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 IPXA2024012287659Skin · cracked**SUPPLEMENTAL SDR**FAULT - CRACK - SKIN, RH WING NO.18 VC FLAP FOLDING NOSE INBD END. (REPAIR) REVIEWEDSDR IPXA2024012285873Skin · debonded**SUPPLEMENTAL SDR**FAULT - DISBOND - SKIN PNL, LH WING INBD FORE FLAP NOSE SKIN PNL (REPAIR) REVIEWEDSDR DALA2024010800282Unknown · unknownSHIP 3120 CORROSION ON LUG I/B AND O/B FACE ON TRACK 3 LH O/B FLAP. CORRECTIVE ACTION: REPAIRED PER ER/A # 614191-14. (0141456)SDR ASAA2024010447267Skin · debondedCUSTOMER REQUEST PER MONTHLY-LW OB TE AFT FLAP LOWER INBOARD SKIN DELAMINATED. GROUNDED - YES. REPAIRED L/W O/B T/E AFT FLAP I/B SKIN DELAMINATION IAW B737-900ER SRM 57-53-01-2R-16 REP.16 51-70-10-2R-0. THIS IS AN INTERIM REPAIR AND WILL REQUIRE TAP TEST INSPESDR DALA2024010900365Unknown · unknownSHIP 1705 WHEN PERFORM WORD CARD 5750-01118-1208, INSTALL THE TORQUE TUBE (P/N:113T2250-7) WITH THE SHEAR TUBE(P/N :113T2251-3), FOUND THE BUSHING(PN:113T2231-2) OF THE TORQUE TUBE(P/N:113T2250-7) INNER DIAMETER SMALL. CORRECTIVE ACTION: THE OLD BUSHING REMOVESDR DALA2024010500180Unknown · unknownSHIP 1705 WHEN PERFORM WORD CARD 5750-01118-1308, INSTALL THE TORQUE TUBE (P/N:113T2250-7) WITH THE SHEAR TUBE(P/N :113T2251-3), FOUND THE BUSHING(PN:113T2231-2) OF THE TORQUE TUBE(P/N:113T2250-7) INNER DIAMETER SMALL, THE SHEAR TUBE(P/N: 113T2251-3) CAN NOT ISDR DALA2024010500166Unknown · unknownSHIP 3123 CORROSION, RH WING INB FLAP TRACK 2 BEARING AT RIB 9 LEVEL OUTB PLATE. CORRECTIVE ACTION: REPAIRED PER ERA 609759-14. (0139951)SDR DALA2024010500165Unknown · unknownSHIP 3123 CORROSION, LH WING INB FLAP TRACK 2 BEARING AT RIB 9 LEVEL INB & OUTB PLATES. CORRECTIVE ACTION: REPAIRED PER ERA 609798-14. (0139866)SDR ASAA2024010348679Skin · corrodedLESSOR ITEM 38; (74009) R/H INNER FLAP UPPER SURFACE I/B SURFACE CORROSION GROUNDED - YES. REMOVED CORROSION ORIG .023 MATERIAL LOSS .004 REMAINING .019 HFEC AND DVI NO DEFECTS NOTED, REMOVED AND REINSTALLED FASTENERS FOUND TO BE WITHIN LIMITS, RESTORED COATINSDR ASAA2024010348175Skin · dentedDENT/NICK ON RH OUTBOARD FLAP LOWER SKIN TRAILING EDGE OVER INBOARD FLAP TRACK FAIRING GROUNDED - YES. CLEANED AREA AND EVALUATED DENT IAW-A320-SRM-57-53-00-283-092 FIG 1 AND FOUND TO BE WITHIN LIMITS PER L= .375" D= .0025 PERFORMED HFEC IAW-A320-NTM-51-10-08SDR IPXA2024021663705Skin · dentedWING LEFT I/B FWD FLAP EXTERNAL SURFACE HAS SOME DENTS.DOT119-001 EVALUATED DENT'S AT WING LEFT I/B FWD FLAP EXTERNAL SURFACE IAW SRM 