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 DALA2023101308427Unknown · unknownSHIP 3117 EXCESSIVE PLAY ECCENTRICAL BEARING ON TRACK 2 INBOARD FLAP RH WING. CORRECTIVE ACTION: REPLACED SPHERICAL BEARING ON TRACK 2 INBOARD FLAP RH WING AS PER A320 FAM AMM 57-52-21-000 -001-A AND AMM 57-52-21-400-001-A. (0014176)SDR SWAA2023101209918Flap · delaminatedRIGHT WING OTBD T/E FLAP DISBONDED AT INBD LOWER SKIN APROX 1.5 ' FROM INBD EDGE AND 1' FROM T/E. DELAMINATION MEASURES 14' IN LENGTH AND 10' IN WIDTH<[01] R&R RIGHT WING OTBD T/E FLAP IN REF WITH AMM 27-51-22. REQUIRES OPS CHECK;[02] PERFORMED OPS CHECK IAW ASDR FDEA202310111741Vane · failedR/H WING O/B FLAP I/B HINGE, AREA ABOVE FLAP, FLAP VANE BOTTOM SIDE HAS A DEEP GOUGE WITH SCREW IMBEDDED INSIDE SKIN. REPAIRED R/H WING O/B FLAP I/B HINGE, AREA ABOVE FLAP, FLAP VANE BOTTOM SIDE GOUGE PER SRM 57-50-80-2R, PG.25-26, REPAIR INSTRUTION 4, FIGSDR A6WA202310108669Skin · dentedDENT ON THE R/H INBD UPPER SURFACE INBD END. DENT ON R/H INBD FLAP UPPER SKIN WS 50.489+13. L=5.200Ï¿½ X W=0.400Ï¿½ X D=0.008Ï¿½ FOUND TO BE OUT OF LIMITS IAW SRM 57-52-00 REV 39. AIRCRAFT REMOVED FROM SERVICE. PERFORMED HFEC WITH NO INDICATIONS. VERIFIED NSDR AALA202310130993Flaperon · out of toleranceAIRCRAFT IN BASE MAINTENANCE: ELONGATED HOLE IN RIGHT WING TRAILING EDGE AREA FORWARD POSITION ON FLAPERON. REPAIRED FLAPERON PER SRM 51-70-04-2R PROCEDURE 10 REPAIR 10.SDR AALA202310120333Flap · debondedAIRCRAFT IN BASE MAINTENANCE: DISBONDED AREA ON TRAILING EDGE 2 UPPER AND LOWER SKIN OF LEFT-HAND OUTBOARD FLAP BETWEEN WS 7316 TO WS 8268 AND BETWEEN FLAP RIB 10 AND FLAP RIB 11. REPAIRED FLAP PER EA 347143.SDR AALA202312150980Doubler · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING OUTBOARD TRAILING EDGE FLAP EXTERNAL DOUBLER AT FLAP TRACK #4. REPLACED DOUBLER PER SRM 57-53-21-300-003.SDR SWAA2023111309108Panel · delaminatedLOWER FUS PANEL 194D DELAMINATED @ FASTENERS HOLES MKD DOTS<[01] INSTALLED A PERMANENT REPAIR ON DAMAGE FASTENER HOLES AT LOWER FUSE FAIRING PANEL 193D AS PER B737 SRM 57-53-70-2R-3; SRM 51-70-04-2R-9 PAR 4(D-N) AND 51-70-04-2R-0 PAR 4(E-N). TEMPERATURE CONTROSDR FDEA202310091733Flap · damagedLH IB AFT FLAP I/B LWR SURFACE FROM IB TO OB 65INCH CROSS LE TO TE 34INCH FOUND ONE BIRD STRIKE. EVALUATED LH IB AFT FLAP I/B LWR SURFACE FROM IB TO OB 65INCH CROSS LE TO TE 34INCH ONE BIRD STRIKE, DAMAGE SIZE L*W=1" *0.75" WITHIN REPAIR LIMIT AS PER B777SDR FDEA202310081728Flap · damagedLH OB FLAP LWR SURFACE FROM IB TO OB 52 INCH CROSS LE