JASC 5730
Service difficulty reports · 27,254
Reports filed under 5730 · Wing, Plate/Skin, 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 = '5730' 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 = '5730' 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 KCSA202606031066Skin · corrodedLEFT WING FUEL TANK ACCESS CUTOUT 552CB HAS EVIDENCE OF CORROSIONSDR KCSA202606031065Skin · corrodedLEFT WING FUEL TANK ACCESS CUTOUT 552BB HAS EVIDENCE OF CORROSIONSDR KCSA202606031064Skin · corrodedLEFT WING FUEL TANK ACCESS CUTOUT 552AB HAS EVIDENCE OF CORROSIONSDR KCSA202606031063Skin · corrodedLEFT WING FUEL TANK ACCESS CUTOUT 545AB HAS EVIDENCE OF CORROSIONSDR KCSA202606031062Skin · corrodedLEFT WING FUEL TANK ACCESS CUTOUT 546BB HAS EVIDENCE OF CORROSIONSDR KCSA202606031059Skin · corrodedLEFT WING FUEL TANK ACCESS CUTOUT 546AB HAS EVIDENCE OF CORROSIONSDR KCSA202606031058Skin · corrodedRIGHT WING FUEL TANK ACCESS CUTOUT 653KB CUTOUT HAS EVIDENCE OF CORROSIONSDR KCSA202606031057Skin · corrodedRIGHT WING FUEL TANK ACCESS CUTOUT 653BB CUTOUT HAS EVIDENCE OF CORROSIONSDR KCSA202606031056Skin · corrodedRIGHT WING FUEL TANK ACCESS CUTOUT 652EB CUTOUT HAS EVIDENCE OF CORROSIONSDR AALA202607157959Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LOWER SKIN PANEL CUTOUT FOR ACCESS PANEL 640HB, BETWEEN WING RIBS 13 AND 14, BETWEEN WING STRINGERS 8 AND 11. REPAIRED SKIN PANEL PER EA 376036.SDR KCSA202606021055Skin · corrodedRIGHT WING FUEL TANK ACCESS CUTOUT 652DB CUTOUT HAS EVIDENCE OF CORROSIONSDR KCSA202606021054Skin · corrodedRIGHT WING FUEL TANK ACCESS CUTOUT 652CB CUTOUT HAS EVIDENCE OF CORROSIONSDR KCSA202606021053Skin · corrodedRIGHT WING FUEL TANK ACCESS CUTOUT 652BB CUTOUT HAS EVIDENCE OF CORROSIONSDR KCSA202606021052Skin · corrodedRIGHT WING FUEL TANK ACCESS CUTOUT 646BB CUTOUT HAS EVIDENCE OF CORROSIONSDR KCSA202606021051Skin · corrodedRIGHT WING FUEL TANK ACCESS CUTOUT 646AB CUTOUT HAS EVIDENCE OF CORROSIONSDR KCSA202606021050Skin · corrodedRIGHT WING FUEL TANK ACCESS CUTOUT 652AB CUTOUT HAS EVIDENCE OF CORROSIONSDR KCSA202606021049Access Panel · corrodedRIGHT WING FUEL TANK ACCESS PANEL 645BB HAS EVIDENCE OF CORROSIONSDR 2026FA0000698Skin · crackedRIGHT WING FWD WING WALK SKIN CRACKED ON CORRUGATED SKIN. REPLACED WING WALK CORRUGATED SKIN ASSY WITH NEW.SDR R61A2026063000177Skin · crackedDURING HEAVY CHECK MAINTENANCE FOUND CRACK ON RH LOWER WING SKIN SURFACE BETWEEN RIB 5-6 AND STRGR 18. RT WING LOWER SKIN SURFACE BETWEEN RIB 5-6 AND STRGR 18 REPAIRED IAW ETD2026-170-009575.SDR SWAA2026062308323Access Panel · damagedELONGATED HOLE ACCESS PANEL 661BB AT RT WING. REPAIRED ACCESS PANEL 661BB AT RT WING IAW SRM 51-70-04-2R-10, REPAIR 10.SDR SWIA2026053177681Skin · damagedUPON REMOVAL OF RH WING LEADING EDGE PANEL 622AB FOUND ELONGATED HOLE LOCATED ON PANEL LANDING STRUCTURE MARKED MX 32357423 C-CHECK RO 10132026OPENED HOLE IN WING PLANK, COLD WORKED HOLE, FABRICATED AND INSTALLED FREEZE PLUG, LOCATED AND DRILLED HOLE AND INSSDR SWIA2026053177208Skin · damagedFAILED NDT FOUND FULL SCREEN INDICATIONS ON THE LANDING OF RT WING LOWER PLANK ACCESS HOLE OF PANEL 640DB. REPAIRED 640DB ACCESS HOLE IAW REO 601R-57-21--030, REV L.SDR SWIA2026053177198Skin · damagedFAILED NDT FULL SCREEN INDICATIONS FOUND ON RT WING LOWER PLANK ACCESS HOLE WS1855 PANEL 650BB. REPAIRED 650BB ACCESS HOLE IAW REO 601R-57-21--030, REV L. COMPLETED SKYCARD 51-900-1003-SKY. NO WEIGHT CHANGE. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMESDR SWIA2026053177192Skin · failedFAILED NDT FULL SCREEN INDICATIONS FOUND ON RT WING LOWER PLANK ACCESS HOLE WS11683 PANEL 640EB. REPAIRED 640EB ACCESS HOLE IAW REO 601R-57-21--030 REV L, COMPLETED SKYCARD 51-900-1003-SKY. NO WEIGHT CHANGE. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMESDR IPXA2026061336906Skin · erodedERODED SKIN, LT WING L/E LOWER PANEL 521AB EXTERNAL SURFACE, ADJACENT NO.2 PYLON. I.A.W. 747-400F SRM 57-41-01-2R-2 REFER TO SRM 51-70-07-0G-0 REV. 106. REMOVE THE DAMAGE MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260 F FOR 130 MINUSDR CALA2026060116725Skin · crackedLEFT WING INBD L/E SKIN HOLES NR 10 AND 11 HAVE CRACK INDICATIONS. FABRICATED DOUBLER AND FILLER IAW UAL ECRA 5720-03641 AND SRM 57-41-01-2R-8 REPAIR 8. INSTALLED DOUBLER AND FILLER PER B737-900ER SRM 57-41-01-2R-8 REPAIR 8 AND ECRA 5720-03641.SDR CALA2026060116723Skin · crackedRIGHT WING INBD L/E SKIN HOLE NR 12 HAS A CRACK INDICATION. REPAIRED RT WING L/E SKIN AT HOLE NR 12 WITH FILLER AND DOUBLER AND APPLIED PROTECTIVE FINISHES IAW SRM 57-41-01 AND 51-20-01.SDR SWIA2026053076740Skin · crackedONE CRACK, LT WING AFT LOWER PLANK. DWG 601R10046, 7475 T7351. AFT EDGE AT WS 45. CRACK IS 1.3? LONG AND STARTS FROM AFT EDGE OF LT AFT LOWER WING PLANK AT WS 45. REPAIRED THE LH AFT LOWER WING PLANK AREA AT WS 45 IAW REO 601R-57-21-4080, REV-.SDR IPXA2026061306942Skin · erodedERODED SKIN, RT WING L/E NR 4 PYLON INBD FIXED PANEL. IAW AMM 06-09-08-912-001, REV 116, REMOVEED RT WING L/E NR 4 PYLON INBD LWR FIXED PANEL. REMOVED THE ERODED MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260 F FOR 130 MINUTES WITH SDR JGVR202605290201Panel · corrodedREPAIRED CORRODED LH AND RH WING PANEL LANDS COMMON TO PANELS 551TB AND 651TB BY BLENDING CORRODED AREAS, PERFORMING NDT, AND REPORTING FOR REPAIR DISPOSITION. FABRICATED AND INSTALLED REPAIR DOUBLERS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.SDR IPXA2026061688559Skin · erodedERODED SKIN, LT WING L/E LOWER PANEL 521EB FWD EDGE. IAW SRM 51-70-07-0G-0 REV. 106 REMOVED THE EROSION MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260 F FOR 130 MINUTES WITH A MINIMUM VACUUM OF 22 IN/HG. IAW AMM 20-51-01-912-008, SDR IPXA2026061688661Skin · erodedERODED SKIN, RT WING L/E NR.3 PYLON PNL NO.471DL. IAW AMM 20-51-01-912-008, REV 116. REMOVED THE PANEL 471DL. REMOVED THE EROSION MATERIALS AND CLEAN. BOND THE REPAIR PLIES AND THE FOIL WITH RESIN CURED AT 200 F FOR 220 MINUTES WITH MINIMUM VACUUM OF 22 IN/HGSDR IPXA2026061388574Skin · crackedCRACKED SKIN, RT WING T/E PANEL 673CB. IAW AMM 06-09-08-912-001, REV 116, REMOVED PANEL 673CB. IAW AMM 20-51-01-912-008, REV 116 TO INSTALL PANEL 673CB.SDR IPXA2026061388605Skin · erodedERODED RT WING LEADING EDGE LOWER FIXED PANEL 611BB. IAW SRM 57-41-01-2R-2, REFER TO SRM 51-70-07-0G-0 REV. 106. REMOVED THE DAMAGE MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260 F FOR 130 MINUTES WITH A MINIMUM VACUUM OF 22 