JASC 5753
Service difficulty reports · 31,493
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 IPXA2025092606949Rib · crackedLEFT WING CENTER FLAP, TOP SKIN RIB FLANGE, 2 CRACKS NOTED AT RIB11. CIRCLED IN RED.ACCOMPLISHED THE REPAIR IN ACCORDANCE WITH EO-94890-REQ1 AND VT-MAE EA 300-5750-27-A4108.SDR IPXA2025092607053Rib · crackedLEFT WING CENTER FLAP, TOP SKIN RIB FLANGE, 1 CRACK NOTED AT RIB15. CIRCLED IN RED.ACCOMPLISHED THE REPAIR IN ACCORDANCE WITH EO-94890-REQ1 AND VT-MAE EA 300-5750-27-A4108.SDR IPXA2025092607057Rib · crackedLEFT WING CENTER FLAP, TOP SKIN RIB FLANGE, 1 CRACK NOTED AT RIB19. CIRCLED IN RED.ACCOMPLISHED THE REPAIR IN ACCORDANCE WITH EO-94890-REQ1 AND VT-MAE EA 300-5750-27-A4108.SDR IPXA2025092607061Rib · crackedLEFT WING CENTER FLAP, TOP SKIN RIB FLANGE, 1 CRACK NOTED AT RIB25. CIRCLED IN RED.ACCOMPLISHED THE REPAIR IN ACCORDANCE WITH EO-94890-REQ1 AND VT-MAE EA 300-5750-27-A4108.SDR IPXA2025091499931Flap · corroded***SUPPLEMENTAL SDR*** FAULT - STR, Z600, RH WING, O/B FLAP, UPPER SKIN, O/B SIDE, UNDER STATIC WICK HAS CORROSION. DOT 103-8. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-94994-REQ1 AND VT-MAE EA 300-5754-27-A4128.SDR IPXA2025092607301Rib · crackedRIGHT WING CENTER FLAP, TOP SKIN RIB FLANGE, TWO CRACKS NOTED AT RIB 25. ACCOMPLISHED PERMANENT REPAIR IAW EO-94891-REQ1 AND EA 300-5750-27-A4107, REV -.SDR IPXA2025101307330Rib · crackedRIGHT WING CENTER FLAP, TOP SKIN RIB FLANGE, TWO CRACKS NOTED AT RIB 27. ACCOMPLISHED PERMANENT REPAIR IAW EO-94891-REQ1 AND EA 300-5750-27-A4107, REV -.SDR IPXA2025092607320Rib · crackedMAJOR REPAIR, RT WING CENTER FLAP, TOP SKIN RIB FLANGE, TWO CRACKS NOTED AT RIB 26. ACCOMPLISHED PERMANENT REPAIR IAW EO-94891-REQ1 AND EA 300-5750-27-A4107, REV. -.SDR IPXA2025092607221Rib · crackedMAJOR REPAIR, RT WING CENTER FLAP, TOP SKIN RIB FLANGE, TWO CRACKS NOTED AT RIB 13. ACCOMPLISHED PERMANENT REPAIR IAW EO-94891-REQ1 AND EA 300-5750-27-A4107, REV. -.SDR IPXA2025092607255Rib · crackedMAJOR REPAIR. RT WING CENTER FLAP, TOP SKIN RIB FLANGE, ONE CRACK NOTED AT RIB18. ACCOMPLISHED PRMANENT REPAIR IAW EO-94891-REQ1 AND EA 300-5750-27-A4107, REV. -.SDR IPXA2025091007330Rib · crackedMAJOR REPAIR, RT WING CENTER FLAP, TOP SKIN RIB FLANGE, 2 CRACKS NOTED AT RIB27.SDR IPXA2025091907221Rib · crackedMAJOR REPAIR, RT WING CENTER FLAP, TOP SKIN RIB FLANGE, 2 CRACKS NOTED AT RIB13.SDR IPXA2025091549931Skin · corrodedRIGHT WING, OTBD FLAP, UPPER SKIN, O/B SIDE, UNDER STATIC WICK HAS CORROSION. DOT 103-81 VERIFIED STEP #22 OF PRELIMINARY #1, E.A.