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 SWAA2025091715230Skin · delaminatedLEFT INBD MAIN FLAP OTBD OF NR 3 CANOE ON TRAILING EDGE OF FLAP; UPPER SIDE IS DELAMINATED. ACCOMPLISHED TAP TEST ON UPPER DISCREPANCY AREA; NO DELAM NOTED. FOUND DEFORMED AND WARPED ON UPPER SKIN FROM LOWER SKIN SEPARATION. APPLIED SPEED TAPE ON LT INBD SDR DALA2025091706835Skin · dentedRIGHT WING INBD AFT FLAP LOWER SURFACE AT 30" FROM OTBD FAIRING INBD SIDE FOUND DENTED. RT WING INBD AFT FLAP LOWER SURFACE AT 30" FROM OTBD FAIRING INBD SIDE DENT REPAIRED IAW SRM 51-70-10-2R-3, SRM 57- 53-01-2R-1, AND SRM 51-70-10-2R. (1201666)SDR SWIA202511240913Rib · wornRIGHT OTBD FLAP BUTE DOOR CAMS & RIB FITTINGS HAVE WEAR & ARE MUSHROOMED AT ALL 5 LOCATIONS. REPAIRED THE BUTE DOOR CAMS AND RIB FITTINGS, REPLACED OTBD MOST LOCATION IAW REO 670-57-53-008 REV -D, & DWG 601R14502, REV D, CHECKS GOOD. COMPLIED WITH SKYWEST SDR CALA2025091709001Flap · no discrepancyFLAP OVERSPEED AT FL10 BY 4 KNOTS. PERFORMED PHASE 1 INSPECTION IAW AMM 05-51-08-210-801. NO DEFECTS FOUND. OK FOR SERVICESDR DALA2025091506788Support Fitting · corrodedCORROSION ON FITTING SUPPORT THE SPHERICAL BEARING TRACK 2 INBD FLAP LT WING. COMPLIED WITH ER/A 628405-14. (1197264).SDR SWAA2025092914113Skin · delaminatedLEFT OTBD AFT FLAP UPPER SURFACE HAS AREA OF DELAMONATION AT INBD END JUST FWD OF T/E. REMOVED; REPLACED AND ADJUSTMENT CHECKED LT O/B AFT FLAP IAW AMM 27-51-22. VERIFIED TORQUES AND SAFETIES; ADJUSTMENT CHECK GOOD. VERIFIED COMPLETION CORRECTIVE ACTION 1 SDR SWAA2025091513610Skin · delaminatedRIGHT OTBD AFT FLAP HAS DELAMINATION, APPROXIMATELY 5.5 X 4.5 IN SIZE AT INBD UPPER SIDE. R & R RT OTBD AFT FLAP IAW AMM 27-51-22.SDR DALA2025091206731Bearing · corrodedCORROSION WAS FOUND AFFECTING INB'D AND OUTB'D ALUMINUM PLATES IN INNER AND OUTER RIB 5 ECCENTRIC BEARING LH WING OUTG'D FLAP TRACK 3. COMPLIED WITH ER/A 628388-14. (1193993).SDR DALA2025091206730Bearing · corrodedCORROSION WAS FOUND AFFECTING INB'D AND OUTB'D ALUMINUM PLATES IN INNER AND OUTER RIB 5 ECCENTRIC BEARING LH WING OUTG'D FLAP. COMPLIED WITH ER/A 628387-14. (1193865).SDR DALA2025091106713Support Fitting · corrodedCORROSION ON FITTING SUPPORT THE SPHERICAL BEARING TRACK 4 O/B FLAP RH WING. REPAIRED PER ER/A 628418-14. (1192970)SDR SWIA202512020909Fitting · chafedCHAFE ON RT OTBD FLAP ROLLER GUIDE FITTING FROM ROLLER BEARING. REMOVED AND REPLACED THE RT OTBD FLAP ROLLER GUIDE FITTING IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-41-02-001-001-A01, AND DWG CC670-14600, REV C.SDR ASAA2025090961327Rib · wornL-WING OB TRACK UPPER AND LOWER SURFACES AT OB FLAP HAS WEAR SPOTS. GROUNDED - YES. BLENDED DAMAGED AREA IAW B737-900ER SRM 51-10-02; ORIG. MATERIAL THICKNESS .300 IAW BAC DWG 113A3241 REV J; REMAINING MAT. THICKNESS IS .213 AS MEASURED WITH TOOL T-0080353 CALSDR DALA2025091106707Bearing · corrodedCORROSION FOUND AFFECTING INB'D AND OUTB'D AL PLATES AT TRACK #2 IN THE INNER AND OUT RIB 9 ECCENTRIC BEARING, LH