JASC 5753
Service difficulty reports · 31,515
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 UPS08M53500Hinge · corrodedINSPECTION TYPE:N/A RT WING O/B FLAP O/B FWD HINGE LOWER MOUNT O/B BORE FWD & AFT SPOTFACE CORRODED. RT WING O/B FLAP O/B FWD HINGE LOWER MOUNT O/B BORE FWD & AFT SPOT FACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-09.SDR UPS08M53499Hinge · corrodedINSPECTION TYPE:N/A LT WING O/B FLAP O/B FWD HINGE LOWER MOUNT O/B BORE CORRODED. LT WING O/B FLAP O/B FWD HINGE LOWER MOUNT O/B BORE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-09.SDR UPS08M53498Hinge · corrodedINSPECTION TYPE:N/A LT WING O/B FLAP O/B FWD HINGE BARREL NUT LOWER BORE CORRODED. LT WING O/B FLAP O/B FWD HINGE BARREL NUT LOWER BORE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-09.SDR UPS08M53497Hinge · corrodedINSPECTION TYPE:N/A LT WING O/B FLAP O/B FWD HINGE UPPER MOUNT I/B BORE FWD SPOTFACE CORROSION. LT WING O/B FLAP O/B FWD HINGE UPPER MOUNT I/B BORE FWD SPOTFACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-09.SDR UPS08M53496Hinge · corrodedINSPECTION TYPE:N/A LT WING O/B FLAP O/B FWD HINGE LOWER MOUNT I/B BORE FWD & AFT SPOTFACE CORRODED. LT WING O/B FLAP O/B FWD HINGE LOWER MOUNT I/B BORE FWD & AFT SPOTFACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-09.SDR UPS08M53495Hinge · corrodedINSPECTION TYPE:N/A LT WING O/B FLAP O/B FWD HINGE BARREL NUT UPPER BORE CORRODED. LT WING O/B FLAP O/B FWD HINGE BARREL NUT UPPER BORE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-09.SDR UPS08M53490Hinge · corrodedINSPECTION TYPE:N/A LT WING O/B FLAP I/B FWD HINGE UPPER MOUNT O/B BORE FWD & AFT SPOT FACE CORRODED. LT WING O/B FLAP I/B FWD HINGE UPPER MOUNT O/B BORE FWD & AFT SPOT FACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08.SDR UPS08M53489Hinge · corrodedINSPECTION TYPE:N/A LT WING O/B FLAP I/B FWD HINGE LOWER MOUNT O/B BORE CORRODED. LT WING O/B FLAP I/B FWD HINGE LOWER MOUNT O/B BORE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08.SDR UPS08M53488Hinge · corrodedINSPECTION TYPE:N/A LT WING O/B FLAP I/B FWD HINGE LOWER MOUNT O/B BORE FWD & AFT SPOT FACE CORRODED. LT WING O/B FLAP I/B FWD HINGE LOWER MOUNT O/B BORE SPOTFACE CORROSION REMOVED AS PER CMM 57-44-08 AND FOUND WITHIN DWG ARC0502 LIMIT. REPAIR CARRIED OUT ASSDR UPS08M53487Hinge · corrodedINSPECTION TYPE:N/A LT WING O/B FLAP I/B FWD HINGE BARREL NUT UPPER BORE CORRODED. LT WING O/B FLAP I/B FWD HINGE BARREL NUT UPPER BORE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08.SDR UPS08M53486Hinge · corrodedINSPECTION TYPE:N/A LT WING O/B FLAP I/B FWD HINGE BARREL NUT LOWER BORE CORRODED. LT WING O/B FLAP I/B FWD HINGE BARREL NUT LOWER BORE CORROSION REMOVED AND REPAIRED AS PER CMM 57-44-08.SDR SWAA084539Skin · delaminatedDURING SCHEDULED SPV CHECK, FOUND LT WING FORE FLAP UPPER SKIN DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM.SDR