#300-5754-27-A4128OF. VERIFY SERVICE DIFFICULTY REPORT HAS BEEN INITIATED. (T3F18E007E5EA)SDR IPXA2025091507320Rib · crackedRIGHT WING CENTER FLAP, TOP SKIN RIB FLANGE, HAD 2 CRACKS AT RIB 26. COMPLIED WITH STEP 33 OF EA 300-5750-27-A4107, PRELIMINARY 1.SDR SWAA2025082607221Skin · delaminatedTRAILING EDGE LT OTBD AFT FLAP, INBD SIDE, SKIN DELAMINATION ON LOWER SKIN. REMOVED DAMAGE, FABRICATED REPAIR IAW SRM 57-53-01-2R-14, & SRM 51-70-10-2R-4, REPAIR 4, REMOVED OTBD AFT FLAP IB SEAL IAW CMM 57-53-08. INSTALLED REPAIR & BAGGED AND COOKED IASDR IPXA2025092690143Rib · crackedRIGHT WING, CENTER FLAP, TOP SKIN RIB FLANGE, ONE CRACK INDICATION NOTED AT RIB 27. ACCOMPLISHED PERMANENT REPAIR IAW EO-95120-REQ1 AND VT-MAE EA 300-5750-27-A4111.SDR IPXA2025090597004Fitting · gougedRIGHT WING. FLAPS GUIDE ROLLER FITTING HAS CHAFING ON THE LOWER SURFACE.(DM08). ACCOMPLISHED REPAIR PER EO-94899-REQ1 AND VT-SAA EA 757-5750-01-B0560.SDR IPXA2025090495838Tee Angle · brokenR/H WING. I/B FLAP HAS BROKEN T-ANGLE SUPPORT LOCATED AT O/B SIDE OF THE FLAP.(DM09) ATA57. INSTALLED TEE-ANGLE SUPPORT AT R/H WING. I/B FLAP. LOCATED AT O/B SIDE OF THE FLAP I.A.W. B757-200PF SRM 51-40-02-0G-0 AND BOEING DWG NO.113N2605.SDR DALA2025082506315Fairing · corrodedCORROSION BONDING PLATE FLAP TRACK FAIRING 4 (533CB) ON LH WING. COMPLIED WITH ER/A 622998-14TR. (1156742).SDR DALA2025082506314Fairing · corrodedCORROSION BONDING PLATE FLAP TRACK FAIRING 2 (531CB) ON LH WING. COMPLIED WITH ER/A 622998-14TR. (1156727).SDR SWAA2025092206607Skin · delaminatedLEFT WING OTBD AFT FLAP HAS LARGE AREA OF DELAMINATION ON UPPER SURFACE ON INBD CORNER. REMOVED LT WING OTBD AFT FLAP IAW AMM 27-51-22. INSTALLED LT WING OTBD AFT FLAP IAW AMM 27-51-22.SDR SWAA2025082206127Skin · corrodedLH INBOARD AFT FLAP HAS INTERGRANULAR CORROSION AT TRAILING EDGE APPROX. MID WAY DAMAGE IS LOCATED AT TRAILING EDGE 30.5' FROM OUTBOARD EDGE. DAMAGE IS 3.875 ' X 1.625'<[01] REMOVED AND REPLACED LH IB AFT FLAP; OPS CHECK GOOD REF. AMM 27-51-12.SDR DALA2025082106240Skin · dentedFOUND DENT ON RT INBD FLAP. ACTION: PER ER/A 628685-14 (7589627)SDR SWI2025F01693Actuator · gougedRIGHT INBOARD VANE ACTUATOR GOUGED. COMPLIED WITH THE REPAIR OF RH FLAP INBD VANE ACTUATOR IAW REO 670-57-52-257, REV B. OPS CHECKED GOOD.SDR SWAA2025082206039Wedge · debondedLH INBOARD MAIN FLAP (P/N: 113A2100-71; SN: 000489) TRAILING LOWER SKIN DISBOND - PERMANENT REPAIR)<[01] REMOVED L/H I/B DAMAGED FLAP WEDGE AND UPPER PANEL TO FOM PER SRM 51-40-02;[02] REMOVED L/H I/B MAIN FLAP DAMAGED TRAILING EDGE WEDGE ASSEMBLY FOR REPLACEMSDR DALA2025082006233Strut · corrodedCORROSION INTERCONNECTING STRUT OB FLAP ON LH WING. REPLACED INTERCONNECTING STRUT OB FLAP ON LH WING AS PER A320 FAM AMM 27-51-44-000-001-A. (1152557)SDR FDEA202508191506Skin · damagedRH WING, INBD MAIN FLAP, UPPER SURFACE, 68" FROM OUTBD EDGE AND 20" FROM TRAILING EDGE, PUCTURE, RH WING, INBD MAIN FLAP UPPER