TO TE 67 INCH FOUND ONE BIRD STRIKE. EVALUATED LH OB FLAP LWR SURFACE FROM IB TO OB 52 INCH CROSS LE TO TE 67 INCH ONE BIRD STRIKE. DAMAGE SIZE L*W=1" *0.8" WITHIN REPAIR LIMIT AS PER B777 SRM 57-53-01-SDR IPXA2023101060108Flap System · warning message"FLAP ASYM" LIGHT AND EICAS MSG DURING CLIMB OUT SENSOR 279, TARGET CLEARANCE ADJUSTED, AMM SUBTASK 27-88-01-822-160, REV NO. / DATE : 140 / 11 SEP 2023, OUTBOARD AND INBOARD SLAT AUXILIARY TRACK ROLLERS AND SIDE BRACE LINKS LUBRICATED, REFERENCE: AMM TASK 12-SDR IPXA2023100964157Unknown · unknownL/H NOTCH FLAP FRAME CRACKED REMOVED NOTCH FLAP UP TO AND INCLUDING AMM 27-87-13 PAGEBLOCK 0401 STEP B.(10). ROUTED TO SHEET METAL FOR DRILLING OF NEW NOTCH FLAP. QC MATCH DRILLED NEW PART IAW A300 SRM 51-00-00. FAILED NOTCH FLAP HANGER INSPECTION DURING RII SDR VNAA202311280009Skin · nickedPERM REPAIR BEFORE 20,505.22 FH - RH IB FLAP WITHIN 1458.07 FHS FROM IR (BEFORE 20,505.22 FH), REPAIR, OR REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES. RH INBOARD LOWER SKIN WAS REPAIRED PER CRJ-900 SRM 57-52-01-201-005-A01 IN REFERENCE SDR VNAA202311280004Skin · nickedSEVERAL NICKS AND DENTS ON LOWER SKIN OF RH INBOARD FLAP FLS 15.00 TO FLS 65.5. SEVERAL NICKS ON LOWER SKIN OF RH INBOARD FLAP FLS 15.00 TO FLS 65.5 WERE REMOVED PER CRJ900 SRM 51-12-00-001-001-A01; WERE EVALUATED WITHIN LIMITS BTW FLS 45 TO FLS 65.5 AND WERSDR DALA2023100908289Unknown · unknownSHIP 3117 LH WING OUTBOARD FLAP AT FLAP TRACK #3 LEVEL INNER AND OUTER RIB 5 AT ECCENTRIC BEARING CORROSION. CORRECTIVE ACTION: REPAIRED PER ERA 611685. (0004590)SDR DALA2023100908288Unknown · unknownSHIP 3117 LH WING OUTB FLAP PENDULUM ASSY AT TRACK #4 LEVEL CORROSION. CORRECTIVE ACTION: REPAIRED PER ERA 611589-14. (0004485)SDR SWAA2023100908178Tail Cone · delaminatedLEFT WING #3 FLAP FAIRING TAIL CONE DELAMINATED.<[01] REMOVED AND REPLACED LH WING #3 FLAP FAIRING TAIL CONE PER SRM 51-40-02SDR SWAA2023110808099Flap · debondedCUSTOMER REQUEST - DEBONDED OB AFT FLAP LOWER SURFACE AT LT WING 2023-635173<[01] TOOL USED: CALIPER P/N: 500-464 S/N: B17030933 DUE DATE: 17-OCT-23.;[02] TOOL USED: ULTRASONIC EQUIPMENT; P/N: BONDMASTER 600M; S/N: 220052310; DUE DATE: 31 OCT 23.;[03] TOOL USESDR DALA2023100908287Unknown · unknownSHIP 3126 LH OUTBOARD FLAP / FLAP TRACK 3 / BORE CORROSION. CORRECTIVE ACTION: REPAIRED PER ERA 607038-14. (0002787)SDR CALA2023101803109Skin · damagedR/WING O/B FLAP TAILING EDGE, INBD OF FAIRING 632BB HAS SKIN THAT IS SEPERATED DOT 202-200 REPAIRED R/WING O/B FLAP T/E DAMAGED AREA 3.5"X 3.5" DISBOND IAW SRM 57-53-00-300-120 AND SRM 51-77-11-911-023 STA:ST ENGINEERIN G BFMSDR SWAA2023110306973Skin · delaminatedL/H WING OUTBOARD AFT FLAP IS DELAMINATED AT THE INBOARD LOWER SURFACE AT PREVIOUS SPLICE REPAIR.