UPS08M53494Hinge · corrodedINSPECTION TYPE:N/A LT WING O/B FLAP I/B AFT HINGE I/B PIVOT I/B SPOTFACE CORRODED. LT WING O/B FLAP I/B AFT HINGE I/B PIVOT SPOTFACE CORROSION REMOVED AND REPAIRED AS PER CMM 57-52-04.SDR UPS08M53493Hinge · corrodedINSPECTION TYPE:N/A RT WING O/B FLAP AFT HINGE O/B PIVOT BORE CORRODED. RT WING O/B FLAP O/B AFT HINGE O/B PIVOT BORE CORROSION REMOVED AND REPAIR CARRIED OUT AS PER CMM 57-52-04.SDR UPS08M53492Hinge · corrodedINSPECTION TYPE:N/A RT WING O/B FLAP O/B AFT HINGE I/B PIVOT I/B SPOTFACE CORRODED. RT WING O/B FLAP O/B AFT HINGE I/B PIVOT I/B SPOTFACE CORROSION REMOVED AND REPAIR CARRIED OUT AS PER CMM 57-52-04.SDR UPS08M53491Hinge · corrodedINSPECTION TYPE:N/A RT WING O/B FLAP O/B AFT HINGE UPPER MOUNTING CENTER BORE CORRODED. RT WING O/B FLAP O/B AFT HINGE UPPER MOUNTING CENTER BORE CORROSION REMOVED AS PER BSOPM 20-11-02 AND FOUND WITHIN LIMIT AS PER DWG ARC1991.SDR 08FDEA03453Skin · damagedPREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON RT WING OUTBD FLAP LOWER MAIN SKIN AT MAIN SPAR TO REAR SPAR AND FROM THE INBD EDGE TO BETWEEN RIB 2 AND TRACK NR 3, MEASURING 47.7 IN BY 19.9 IN. REMOVED EXISTING REPAIR AND REPAIRED IAW SRM 57-53-12,FIG 210, PG 25SDR 08FDEA03451Fairing · crackedRT WING NR 6 FLAP TRANSMISSION FAIRING IS CRACKED AT CENTER ATTACH HOLE REMOVED FAIRING REF 51-30-2, PG 1-7 STOP DRILLED CRACKS REF 727 SRM 51-10-1 PG 13. NDT VERIFIED CRACK CONTAINMENT. NDT MANUAL PART 6, 51-00-00 FIG 23. ORIGINAL AND REPAIR MATERIAL IDENTSDR 08FDEA03449Fairing · crackedNR 5 FLAP TRACK MIDDLE FAIRING, AFT SKIN BENT/CRACKED. REMOVED DAMAGED SKIN, REF 51-30-2, PG 1-7. ORIGINAL SKIN AND REPLACEMENT BOTH IDENTIFIED AS 7075-T6, .040 REF 65-21795, REV E, PG 35 AND DWG 65-21795, AND A-TAG NR A27927. FABRICATED NEW SKIN, REF SRM 5SDR 08FDEA03440Skin · chafedFOUND CHAFING MARKS ON LT INBOARD FLAP, RIB 11-12, TOP SKIN REPAIR PERFORMED BY BLEND OUT THE CHAFING MARKS, NDT FOR CRACK FREE CONDITION IAW RAS/FOK/228/2008 ISS A, APRROVED BY EA 6-5752-123079.SDR UPS08553288Frame · chafedINSPECTION TYPE:C3 ACCESS PANEL 572HB FWD EDGE IS CHAFED. REMOVED AND REPLACED FRAME PER SRM 51-40-02.SDR UPS08553287Panel · gougedINSPECTION TYPE:C3 LEFT O/B FLAP L/E IS GOUGED AT O/B CARRIAGE. BLENDED GOUGE PER ATS ER08-2722 DATED 25AUG08.SDR 08FDEA03411Skin · chafedFOUND CHAFING MARKS ON LT CENTER FLAP UPPER SKIN AFT OF REPAIR SPAR, RIB 4-4A AND 15-16. REPAIR PERFORMED BY REWORK OF CHAFING MARKS AND INSTALLING A NEW CHAFING PLATE IAW RAS/197/2008 ISS A, APPROVED BY EA 6-5754-123032.SDR 08FDEA03410Skin · chafedFOUND CHAFING MARKS ON LT CENTER FLAP UPPER SKIN RIB 13-13A. REPAIR PERFORMED BY REWORK OF CHAFING MARKS AND INSTALLING A NEW CHAFING PLATE IAW, RAS/197/2008 ISS A, APPROVED BY EA 6-5753-123011.SDR 08FDEA03404Skin · gougedLEFT WING INBD FLAP T/E UPPER SURFACE EXTERNAL SKIN IS GOUGED IN TWO