SURFACE, 68" FROM OUTBD EDGE AND 20" FROM TRAILING EDGE WAS REPAIRED I.A.W. B767 SRM 57-53-01-2R, FIGURE 201 SHEET 2 AND SRM 51-SDR FDEA202508171484Skin · dentedLEFT OTBD FLAP LWR SURFACE FROM IB TO OB 40 INCHES CORSS TE TO LE 12 INCHES FOUND ONE DENT. REPAIRED LH OB FLAP LWR SURFACE DENT AT OTEF STA 73 AS PER B777 SRM 57-53-01-2R REPAIR 2 AND SRM 51-70-04-2R REPAIR 1 REV 47.6 AND EA: G-5750-T0384564 PI, TITLE: WISDR FDEA202508171483Skin · dentedLEFT OTBD FLAP LWR SURFACE FROM OB TO IB 93 INCHES CORSS TE TO LE 4 INCHES FOUND ONE DENT. REPAIRED LH OB FLAP LWR SURFACE DENT AT OTEF STA 434 AS PER B777 SRM 57-53-01-2R REPAIR 2 AND SRM 51-70-04-2R REPAIR 1 REV 47.6 AND EA: G-5750-T0384564 PI, TITLE: WISDR FDEA202508171482Skin · dentedFOUND RHW T/E O/B FLAP LOWER SURFACE 01 EA DENT AT THE CROSS OTEF 428 AND T/E 4 INCHES. REPAIRED RHW T/E O/B FLAP LOWER SURFACE 01 EA DENT AT OTEF STA 428 AS PER B777 SRM 57-53-01-2R REPAIR 2 AND SRM 51-70-04-2R REPAIR 1 REV 47.6 AND EA:G-5750-T0384565 P1SDR FDEA202508171481Skin · dentedFOUND RHW T/E O/B FLAP LOWER SURFACE 01EA DENT AT THE CROSS OTEF 127 AND T/E 01 INCHES. REPAIRED RHW T/E O/B FLAP LOWER SURFACE 01EA DENT AT OTEF STA 127 AS PER B777 SRM 57- 53-01-2R REPAIR 2 AND SRM 51-70-04-2R REPAIR 1 REV 47.6 AND EA: G-5750-T0384565 P1 , SDR SWAA2025090805147Support Bracket · crackedCRACK SUPPORT BRACKET TRAILING EDGE ORSS 271 AT LT WING. REPLACED SUPPORT BRACKET AND FASTENERS LOCATED TRAILING EDGE ORSS 271 AT LT WING I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG: 115A2900 SHEET: 1 REV: E.SDR 7C7A2025081500031Fairing · damagedEVIDENCE OF DAMAGE AT EDGE OF CANOE PANEL 672HB.SDR FDEA202508141452Skin · damagedPUNCTURE ON LEADING EDGE OF OUTBOARD FLAP AT RH WING, AT 72" FROM IMBOARD EDGE. LEADING EDGE OF OUTBOARD FLAP AT RH WING, AT 72" FROM OUTBOARD EDGE WAS REPAIRED I.A.W. B-767, SRM 57-53-01-2R, FIG 201, TABLE I AND SRM 51-70-03-0G, PAR. 5.A, REV. 92, APR-15- SDR FDEA202508141451Skin · delaminatedDELAMINATION ON LEADING EDGE OF OUTBOARD FLAP AT RH WING, AT 135" FROM OUTBOARD EDGE. LEADING EDGE OF OUTBOARD FLAP AT RH WING, AT 135" FROM OUTBOARD EDGE WAS REPAIRED I.A.W. B-767, SRM 57-53-01-2R, FIG 201, TABLE I AND SRM 51-70-03-0G, PAR. 5.A, REV. 92, SDR 7C7A202508130001Hinge · damagedLH ENG OB LOWER BLOCKER FLAP #6 FROM 12 OCLOCK POSITION LOWER HINGE ATTACHEMENT PLATE HAS MISSING PIECESDR SWAA2025091503810Skin · delaminatedLEFT WING OTBD AFT FLAP INBD UPPER SURFACE DELAMINATED. REMOVED AND REPLACED THE LT WING OTBD AFT FLAP IAW AMM 27-51-22-000-801, AND AMM 27-51-22-400-801.SDR FDEA202508121408Skin · crackedNDT INSP FOUND RH WING CENTER FLAP TOP SKIN FLANGE RIB26 STGR2.7 AND STGR 2.8 CRACKED COMPLIED WITH EA: 6-5750-T0384484 P1, TITLE: WINGS - FLIGHT