<[01] REMOVED; AND REPLACED L/H O/B AFT FLAP IAW AMM 27-51-22.;[02] RII INSPECTION C/W FOR WORK PERFORMED IN CORRECTIVE ACTION 1 AND ALL STEPS PER AMM 27-51-22.SDR DALA2023100408172Unknown · unknownSHIP 3117 CORROSION INB FLAP TRACK 2 BEARING AT RIB 9 LEVEL. CORRECTIVE ACTION: REPAIRED PER ERA 612080-14. (2999351)SDR FDEA202310031694Bracket · corrodedRIGHT WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORRODED REWORKED AND FOUND WITHIN LIMIT IAW CMM 57-44-07.OVERSIZED REPAIR BUSHING FABRICATED BY MACHINING AND INSTALLED IAW CMM 57-44-07 AND EA 1-5750-T0331808 A PART 2 STEP SDR FDEA202310031693Bracket · corrodedRIGHT WING WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. RIGHT WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT IAW CMM 57-44-07.OVERSIZED REPAIR BUSHING FASDR FDEA202310031692Bracket · corrodedLEFT WING WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. LEFT WING WING SIDE INBOARD FLAP OUTBOARD HINGE OUTBOARD ACTUATOR LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT IAW CMM 57-44-07. OVERSIZED REPAIR BUSDR FDEA202310031691Bracket · corrodedLEFT WING WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE FOUND CORROSION. LEFT WING WING SIDE INBOARD FLAP OUTBOARD HINGE INBOARD ACTUATOR LUG HOLE BORE (#4 HOLE) REWORKED AND FOUND WITHIN LIMIT IAW CMM 57-44-07.OVERSIZED REPAIR BUSHSDR ASAA2023100246293Skin · debondedLEFT WING I/B FLAP UPPER SURFACE T/E HAS MULTIPLE CORROSION GROUNDED - YES. ACCOMPLISHED PERMANENT CAT A REPAIR TO LEFT WING I/B FLAP T/E PROFILE IAW ASA EA # CMPT-57EA-01966 REV 00 DAMAGE AND REPAIR DIMENSIONS LOCATED IN WORK STEPS ON STEP 007, 009011 A/C : NSDR FDEA202310021685Flap · dentedLH WING OB FLAP LOWER SURFACE FROM OB TO IB 210 INCH CROSS TE TO LE 13 INCH FOUND ONE DENT. EVALUATED LH WING OB FLAP LOWER SURFACE FROM OB TO IB 210 INCH CROSS TE TO LE 13 INCH ONE DENT DAMAGE SIZE LXW=1.5"X1.5" OUT OF ALLOWABLE LIMIT AS PER B777 SRM 57-5SDR FDEA202310021682Flap · corrodedLH WING O/B FLAP O/B END T/E SKIN CORRODED AND DISCHARGER FITTING FOUND BROKEN REPAIRED THE CORRODED SKIN AT LH WING O/B FLAP O/B END T/E PER EA:6-5750-T0376427 P1. TITLE: WINGS - FLIGHT SURFACES - LH O/B FLAP, OUTER TRAILING EDGE, UPPER SKIN CORROSION USDR SWAA2023111005983Fairing · delaminatedL/W FLAP TRACK NO -3 AFT CONE FAIRING 