PLACES. BLENDED GOUGE SMOOTH IAW A300-600 SRM 51-73-10. GOUGED INBD FLAP UPPER SKIN FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 57-50-00; PG 108. FABBED REPAIR AND INSTALLED BOTH IAW A300-6SDR SWAA084563Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING OUTBOARD T/E AFT FLAP UPPER SURFACE DELAMINATED. R&R FLAP PER MM.SDR SWAA084562Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND RT WING FORE FLAP UPPER SURFACE DELAMINATED. R&R FLAP PER MM.SDR 08FDEA03395Rib · crackedRIGHT WING INBD FLAP NOSE RIB NR 9 IS CRACKED AT A RIVET HOLE. FABRICATED A REPAIR DOUBLER REF SRM 57-50-00; PG 204. ALODINED AND PRIMED REF AMM 51-22-00-0; PG 1. INSTALLED REF SRM 51-40-21; PG 7.SDR UPS08853130Skin · gougedINSPECTION TYPE:C1 2 EA GOUGES IN UPPER SKIN OF RT WING O/B FLAP, ON I/B & O/B SIDE OF FLAP STA 219. FABRICATED AND INSTALLED 2 EA REPAIR DOUBLERS IAW SRM 57-07-01 FIG 004, 57-02-00, AND 51-1-21A.SDR USAA920081603Skin · delaminatedMCN C19 MAJOR REPAIR NR 6126557 & 6126556 LT HAND INBOARD AFT FLAP DELAMINATED IN 2 PLACES. WBL117 ON LOWER SURFACE, AND WBL 107 ON UPPER SURFACE. REPAIRED LT HAND INBOARD AFT FLAP IN 2 PLACES. WBL 117 ON LOWER SURFACE, AND WBL 107 ON UPPER SURFACE IAW B737SDR 08FDEA03354Fairing · crackedLEFT WING INBD T/E LWR SURFACE, NR 3 FLAP TRACK FAIRING INBD ATTACH L- ANGLE CRACKED BETWEEN 2 FASTENERS, 12 INCHES FWD OF T/E PANELS AFT EDGE. REMOVED DAMAGED PORTION OF NR 3 FLAP TRACK FWD FAIRING INBD ATTACH L- ANGLE. FABRICATED FILLER AND DOUBLER, AND SDR CNMA20090030Structure · crackedRT OTBD FLAP INBD RIB CLOSURE HAS AN ANGULAR CRACK. REMOVED RT OTBD FLAP, INBD T/E SECTION. REMOVED ALL SCREWS SIZED IAW SRM 51-31-01 VOL 2 REV 93. REMOVED RT OTBD FLAP INBD SECTION T/E IAS MM 20-50-02 REV 81. FABRICATED PN ARC1951-6 IAW DWG ARC1951 AND INSSDR CNMA20090029Panel · crackedLT OTBD FLAP, OTBD HINGE PANEL 526JL, CRACKED. PERFORMED REPAIR IAW SRM 57-00-01, FIG 10.SDR CNMA20090025Panel · crackedLT WING OTBD FLAP INBD HINGE PANEL 535DL CRACKED. PERFORMED REPAIR IAW SRM 57-00-01, FIG 4, SH1, VOL I, REV 94.SDR CNMA20090027Panel · crackedLT OTBD FLAP, INBD HINGE PANEL 535JL CRACKED. REMOVED EXISTING REPAIR IAW SRM 51-31-01 VII PERFORMED WELD IAW DPS10225. REINSTALLED OLD REPAIR IAW SRM 51-35-02 VII 4REV 94.SDR CNMA20090026Panel · delaminatedLT INBD FLAP, OTBD HINGE, PANEL 541JL UNGLUED. PERFORMED REPAIR IAW DWG ARC 2541.SDR CNMA20090024Panel · crackedLT WING OTBD FLAP INBD HINGE PANEL 535DL CRACKED. PERFORMED REPAIR IAW SRM 57-00-01, FIG 4, SH1, VOL I, REV 94.SDR ASAA0843339Skin · dentedRT INBOARD FORE FLAP HAS MULTIPLE SMALL DENTS ON LOWER SURFACE ABOVE NR 3 & 4 TIRES 2 DENTS ON PREVIOUS REPAIRS. REMOVED DAMAGED AREA, FABBED FILLERS & DOUBLERS & BONDED REPAIRS IAW B737 400 SRM 51 70 10 REPAIR 4.SDR IXX2008F00116Skin · misrepairedDURING ROUTINE C-CHECK INSPECTION, FOUND RT OTBD FLAP EXHAUST GATE LOWER SKIN HAS IMPROPER REPAIR. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED TREATED AND PRIMED AREA AND REPAIR PART. INSTALLED NEW FSDR IXX2008F00112Skin · misrepairedDURING ROUTINE C-CHECK INSP, FOUND RT OTBD FLAP LOWER SKIN HAS IMPROPER REPAIR AT STA XF 238.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEWSDR 08FDEA03310Rib · damagedWHILE ACCOMPLISHING EO 6-5750-7-5000 PT 4 "WINGS - INBD FLAP, REPLACEMENT NOSE RIB 7 RT", STEP 10; THE ACCESS HOLE HAS BEEN PREVIOUSLY CUT AND IS 0.500" TOO LARGE. OMITTED FASTENERS AT EXTENDED CUT OUT; INSTALLED OVERSIZED FASTENERS AND PERFORMED SPAR REPAIRSDR 08FDEA03309Skin · damagedWHILE ACCOMPLISHING EO 6-5750-7-5000 PT 3 "WINGS INBD FLAP, REPLACEMENT NOSE RIB 7 LT, STEP 10; THE ACCESS HOLE HAS BEEN PREVIOUSLY CUT AND IS 0.500" TOO LARGE. FLAP WAS FOUND TO BE BEYOND TIMELY REPAIR. RECEIVED NEW FLAP REF TAG NR 6934A5. FOR INSTALLSDR 08FDEA03302Fairing · crackedLEFT WING INBD TE NR 3 FLAP TRANSMISSION JACKSCREW FAIRING ON O/B END OF MID FLAP IS CRACKED OUT OF FWD UPPER HOLE REMOVED FAIRING. NDT VERIFIED CRACK LOCATION. REMOVED DAMAGE AND INSTALLED REPAIR. REINSTALLED FAIRING TO MID FLAP REF SRM 51-30-2 PG 13/ NDT SDR 08FDEA03301Fairing · crackedLEFT WING OB TE NR 2 FLAP TRANSMISSION JACKSCREW FAIRING ON INBD END OF MID FLAP HAS CRACK IN SIDE WEB 19 INCH AFT OF FWD END REMOVED CRACKED WEB. FABRICATED NEW WEB, P/N 65-28131-1. TREATED, PRIMED, AND PAINTED WEB. INSTALLED WEB REF SRM 51-30-2 PG 2-4/SRMSDR UPS08M53459Wedge · delaminatedINSPECTION TYPE:C LT WING O/B FLAP T/E DELAMINATION. REPAIRED LT WING O/B FLAP T/E WEDGE PANEL DELAMINATED AREA AS PER EN1339-08 AND UPS EO MD11-5750-30265A.SDR 2008UALA04163Skin · delaminatedLEFT WING INBOARD MID FLAP HAS DELAM. ON TOP SIDE. DAMAGE AREA IS APPROX. 4" X 6" AND MARKED IN RED. *S/D* REMOVED LT INBOARD MID FLAP TRAILING EDGE PANEL FOR IN SHOP REPAIR DUE TO DELAMINATION. REPAIR ACP BY SHOP, INSTALLED PANEL AND CHECKED FIT AND FAIR.SDR CALA0800776Structure · deformedRIGHT WING OUTBOARD MID FLAP DAMAGED ON TRAILING EDGE. REPAIRED DAMAGED AREA RT WING O/B MID FLAP TRAILING EDGE WEDGE REF BOAC 737-300 SRM 51-70-10.SDR SWAA084387Skin · delaminatedDURING SCHEDULED HC2 CHECK, FOUND LT WING OUTBOARD T/E AFT FLAP OUTBOARD LOWER SURFACE DELAMINATED. REMOVED AND REPLACED FLAP PER MM.SDR IXX2008F00113Skin · misrepairedDURING ROUTINE C-CHECK INSP, FOUND LT OTBD FLAP UPPER SKIN HAS IMPROPER REPAIR AND AT STA XF420.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR, REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PSDR ASM2008F00002Fairing · puncturedDURING TRANSIT CHECK, MAINTENANCE PERSONNEL DETECTED A PUNCTURE OF 6"X7" IN THE LT INTERIOR FLAP FAIRING AT FWS LOWER AREA AND A CRACK OF 6 INCHES IN LATERAL SIDE WITH THE BRACKET LOOSENED. THE INTERIOR FLAP FAIRING WAS REPLACED IAW MM 27-61-18, TESTED CORREC
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