SURFACES - RH CENTER FLAP - CRACK IN UPPER FLANGES OF RIB 26 REPAIRED THE CRACKED RIB UPR FLANGE AT RH WING SDR SWAA2025081803425Fairing · pulledFLAP SUPPORT FAIRING NO. 3 AFT TAIL CONE HAS FASTENER PULLING THROUGH FAIRING.SDR DALA2025081306057Bearing · looseLEFT WING O/B MAIN FLAP I/B SPHERICAL BEARING LOOSE. COMPLIED WITH ER/A 627489-14.SDR SWI2025F01117Flap Track · out of limitsR/H WING FLAP TRACK #1A UPPER FLANGE HAS THICKNESS REDUCTION OF .040" WITH FLAPS EXTENDED. ASSET TC2-7654 CAL DUE 01/15/26 (C-CHECK RO 08/26/2025)REMOVED AND REPLACED R/H WING FLAP TRACK #1A REF EMB 175 AMM 57-54-25. ASSET #TC1-601 CAL DUE 7/17/26.SDR SWI2025F01116Flap Track · out of limitsL/H WING FLAP TRACK #1A I/B UPPER FLANGE HAS THICKNESS REDUCTION OF .030" WITH FLAPS EXTENDED. ASSET TC2-7654 CAL DUE 01/15/26 (C-CHECK RO 08/26/2025)REMOVED AND REPLACED L/H WING FLAP TRACK #1A I/B. REF ERJ175 AMM 57-54-25. TW ID# HG4-50096 CAL DUE 3-20-26.SDR SWAA2025081400110Skin · delaminatedLEFT TRAILING EDGE OTBD AFT FLAP HAS DELAMINATION AND DAMAGE ON I/B AFT EDGE. THE DELAMINATION AREA OF THE LOWER SKIN IS APPROX. 11.5' BY 14'. INCLUDING 5 FASTENER HOLES COMPLETELY PULLED THROUGH. THE MISSING MATERIAL TO THE LOWER SKIN IS ROUGHLY 5.5' X 2.0'. SDR SWAA2025091199670Access Panel · damagedELONGATED HOLE ACCESS PANEL 551BT TRAILING EDGE AT LT WING. REPAIRED ACCESS PANEL 551BT TRAILING EDGE AT LT WING IAW B737-800 SRM 51-70-04-2R-10 REPAIR 10.SDR AALA202509057901Plate · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT WING TRAILING EDGE OUTBOARD FLAP UPPER SURFACE PLATE WORN BETWEEN FLAP RIBS 1 AND 2. REPLACED PLATE PER SRM 57-53-11-300-008.SDR JJBA20250827059Angle · corrodedRIGHT INBD FLAP INBD TIP, ONE ANGLE IS CORRODED. RT INBD FLAP INBD TIP, ONE ANGLE BLENDED OUT OF LIMITS. RH INBD FLAP INBD TIPO, ANGLE REMOVED AND REPLACED.SDR COEA2025081101819Skin · damagedFLT # 7739, BIL-GTF. HAIL DAMAGE ON LEFT SIDE FLAP CORRECTIVE ACTION: FERRIED TO COE FOR FURTHER EVALUATION. UPON FURTHER REVIEW, THE DAMAGE DISCOVERED ON THE L/H SIDE WING DID NOT WARRANT REPORTING DUE TO BEING SECONDARY STRUCTURE.SDR UIEA2025080501086Fairing · delaminatedLEFT WING OTBD FORE FLAP L/E FAIRING FOUND DELAMINATED. PERFORMED PERMANENT COMPOSITE REPAIR AS PER SRM 51-70-07, PAR.5.A.(1). NO FURTHER DEFECTS NOTED.SDR UIEA2025080501087Fairing · delaminatedLEFT WING OTBD FORE FLAP L/E FAIRING FOUND DELAMINATATED. PERFORMED PERMANENT COMPOSITE REPAIR IAW SRM 51-70-07, PAR.5.A.(1). NO FURTHER DEFECTS NOTED.SDR UIEA2025080501088Fairing · delaminatedLEFT WING OTBD MID FLAP L/E FAIRING FOUND DELAMINATED. PERFORMED PERMANENT COMPOSITE REPAIR AS PER SRM 51-70-07, PAR.5.A.(1). NO FURTHER DEFECTS NOTED.
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