57-53-01-1A-1 DETAIL VII / ALL DENT'S FOUND TO BE IN LIMITS. T96232, T97504. C/W. EXTERNAL FLAP UPPER PANEL WAS REPAIRED ON FASDR IPXA2024010463705Unknown · unknownWING LEFT I/B FWD FLAP EXTERNAL SURFACE HAS SOME DENTS.DOT119-001 APPROVED.SDR FDEA202401030012Unknown · unknownLH WING CENTER FLAP RIB UPR FLANGE FOUND CRACKS AT RIB17 BETWEEN STGR2.8 AND REAR SPARSDR FDEA202401030011Rib · crackedLH WING CENTER FLAP RIB UPR FLANGE FOUND 1EA CRACK AT RIB11 BETWEEN STGR2.8 AND REAR SPAR COMPLIED WITH EA 6-5750-T0377620 P1 REPAIRED THE LH WING CENTER FLAP CRACKED RIB UPR FLANGE AT RIB11 BETWEEN STGR2.8 AND REAR SPAR. TITLE: WING - FLIGHT SURFACES - LHSDR FDEA202401030010Flap · crackedRH WING CENTER FLAP RIB UPR FLANGE FOUND 3EA CRACKS AT RIB12 STGR2.5-STGR2.7 AND RIB11 STGR2.7-STGR2.8 REPAIRED THE RH WING CENTER FLAP RIB CRACKED UPPER FLANGE AT RIB12 STGR2.5-STGR2.7 AND RIB11 STGR2.7-STGR2.8 PER A300-600F SRM57-50-00-201 PARA.4.A FIG.2SDR FDEA202401030009Flap · crackedRH WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB15 BETWEEN STGR2.5 AND STGR2.6 REPAIRED THE RH WING CENTER FLAP RIB CRACKED UPPER FLANGE AT RIB15 BETWEEN STGR2.5 AND STGR2.6 PER A300-600F SRM57-50-00-201 PARA.4.A FIG.201 AND REPAIRED THE RH WISDR AALA202402294846Skin · debondedAIRCRAFT WAS NOT GROUNDED: DEBONDED UPPER SURFACE OUTBOARD FLAP LOCATED ON LEFT HAND WING AT 163.15 INCHES FROM INBOARD EDGE AND 2.5 INCHES FROM TRAILING EDGE. REPAIRED UPPER SURFACE OUTBOARD FLAP ON LEFT HAND WING PER EA 350937.SDR IPXA2024012439367Fairing · crackedFAULT - CRACK FAIRING, LH WING NO.3 FLAP TRACK AFT FAIRING INBD LE (REPAIR) REVIEW COMPLETESDR DALA2024010300085Unknown · unknownSHIP 3120 CORROSION OUTBD FLAP TRACK #3 INNER & OUTER RIB 5 AT ECCENTRIC BEARING. CORRECTIVE ACTION: REPAIRED PER ERA 614191-14. (0136639)SDR IPXA2024010239367Unknown · unknownCRACK FAIRING, LH WING NO.3 FLAP TRACK AFT FAIRING INBD LE (REPAIR) OK TO WORK. OPENSDR IPXA2023123129322Unknown · unknownDENT ON LEFT INBD FLAP LEADING EDGE. SEE BARCODE[T3F18E0033BK4] FOR ORIGINAL WRITE UP AND DEFERRAL. THIS ITEM WAS CLOSED IN ERROR. SEE ORIGINAL WRITE UP DENT ON LEFT INBD FLAP LEADING EDGE. SEE BARCODE[T3F18E0033BK4]. THE REPAIR HAS BEEN UPGRADED TO CATEGORSDR UIEA2023122701025Unknown · unknownLEFT WING, OUTBOARD TE FLAP, UPPER SURFACE, SEVERAL DENTS BTWN WS 616.2 AND WS 668.2 TO 31" TE.