542EB O/B SIDE SKIN APPEARS 5 INC. DELAMINATION MKD DOT<[01] APPLIED REPAIR AT L/W FLAP TRACK NO -3 AFT CONE FAIRING 542EB PER<BR>B737 SRM 57-53-70-2R-4 ; B737 SRM 51-70-04-2R-1 AND B737 SRM 51-70-04-0 PARAGRAPH 4.EQUIPMENSDR IPXA2023101728006Flap · unknownTHE L/H WING CENTER FLAP HAS A CRACK (1EA) ON RIB FLANGE #11, AREA MARKED IN RED NR 298439 ACCOMPLISHED WORK PERMANENT PER PRELIMINARY EA 300-5750-27-A3373 REV AND UPS E0:E0-88449-REQ1. REVIEWEDSDR IPXA2023101727870Flap · unknownTHE L/H WING CENTER FLAP HAS A CRACK (1EA) ON RIB FLANGE #26 FWD SIDE, AREA MARKED IN RED NR 298446 ACCOMPLISHED WORK PERMANENT PER PRELIMINARY EA 300-5750-27-A3373 REV AND UPS E0:E0-88449-REQ1. REVIEWEDSDR IPXA2023101727655Flap · unknownTHE L/H WING CENTER FLAP HAS MULTIPLE CRACKS (2EA) ON RIB FLANGE #26, AREA MARKED IN RED NR 298444 ACCOMPLISHED WORK PERMANENT PER PRELIMINARY EA 300-5750-27-A3373 REV AND UPS E0:E0-88449-REQ1 REVIEWED.SDR IPXA2023101727615Flap · unknownTHE L/H WING CENTER FLAP HAS A CRACK (1EA) ON RIB FLANGE #18 AREA MARKED IN RED NR 298443 ACCOMPLISHED WORK PERMANENT PER PRELIMINARY EA 300-5750-27-A3373 REV AND UPS E0:E0-88449-REQ1 REVIEWEDSDR IPXA2023101727576Flap · unknownTHE L/H WING CENTER FLAP HAS CRACK (1EA) 0N RIB FLANGE #12, AREA MARKED IN RED NR 298441 ACCOMPLISHED WORK PERMANENT PER PRELIMINARY 1 EA 300-5750-27-A3373 REV AND UPS E0:E0-88449-REQ1. REVIEWEDSDR IPXA2023101727963Unknown · unknownTHE L/H CENTER FLAP HAS A CRACK (1EA) ON RIB FLANGE #27, AREA MARKED IN RED NR 298447 ACCOMPLISHED WORK PERMANENT PER PRELIMINARY EA 300-5750-27-A3373 REV AND UPS E0:E0-88449-REQ1. REVIEWEDSDR IPXA2023101727788Flap · unknownR/H WING CENTER FLAP HAS A CRACK (1 EA) ON RIB FLANGE #19, AREA MARKET IN RED (CARD NO. 298435) ACCOMPLISHED PERMANET REPAIR WORK PER UPS EO: EO-88450-REQ1 AND VTMAE FINAL EA 300-5750-27-A3372 REV-. REVIEWEDSDR IPXA2023101727965Flap · unknownTHE R/H WING CENTER FLAP HAS A CRACK (1 EA) ON RIB FLANGE #12, AREA MARKED IN RED (CARD NO. 298439) ACCOMPLISHED PERMANET REPAIR WORK PER UPS EO: EO-88450-REQ1 AND VTMAE FINAL EA 300-5750-27-A3372 REV-. REVIEWEDSDR IPXA2023101727881Flap · unknownTHE R/H WING FLAP, HAS A CRACK (1 EA) ON RIB FLANGE #11, AREA MARKED IN RED (CARD NO. 298432) ACCOMPLISHED PERMANET REPAIR WORK PER UPS EO: EO-88450-REQ1 AND VTMAE FINAL EA 300-5750-27-A3372 REV-. REVIEWEDSDR IPXA2023101727847Flap · unknownTHE RH CENTER FLAP HAS MULTIPLE CRACKS (2EA) ON RIB FLANGE #25, AREA MARKED IN RED NR 298436 ACCOMPLISHED PERMANET REPAIR WORK PER UPS EO: EO-88450-REQ1 