFT WING NR 1 FLAP FAIRING 1 COVERING (FIXED FAIRING). DEFERRED PER CDL 57-00-09 UNTIL COVER IS REPLACED.SDR FDEA201811213328Support · corrodedRIGHT HAND WING OUTBOARD FLAP VANE HORN FITTING 'F' ECCENTRIC HOLE BORE CORROSION. TEE FITTING 'F' HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIG 201 REPAIR 5. OVERSIZED BUSHING FABRICATED AS PER EA 1-5750-T0343646 P1 STEP 1B. TRACK SUPPOSDR FDEA201811213327Support · corrodedRIGHT HAND WING OUTBOARD FLAP VANE HORN FITTING 'E' ECCENTRIC HOLE BORE CORROSION. TEE FITTING 'E' HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIG 201 REPAIR 5. OVERSIZED BUSHING FABRICATED AS PER EA 1-5750-T0343646 P1 STEP 1A. TRACK SUPPOSDR AALA201812129003Tab · delaminatedAIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATION ON INBOARD FLAP TAB LOCATED AT STA RIB 4 TO RIB 6. REPAIRED INBOARD FLAP TAB ON RIGHT HAND WING PER EA 287340.SDR FDEA2018112103322Hinge Bracket · corrodedRIGHT WING - INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT HOLE SURFACE FOUND CORROSION CORROSIONS AT RIGHT WING - INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT HOLE SURFACE REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. REPAIR EVALUATED AND SDR FDEA2018112103321Hinge Bracket · corrodedRIGHT WING - INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT HOLE BORE FOUND CORROSION CORROSIONS AT RIGHT WING - INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT HOLE BORE (HOLE #3) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED BUSHINGSDR FDEA2018112103320Hinge Bracket · corrodedLEFT WING - INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT HOLE SURFACE FOUND CORROSIONS. CORROSIONS AT LEFT WING - INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-07. REPAIR EVALUATED AND SDR FDEA2018112103319Hinge Bracket · corrodedLEFT WING - INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT HOLE BORE FOUND CORROSIONS. CORROSIONS AT LEFT WING - INBOARD FLAP OUTBOARD HINGE (WING SIDE) PIVOT HOLE BORE (HOLE #3) REWORKED AND FOUND WITHIN LIMIT AS PER MD-11 CMM 57-44-07. OVERSIZED BUSHINGSDR FDEA2018112103318Hinge Bracket · corrodedLEFT WING - INBOARD FLAP OUTBOARD HINGE (WING SIDE) OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSIONS. CORROSIONS AT LEFT WING - INBOARD FLAP OUTBOARD HINGE (WING SIDE) OUTBOARD ACTUATOR LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 SDR FDEA201811203326Support Fitting · corrodedRIGHT WING OUTBOARD FLAP VANE NR 4 SUPPORT FITTING ECCENTRIC BORE HOLE FOUND CORROSION. SUPPORT FITTING HOLE BORE REWORKED AND FOUND EXCEED LIMIT AS PER SRM 57-50-02-2R FIG 201 REPAIR 5. REPAIR BUSHING FABRICATED AS PER EA 1-5750-T0343705 P1 STEP 1A. TRACK SUP
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