(<P>LEFT WING, OUTBOARD TE FLAP, ACCESS PANEL 566 KT, UPPER SURFACE WAS REPAIRED IAW SRM 57-53-01-2R-1 REP 1 FIG 201 SHEET 3 PAGE 1-7 AND SRM 51-70-10-2R-4 REP 4 FIGSDR UIEA2023122701019Unknown · unknownRH WING INBOARD MAIN FLAP L/E HOLE (FROM 26 IN RH EDGE)(<P>RH WING INBOARD MAIN FLAP, AFT FLAP WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG 201 SHEET 5 PAGE 2-3, 6 AND SRM 51-70-17-0G-0 PAR 4 B FIG 24 PAGE 14, 55 REV.124 DEC 15/2023</P>)SDR UIEA2023122401012Unknown · unknownDENT ON LH WING INBD AFT FLAP LOWER SKIN AT 11.50" FROM OUTBD EDGE AND 2.5" FROM AFT EDGE(<P>PART WAS REPAIRED IAW SRM 57-53-01-2R-1. NO FURTHER DEFECTS NOTED</P>)SDR SWIA2024010200030Unknown · dentedFOUND DENT ON THE LEADING EDGE OF THE FLAP-VANE ON THE LEFT OB FLAP AT APPROX. F/STA 210.50 (FILED CLSOED) FOUND DENT AT LEFT WING O/B FLAP VANE F.S. 210.50 TO BE OUT OF LIMITS PER SRM 57-53-00 FIG 102 SHEET 3. NO DENTS PERMITTED. REF CP 27621022 FOR FURTHER SDR SWAA2024011536217Intercostal · crackedUPPER TRAILING EDGE PANEL SUPPORT INTERCOSTAL INBOARD OF R/H DEFLECTION RIB IS CRACKED AT UPPER FLANGE.<[01] REMOVED AND REPLACED UPPER TRAILING EDGE PANEL SUPPORT INTERCOSTAL INBOARD OF R/H DEFLECTION RIB PER SRM 51-40-02;[02] C/W INSP.;[03] C/W INSP.SDR SWAA2024010436343Flap · debondedRIGHT WING AFT FLAP INBOARD LOWER SIDE HAS A REPAIR AND THE METAL BOND OF THE REPAIR IS DISBONDED; AND THE TOP HAS A DELAMINATED ON THE OPPOSITE SIDE.<[01] REMOVED AND REPLACED RH OTBD AFT FLAP. IAW AMM 27-51-22 STEP A-F;[02] VERIFIED THE REMOVAL AND REPLACEMESDR DALA2023122910707Unknown · unknownSHIP 3120 CORROSION BONDING PLATE FLAP TRACK FAIRING 4 (533CB) ON LH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 613776-14. (0129651)SDR DALA2023122810694Unknown · unknownDENTS (8 LOCATIONS) ON UPPER SKIN OF AFT MOVABLE VANE BTW STA XRS=77 TO XRS=88 AT RH WING. SUMMARY OF NRC 00077: AFT MOVABLE VANE BTW STA XRS=77 TO XRS=88 OF RH WING WAS REPAIRED PER ER/A 614501-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-6SDR 2023F00354Flap · damagedON A REPOSITION FLIGHT FROM KHYA TO KBED TO PICK UP PASSENGER. FLIGHT WAS OPERATED UNDER PART 91, NON-REVENUE AND NO PASSENGER. WEATHER AND VISIBILITY REPORTED BY KBED’S TOWER AT MINIMUMS. CREWS PROCEEDED WITH FINAL APPROACH AND LANDED. DURING LANDING ROLLOUT,SDR DALA2023122810669Unknown · unknownSHIP 1603 RHW O/B FLAP LOWER SURFACE DELAMINATION FROM AFT EDGE 27 INCH AND I/B EDGE 54 INCH. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER SRM 55-30-01-2R-1 & SRM 51- 70-10-2R-4 & SRM 51-70-10-2R-0 (0125192)SDR ASAA2023122447377Skin · dentedLESSOR ITEM A215: RH WING, INBOARD FLAP LOWER SKIN WITH SEVERAL DENTS LOCATED BEHIND #4 WHEEL AREA GROUNDED - YES. REPAIRED DENTS ON RH WING IB FLAP TE WEDGE LOWER SKIN BEHIND #4 WHEEL AREA IAW A320-200 SRM 57-52-00-300-091.THIS IS A CATEGORY A PERMENT REPAIRSDR ASAA2023122447376Skin · dentedLESSOR ITEM A214: RH WING, INBOARD FLAP LOWER SKIN WITH PREVIOUS REPAIR BEHIND #4 WHEEL AREA GROUNDED - YES. REPAIRED DENTS ON RH WING I/B FLAP TE WEDGE LOWER SKIN BEHIND #4 WHEEL AREA IAW A320-200 SRM 57-52-00-300-091.THIS IS A CATEGORY A PERMENANT REPAIR RHSDR ASAA2023122447375Skin · dentedLESSOR ITEM A211: RH WING, INBOARD FLAP LOWER SKIN WITH SEVERAL DENTS LOCATED BEHIND WHEEL #3 AREA. GROUNDED - YES. REPAIRED DENTS ON RH WING IB FLAP TE WEDGE LOWER SKIN AFT OF #3 WHEEL IAW A320-200 SRM 57-52-00-300-091.THIS IS A CATEGORY A PERMENANT REPAIR.FSDR SWAA2024020534383Fitting · damagedR/W REAR SPAR T/E LOWER WIGGLE FITTING HAS SHEARED RIVETS AND ELONGATED HOLE O/B OF FLAP TRACK # 6 MKD DOT<[01] REMOVED AND REPLACED WIGGLE FITTING AT R/W REAR SPAR T/E LOWER SRM 51-40-92-0G-0 AND DWM 115A2781;[02] VERIFIED CORRECTIVE ACTION.SDR AALA202403226697Flap · crackedAIRCRAFT IN BASE MAINTENANCE: RIGHT WING TRAILING EDGE OUTBOARD FLAP CRACKED BETWEEN RIBS 9 AND 10. REPAIRED FLAP PER SRM 57-53-00-300-029.SDR SWAA2024011734157Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE ORSS 261 AT RT WING 2023-761733<[01] REPLACED CORRUGATED PLATE(PLATE ASSY - WIGGLE) LOC. TRAILING EDGE ORSS 261 AT RT WING ;MEASURE OF CRACK 2.354 INCHES;TOOL USED DIGITAL CALIPER P/N=500-196-30 S/N=0051665 DUE DATE= 27-AUGSDR SWAA2024011734158Angle · crackedCRACK ANGLE TRAILING EDGE LOCATED IRSS 141 RT WING 2023-761734<[01] DRILL NEW HOLES AND APPLY PROTECTIVE TREATMENT;[02] CORRECTED STEP 1; REPLACED ANGLE TRAILING EDGE LOCATED IRSS 141 RT WING IAW B737-700 SRM 51-40-02-0G-0 AND DWG 115A2000 REV A MEASURE OF CRASDR DALA2023122110453Unknown · unknownSHIP 3120 EXCESSIVE PLAY CRUISE ROLLER OB FLAP LOC INBOARD EDGE LH WING. CORRECTIVE ACTION: REPLACED CRUISE ROLLER OB FLAP ON LH WING AS PER AIRBUS CMM 57- 53-21. (0119007)SDR ASAA2023121948900Skin · damagedLESSOR ITEM A087:LH OUTER FLAP WITH PREVIOUS REPAIR ON THE TRAILING EDGE TO 16IN APPROX FROM THE OUTBOARD EDGE. PLEASE PROVIDE THE DOCUMENTATION GROUNDED - YES. REPAIR L/H OUTER FLAP ON THE T/E 16" FROM THE OUTBOARD EDGE. FINAL REPAIR MEASURMENT CUT OUT OF THESDR JJBA20240115014Unknown · unknownRH OB FLAP SHROUD I/B HINGE, LUG DAMAGED ON SHROUD. REPLACEDSDR SWAA2024011732923Bracket · crackedCRACK ON BRACKET LOCATED AT LEVEL ORSS 270 