IN/HG. SDR IPXA2026061388652Skin · erodedERODED SKIN, LT WING L/E LOWER PANEL 531AB FWD EDGE. IAW SRM 57-41-01-2R-2 REFER TO SRM 51-70-07-0G-0 REV. 106. REMOVED THE ERODED MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260 F FOR 130 MINUTES WITH A MINIMUM VACUUM OF 22 IN/HGSDR IPXA2026060488562Skin · crackedCRACKED SKIN, RT WING T/E UPPER FIXED PNL WBL 232. IAW SRM 51-40-02-0G REV.106 AND BOEING DWG 113U1011, SHEET 22, REV A. INSTALL FASTENERS AT RT WING T/E UPPER FIXED PANEL WBL 232.SDR 2026FA0000697Skin · crackedRIGHT WING FWD WING WALK SKIN CRACKED ON CORRUGATED SKIN. REPLACED WING WALK CORRUGATED SKIN ASSY WITH NEW.SDR SWAA2026060107518Access Panel · leakingDURING BRIEFING WITH THE GROUND CREW I WAS ASKED TO GO ALOOK AT THE LEFT (CAPTAIN SIDE) WING WE HAD ALREADY PULLED POWER AND WE OPERATING APU. LT WING HAD SIGNIFICANT FUEL LEAK . FUEL WAS RUNNING DOWN THE WING IN TO A/C BAY AND OUT TO THE GROUND . HAD PAX DESDR SWAA2026061706551Access Panel · damagedELONGATED HOLE ACCESS PANEL 661BB AT RT WING. REPAIRED THE ACCESS PANEL 661BB AT RT WING IAW SRM 51-70-04-2R-10, REPAIR 10.SDR SWAA2026061706552Access Panel · damagedELONGATED HOLE ON ACCESS PANEL 661CB TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661CB TRAILING EDGE AT RT WING IAW SRM 51-70-04-2R-10, REPAIR 10.SDR SWAA2026061706548Access Panel · damagedELONGATED HOLE ACCESS PANEL 561AB AT LT WING. REPAIRED THE ACCESS PANEL 561AB AT LT WING IAW SRM 51-70-04-2R-10, REPAIR 10.SDR SWAA2026061706550Access Panel · damagedELONGATED HOLE ACCESS PANEL 561BB AT LT WING. REPAIRED THE ACCESS PANEL 561BB AT LT WING IAW SRM 51-70-04-2R-10, REPAIR 10.SDR 21GA2026052623802Skin · corrodedCORROSION ON LOWER RH WING AT WS 314.30 - 372.20 STR 16-18SDR DALA2026052903251Doubler · gougedGOUGES (2 EAS) ON FIXED LEADING EDGE PREVIOS REPAIR DOUBLER BTW XOS 384.0 TO XOS 386.0 APPROX AT RT WING. REPAIRED PER PRI 634250-14 (1611243) (AIRCRAFT GROUNDED)SDR SWAA2026061505851Access Panel · crackedCRACKED ANGLE ACCESS PANEL 551FB AT LT WING REPLACED ANGLE ACCESS PANEL 551FB AT LT WING IAW B737-700 SRM-51-10-02 ITEM 9 AND SRM-51-40-02-0G-0.SDR SWAA2026061505944Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 561CB TRAILING EDGE AT LT WING REPAIRED ACCES PANEL 561CB TRAILING EDGE AT LT WING IAW SRM 51-70-04-2R-10 REPAIR 10.SDR SWAA2026061505945Access Panel · damagedELONGATED HOLES ACCESS PANEL 561AB AT LT WING. REPAIRED ACCESS PANEL 561AB AT LT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.SDR UIEA2026042900266Skin · damagedL/E SKIN REPAIRED FOR LHW L/E NEAR #1 PYLON I/B D-BEAM UPPER CHORD REPAIR(<P>L/E SKIN REPAIRED AS PER SRM 57-41-13-2R-2 REPAIR 2. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042900267Skin · damagedL/E SKIN REPAIRED FOR LHW L/E NEAR #1 PYLON I/B D-BEAM UPPER CHORD REPAIR(<P>L/E SKIN REPAIRED AS PER SRM 57-41-13-2R-2 REPAIR 2. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026042900268Skin · unsecureLHW L/E SKIN NEAR #1 PYLON I/B AREA FOUND RIVETS LOOSE.(<P>L/E SKIN REPLACED AS PER SRM 51-10-02, AND NEW L/E SKIN HOLES TRANSFERRED AS PER SRM 51-40-05, AND NEW L/E SKIN INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)
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