WING,INB'D FLAP. COMPLIED WITH ER/A 628405-14. (1190565).SDR SWI2025F01888Rod · dentedRIGHT INBD FLAP INBD VANE ACTUATOR ROD HAS DENT. RT INBOARD FLAP INBD VANE ACTUATOR ROD END REPAIRED REF REO 670-57-52-257, REV -B, SYSTEM OPS TESTED GOOD. SKYWEST TASKCARD 51-900-1002-SKY COMPLETED.SDR SWI2025F01886Rod · dentedRIGHT INBD FLAP OTBD VANE ACTUATOR ROD HAS DENT. RT INBD FLAP OTBD VANE ACTUATOR ROD END REPAIRED REF REO 670-57-52-257, REV -B, SYSTEM OPS TESTED GOOD. SKYWEST TASKCARD 51-900-1002-SKY COMPLETED. SEE CONTINUE CARD FOR DETAILS.SDR FDEA202509081644Skin · corrodedLEFT WING INBOARD MAIN FLAP LOWER SKIN HAS CORROSION, (OUTBOARD FLAP TRACK AREA) UPON FURTHER EVALUATION ON LT WING INBD MAIN FLAP LOWER SKIN CORROSION FOUND OUT OF LIMITS IAW SRM 57-53-01-1A DETAIL I, FIG 101, SHEET 1, NOTE F AND APPLIED PERMANENT REPAIR IN SSDR DALA2025090806613Bearing · corrodedCORROSION SPHERICAL BEARING OUTBOARD FLAP TRACK 3 LH WING. REPLACED SPHERICAL BEARINGS OUTBOARD FLAP TRACK 3 LH WING AS PER A320- FAM AMM 57-53-21-000-001-A AS PER A320-FAM AMM 57-53-21-400-001. (1185070).SDR FDEA202509051622Skin · dentedRIGHT WING OB FLAP LWR SURFACE FOUND DENT AT 248 INCHES TO IB EDGE AND 6 INCHES TO AFT EDGE. REPAIRED RH WING OB FLAP LWR SURFACE DENT AT OTEF STA 261 AS PER B777 SRM 57-53-01-2R- 2 AND SRM 51-70-04-2R-1 REV 47.6 AND EA: G-5750-T0384798 P1. TITLE: WING-FLSDR SWIA2025120100903Skin · dentedADM# N606SK-8233. LEFT INBOARD FLAP AT FS 27 NEAR THE TRAILING EDGE. DENT ON LOWER SKIN MEASURES WIDTH 1/4 IN. X DEPTH .035". SRM 57-53-01. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICESSDR YENA2025090400909Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION ON TOP SKIN, TRAILING EDGE OVERHANG, LOWER SURFACE, BTW WX4013 AND WX4349 ( BTW RIB 8 7 RIB 9 ), ON RH WING; REFERENCE AEROMAN W.O. 2025 279 / 1- N.R. 481112 * PERFORMED PERMANENT REPAIR ON TOP SKIN PANEL #2, TRAILING EDGE OSDR YENA2025090400908Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION ON TOP SKIN, TRAILING EDGE OVERHANG, LOWER SURFACE, BTW WX40 13 & WX4349 ( BTW RIB 8 AND 9) ON LT WING; REFERENCE SAL WO 2025 279/1 NR 2025-481126. EVALUATED BLENDED AREA LOCATED ON TOP SKIN, T/E OVERHANG, LOWER SURFACE, BTWSDR REXA2025092500884Fitting · wornWEAR ON TWO FLAP FITTINGS, STUB FAIRINGS 171DL & 172DR, RT & LT WING TRAILING EDGE. FLAP FITTINGS WERE EVALUATED, AND DUE TO EXCESIVE DAMAGE, WERE REPLACED SRM 53-00-00-101-001-A01, AMM 20-21-00-910-801-A01, AND SRM 51-42-21-001-001-A01.SDR REXA2025092500883Support · wornWEAR ON TWO PLATE SUPPORTS OF FLAP STUB FAIRING 171DL & 172DR, RT & LT WING TRAILING EDGE. PLATE SUPPORTS WERE EVALUATED DUE TO EXCESIVE DAMAGE AND WERE REPLACED IAW SRM 53-00-00-101-001-A01, AMM 20-21-00-910-801-A01, AND SRM 51-42-21-001-001-A01.SDR DALA2025090106457Strut · corrodedCORROSION ON INTERCONNECTING STRUT CONNECTOR FIN 7543VC AT LT WING IB FLAP. REPLACED INTERCONNECTING STRUT CONNECTOR FIN 7543VC AT LH WING IB FLAP IAW ESPM 20-44-11. (1175108).SDR DALA2025090806611Strut · corrodedSHIP 3152 CORROSION INTERCONNECTING STRUT OB FLAP ON LH WING. CORRECTIVE ACTION: REMOVED AND REPLACED INTERCONNECTING STRUT FLAP ON LH WING ON SERVICEABLE CONDITION AS PER A320 FAM AMM 27-51-44-000-001-A AND AMM 27-51-44-400-001-A. (1172915).SDR DALA2025090806610Strut · corrodedCORROSION INTERCONNECTING STRUT IB FLAP ON RH WING . CORRECTIVE ACTION: REMOVED INTERCONNECTING STRUT OB FLAP ON RH WING ON UNSERVICEABLE CONDITION AS PER A320 FAM AMM 27-51-44-000-001-A. (1172907).SDR DALA2025090106453Strut · corrodedCORROSION INTERCONNECTING STRUT OB FLAP ON LT WING. R & R INTERCONNECTING STRUT OB FLAP ON LT WING ON UN UNSERVICEABLE CONDITION IAW AMM 27-51-44-000-001-A. (1172913).SDR FDEA202508291578Skin · dentedDENT INNER PART OF INBOARD FLAP WING RH INBOARD FLAP, INNER PART, WING RH WAS REPAIRED IAW B767 SRM 57-53-01-2R REPAIR 1, FIG. 201, SHEET 1-6, TABLE I REV.92 APR 15/2025SDR FDEA202508291565Flap · misrepairedEXISTING REPAIR ON RH WING OUTER FLAP LEADING EDGE SKIN BETWEEN RIB14 AND RIB17 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON RH WING OUTER FLAP LEADING EDGE SKIN BETWEEN RIB14 AND RIB17 WAS EVALUATED & FOUND NOT IN CONFORMITY WITH SRM 57-50-0SDR IPXA2025091104660Rib · crackedRIGHT WING, CENTER FLAP, TOP SKIN RIB FLANGE. CRACKS NOTED IN 2 AREAS AT RIB12. CIRCLED IN RED. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-95026-REQ1 AND VT-MAE EA 300-5750-27-A4117 REV. -.SDR IPXA2025091104681Rib · crackedRIGHT WING, CENTER FLAP, TOP SKIN RIB FLANGE. CRACK NOTED IN 1 AREA AT RIB15.CIRCLED IN RED. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-95026-REQ1 AND VT-MAE EA 300-5750-27-A4117 REV. -.SDR IPXA2025091104842Rib · crackedRIGHT WING,CENTER FLAP, TOP SKIN RIB FLANGE. CRACKS NOTED IN 3 AREAS AT RIB26. ACCOMPLISHED THE REPAIR IN ACCORDANCE WITH EO-95026-REQ1 AND VT-MAE EA 300-5750-27-A4117 REV. -.SDR IPXA2025091104710Rib · crackedRIGHT WING,CENTER FLAP, TOP SKIN RIB FLANGE. CRACK NOTED IN 1 AREA AT RIB16. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-95026-REQ1 AND VT-MAE EA 300-5750-27-A4117 REV. -.SDR IPXA2025091104697Rib · crackedRIGHT WING,CENTER FLAP, TOP SKIN RIB FLANGE. CRACKS NOTED IN 2 AREAS AT RIB19. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-95026-REQ1 AND VT-MAE EA 300-5750-27-A4117 REV. -.SDR IPXA2025091104847Rib · crackedRIGHT WING, CENTER FLAP, TOP SKIN RIB FLANGE. CRACKS NOTED IN 3 AREAS AT RIB27. CIRCLED IN RED. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-95026-REQ1 AND VT-MAE EA 300-5750-27-A4117 REV. -.SDR IPXA2025091104635Rib · crackedRIGHT WING, CENTER FLAP, TOP SKIN RIB FLANGE. CRACKS NOTED IN 3 AREAS AT RIB13. CIRCLED IN RED. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-95026-REQ1 AND VT-MAE EA 300-5750-27-A4117 REV. -.SDR IPXA2025091104804Rib · crackedRIGHT WING,CENTER FLAP, TOP SKIN RIB FLANGE. CRACKS NOTED IN 2 AREAS AT RIB25. ACCOMPLISHED REPAIR IR ACCORDANCE WITH EO-95026-REQ1 AND VT-MAE EA 300-5750-27-A4127, REV. -.SDR IPXA2025091104437Skin · crackedRIGHT WING, CENTER FLAP, TOP SKIN RIB FLANGE. CRACKS NOTED IN 2 AREAS AT RIB11. CIRCLED IN RED. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-95026-REQ1 AND VT-MAE EA 300-5750-27-A4117 REV. -.SDR VNAA202508280061Beam · chafedLH IB FLAP VANE ACTUATOR BEAMS (ALL 4) FOUND THERE TO BE VISUAL SIGNS OF WEAR/CHAFING FROM ROLLER CONTACT CORRECTIVE ACTION: REO 670-57-52-257 REV -A DATED 2024-08-20 COMPLIED WITH.SDR FDEA202508281560Skin · dentedDENT ON LOWER SURFACE OF OUTBOARD FLAP, AT 70" FROM OUTBOARD EDGE AND 8" FROM TRAILING EDGE, LH WING. LOWER SURFACE OF OUTBOARD FLAP, AT 70" FROM OUTBOARD EDGE AND 8" FROM TRAILING EDGE, LH WING WAS REPAIRED IAW B767 SRM 53-53-01-2R REPAIR 1, FIG. 201, SHESDR FDEA202508281557Wedge · dentedLH WING O/B FLAP (MPN: 113T3100-1078) TRAILING EDGE WEDGE LWR SURFACE A (7.7-INCH X 6.7- INCH) DENT AT WS. 672. REPAIRED LH WING O/B FLAP TRAILING EDGE WEDGE LWR SURFACE A (7.7- INCH X 6.7-INCH) DENT AT WS. 672. IAW SRM 57-53-01-2R AND SRM 51-70-05-0G. THSDR FDEA202508281553Skin · dentedR/H OTBD TRAILING EDGE FLAP HAS A DENT LOCATED ON THE LOWER SURFACE INBOARD OF THE INBOARD HINGE FAIRING (MWT). REPAIRED R/H WING OTBD TRAILING EDGE FLAP LOWER SKIN SURFACE DENT (3.3" X 2.0") AT LOCATION INBD OF THE INBOARD HINGE FAIRING AT WS 601, IN REF.SDR SWAA2025092408976Wedge · delaminatedLEFT INBD T/E MAIN FLAP AFT WEDGE DELAMINATED. LOCATED AND DRILLED FASTENER HOLES IN NEW MAIN FLAP T/E WEDGE REF SRM 51-40-02-0G-0. REPLACED THE WEDGE IAW SRM 51-10-02 & SRM 51-40-02-0G-0.SDR SWAA2025092408973Wedge · delaminatedRIGHT INBD T/E MAIN FLAP AFT WEDGE DELAMINATED. LOCATED AND DRILLED NEW WEDGE IAW SRM 51-40-02. INSTALLED NUTPLATES IAW SRM 51-40-02. INSTALLED THE NEW WEDGE 113A2550-604 IAW SRM 51-40-02.SDR SWAA2025092408417Skin · delaminatedR WING OTBD TRAILING EDGE AFT FLAP LOWER INBD SURFACE HAS DELAMINATION.SDR SWI2025F01699Shaft · damagedLEFT INBOARD FLAP, VANE ACTUATOR AT 584CB, SHAFT HAS MARRING. COMPLIED WITH THE REPAIR OF LT INBD FLAP, VANE ACTUATOR AT 584CB IAW REO 670-57-52-257, REV B. OPS CHECKED GOOD. NO DEFECTS FOUND.SDR SWI2025F01698Bonding Cable · brokenLEFT INBOARD FLAP, VANE ACTUATOR AT 584BB, HAS BROKEN BONDING CABLE AND MARRING INBETWEEN ACTUATOR CRADLE, COMPLIED WITH THE REPAIR OF LT INBD FLAP VANE ACTUATOR AT 584BB IAW REO 670-57-52-257 REV B. OPS CHECKED GOODSDR SWIA2025120200824Vane · damagedLEFT INBOARD FLAP, OUTBOARD VANE ACTUATOR SHAFT HAS MARRING, COMPLIED WITH THE REPAIR OF LEFT INBD FLAP, O/B VANE ACTUATOR SHAFT IAW REO 670-57-52-257, REV B. OPS CHECKED GOOD.SDR DALA2025082506283Flap · missingFCNT- AIRCRAFT ARRIVED AUS WITH THE LEFT WING OUTBOARD TRAILING EDGE AFT FLAP MISSING. MAINTENANCE REPLACED LEFT OUTBOARD FLAP, BOTH BELLCRANKS ASSYS, 4 CONTROL RODS AND THE #1 AND 2 FLAP CANOES PER B 737 AMM 27-51. REFER TO LOG PAGES 7056569, 7056570 AND 705SDR DALA2025082506292Skin · damaged(LOG 7056570) FOUND LT O/B FLAP DAMAGED. R/R LT OB FLAP IAW A/C 2750-4569-01.
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