AND VTMAE FINAL EA 300-5750-27-A3372 REV-. REVIEWEDSDR IPXA2023101627709Flap · unknownTHE R/H WING CENTER FLAP HAS A CRACK (1 EA) ON RIB FLANGE #27, AREA MARKED IN RED (CARD NO. 298438) ACCOMPLISHED PERMANET REPAIR WORK PER UPS EO: EO-88450-REQ1 AND VTMAE FINAL EA 300-5750-27-A3372 REV-. REVIEWED.SDR IPXA2023093011200Flap · gougedABSORB FOUND L/H WING I/B FLAP I/B ATTACHMENT MOUNT UPPER BOLT HOLE CUT-OUT IS GOUGED, DURING IN-PROCESS INSTALL VERIFIED STEP 1 AND 2SDR VNAA20231120006Skin · damagedNICKS AND DENTS ON LOWER SKIN OF LH INBOARD FLAP BTW FLS 15.00 TO FLS 65.5. FLAP WAS REMOVED PER CRJ900 SRM 51-12-00-001-001-A01 AND WAS EVALUATED AS FOLLOWS: BTW FLS 45 TO FLS 65.5 WAS FOUND WITHIN LIMITS AND BTW FLS 15 TO FLS 45 WAS FOUND OUT OF LIMITS PERSDR SWAA2023101905617Flap · delaminatedRIGHT WING O/B AFT FLAP LOWER SURFACE AT I/B CORNER. DELAM APPROX 4'X5'<[01] R/W O/B AFT REPLACED ON FAULT #TTG8Q00NQHUR;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLESDR IPXA2023101094827Unknown · unknownDURING WALK AROUND FOUND PUNCTURE IN LEFT INBOARD FLAP INSTALLED FLAP VANE TRACKS WITH FLAP VANE INSTALLED. REF AMM 27-50-24. VERIFIED FINAL INSTALLATION STEPS, SEE BARCODE #T3F18E0033F5E.SDR SWAA2023102305599Flap · crackedFOUND DENT WITH A CRACK OUT OF LIMITS ON UPPER SURFACE L/H WING I/B AFT FLAP AT 21.5' I/B EDGE AND 12.5' T/E; LENGTH OF DENT CRACK = 1'.<[01] APPLIED REPAIR AT UPPER SURFACE L/H WING I/B AFT FLAP PER B737 SRM<BR> 57-53-01-2R-4; SRM 51-70-10-2R-4 AND SRM 51-70-SDR DALA2023100308106Unknown · unknownSHIP 3168 CORROSION INTERCONNECTING STRUT IB FLAP ASSY. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT I/B FLAP ASSY RH WING AS PER A320 FAM AMM 27-51-44-000-001-A AND AMM 21-51-44-400-001-A. (2990699)SDR DALA2023100308105Unknown · unknownSHIP 3168 CORROSION INTERCONNECTING STRUT OB FLAP ASSY. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT O/B FLAP ASSY LH WING AS PER A320 FAM AMM 27-51-44-000-001-A AND AMM 21-51-44-400-001-A. (2990691)SDR DALA2023101608509Unknown · unknownSHIP 3129 CORROSION INTERCONNECTING STRUT IB FLAP ON LH WING. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT ON LH WING AS PER A320 FAM AMM 27 -51-44-000-001-A, A320 FAM AMM 27-51-44-400-001-A. (2989875)SDR DALA2023092807978Unknown · unknownSHIP 3129 CORROSION INTERCONNECTING STRUT IB FLAP ON RH WING. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT IB FLAP ON RH WING AS PER AMDS CARD 2750-1010-RT AND AMDS CARD 2750-6010-RT. (2989867)
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