DEFLECTION CONTROL RIB AREA AT RT WING 2023-761641<[01] REPLACED BRACKET LOC. AT LEVEL ORSS 270 DEFLECTION CONTROL RIB AREA AT RT WING IAW B737-700 SRM 51-40-02-0G-0 AND DWG 115A2930 REV - MEASURE OF CRACK IS 0.653? TSDR SWAA2024011733021Angle · crackedCRACK ON ANGLE LOCATED AT LEVEL ORSS 277 DEFLECTION CONTROL RIB AREA AT LT WING 2023-761649<[01] REPLACED ANGLE LOCATED AT LEVEL ORSS 277 DEFLECTION CONTROL RIB AREA AT LT WING IAW B737-700 SRM 51-40-02 AND DRAWING MEASURE OF CRACK IS: L=1.735 TOOL USED CALIPESDR SWAA2024011632047Flap · debondedLT WING O/B AFT FLAP I/B END LOWER SKIN AT T/E IS DISBONDED.<[01] REMOVED AND REPLACED LT. WING O/B AFT FLAP IAW AMM 27-51-22-000-801 & AMM 27-51-22-400-801 STEPS 3F(4). TORQUES AND SAFETIES VERIFIED.<BR><BR>CAL TOOLING:<BR> ID DD<BR>ATS2327 10/2024<BR>E11413 SDR SWAA2024010831752Tab · crackedR/H WING T/E AT APROX ORSS 261 CANNON PLUG DISCONNECT BRACKET MOUNT WEB TAB CRACKED AT RIB . PICTURE ATTACHED INFO: PART REQUIRED IS MPN 287A9152-98. NOT IN MAINTENIX SUBMITTED PAR APP DCN-038641. BOB W. 33000<[01] REMOVED R/H WING T/E AT APROX ORSS 261 CANNONSDR SWAA2024010831750Tab · crackedR/H WING INBD FIXED T/E UPPER PANEL BULB SEAL WEB ATTACH TAB CRACKED AT DEFLECTION CONTROL RIB . PICTURE ATTACHED<[01] REMOVED AND REPLACED R/H WING INBD FIXED T/E UPPER PANEL WEB ATTACH TAB PER SRM 51-4-02.;[02] REMOVED AND REPLACED R/H WING INBD FIXED T/E UPSDR UIEA2023121200985Unknown · unknownLEFT WING, INBOARD FLAP MECHANISM SUPPORT STRUCTURE, AT FLAP SUPPORT ARM WITH WEAR.(<P>LEFTT WING, INBOARD FLAP MECHANISM SUPPORT STRUCTURE AT FLAP SUPPORT ARM WITH WEAR. WAS PERFORMED TRE6757227 ISSUED DATE NOV22, 2023. RDR NUMBER: CMA-TLS-23-0168-07B DATE 22SDR UIEA2023121200989Unknown · unknownRH WING INB AFT FLAP DENT(<P>RH WING INB AFT FLAP WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG.201 SHEET 4 PAG.2,5 AND SRM 51-70-10-2R-4 REPAIR 4 FIG.- 201 PAG.1-3,7 REV.123 AUG 15/2023</P>)SDR UIEA2023121200990Unknown · unknownLH WING INBOARD FWD FLAP UPPER SKIN HOLE AT 5 IN FROM T/E & APROX 53 IN FROM OUTER EDGE(<P>LH WING INBOARD FWD FLAP COVE PANEL UPPER SKIN WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG.201 SHEET 5 PAG.2-3,6 AND SRM 51-70-03-G-0 PAR.5.B FIG.15 PAG.11,- 40 REV.124 DEC 1SDR SWAA2023121531634Fairing · crackedL/H INBOARD FLAP #3 CANOE AFT FAIRING #542EB IS CRACKED BOTTOM CENTER 3.5X2.5<[01] REMOVE AND REPLACE L/H INBOARD FLAP #3 CANOE AFT FAIRING # 542EB REF AMM 27-51-18.
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