JASC 5730
Service difficulty reports · 27,259
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 NACA2025040800005Skin · corrodedCORROSION WAS FOUND AT LT WING UPPER SKIN UPPER SURFACE BETWEEN WS.364 AND WS.367 , LEADING EDGE SKIN AREA. WS.371 AND WS.374 , LEADING EDGE SKIN AREA. WS.422 AND WS.424 , LEADING EDGE SKIN AREA. WS.428 AND WS.430 , LEADING EDGE SKIN AREA. WS 456 AND WS.4SDR NACA2025040800004Skin · chafedLEFT WING UPPER SKIN UPPER SURFACE BETWEEN WS.260 AND WS.208.5, 363, AND WS.366 , WS.376 AND WS.380 , WS 417 AND WS.418.5 , WS.427 AND WS.428.5 , WS.433 AND WS.434.5 , FRONT SPAR AREA . REMOVED CORROSION LEVEL AT LH WING UPPER SKIN SURFACE SRM 51-10-02 PARA 1SDR NACA2025040800003Skin · chafedCORROSION FOUND AT RH WING UPPER SKIN UPPER SURFACE WS.135 , STR-7, WS.136 , STR-6, WS.137 , STR-4, WS.140 , STR-4, WS.147 , STR-7. CORROSION FOUND AT RH WING UPPER SKIN ANGLE WS.143 BETWEEN STR-9~ STR-10. PERFORMED REPAIR AS PER EO NO 737-57-0052 CAT B REPSDR AALA202504093812Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN LEFT WING UPPER SKIN TRAILING EDGE FROM STA 1530 TO STA 1580, FROM WL 123 TO WL 124. REPAIRED PER EA 362936.SDR 2025FA0000255Panel · crackedLH WING UPPER SKIN PANEL FOUND CRACKED, DELAMINATED, FOUND DURING INSPECTION PER B223914; EXTERNAL - GV: WING UPPER SKIN PANELS. TO INCLUDE: FORWARD OF LEADING EDGE SPAR, FRONT SPAR TO REAR SPAR, & AFT OF REAR SPAR. ACCESS NOTE: UPPER WING SKIN LOWER SURFACE -SDR EE4Y2025040822152Skin · bulgedLEFT WING REAR SPAR, TOP SKIN LOWER SURFACE OVERHANG AREA BETWEEN RIB 13 AND RIB 15 SEAL PLATE BULGED. PERFORMED BLEND OUT REPAIR ON LH WING TOP SKIN PANEL 2 LOWER SURFACE BETWEEN RIB 13 AND RIB 15 IAW COOPESA EO N° COO-EO-2025-21701-R02 DATED 03/21/2025. APPRSDR EE4Y2025040822150Skin · corrodedLH WING BOX TOP SKIN TRAILING EDGE OVERHANG AREA LOWER SURFACE EXISTING BLEND OUT WITH CORROSION AT RIB 14+400MM. PERFORMED BLEND OUT REPAIR ON LH WING TOP SKIN PANEL 2 LOWER SURFACE AT RIB 14+400MM (AREA 7) IAW COOPESA EO N° COO-EO-2025-21701-R02 DATED 03/21/SDR NACA2025040700003Skin · corrodedCORROSION FOUND AT RH WING UPPER SKIN UPPER SURFACE WS.565 BETWEEN STR-11~ STR-12. PERFORMED REPAIR AS PER EO NO 737-57-0052 CAT B REPAIR, REF FAA 8100-9, EO 202504160065-0003.SDR NACA2025040700002Skin · corrodedCORROSION FOUND AT RH WING UPPER SKIN UPPER SURFACE WS.583 BETWEEN STR-11~ FRONT SPAR. PERFORMED REPAIR AS PER EO NO 737-57-0052 CAT B REPAIR, REF FAA 8100-9, EO 202504160065-0003.SDR NACA2025040700001Skin · chafedCORROSION FOUND AT RT WING UPPER SKIN UPPER SURFACE WS.252, FRONT SPAR. WS.261 , FRONT SPAR . CORROSION FOUND AT RT WING UPPER SKIN UPPER SURFACE WS.266 , SKIN FWD EDGE. CORROSION FOUND AT RT WING UPPER SKIN UPPER SURFACE WS.268, SKIN FWD EDGE. CORROSION FSDR SWAA2025051956234Access Panel · crackedCRACK AROUND HOLES ACCESS PANEL 561BB TRAILING EDGE AT LT WING 2025-242338<[01] TOOL USED: SCALE PN: CR5200 SN: 8343110809 DUE DATE: 06-MAR-26.;[02] TOOL USED: HOT BONDER P/N: HCS9200B; S/N: 18185847; DUE DATE: 01-OCT-25;[03] TOOL USED P/N: EPOCH 600; S/N: 120SDR SWAA2025050554053Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 551ET (6 EA) 2025-232399<[01] TOOL USED ON STEP 10 ULTRASONIC FLAW DETECTOR P/N: EPOCH 650; S/N: 190776902; CAL DUE DATE: 15-OCT-25;[02] SCALE P/N CR5200; S/N: 8343110809; DUE DATE: 06-MAR-26.;[03] TOOL USED: HOT BONDER PN:HCS92SDR CALA2025041403785Skin · corrodedRH WING FUEL TANK RIBS 18-19 PANEL LAND FASTENER HOLES ELONGATED PER HAECO LCQ N/R 9290923/38923 GEN BY V798788SFR COMPLETED ESFR COMPLETED ESFR COMPLETED IDENTIFIED RH WING FUEL TANK PANEL 640NB ELONGATED HOLES P, K, F , B, C, G, L, Q, U, M, AND E. REAMED HOLSDR CALA2025041403784Skin · corrodedRH WING FUEL TANK RIBS 17-18 PANEL LAND FASTENER HOLES ELONGATED EVIDENCE OF CORROSION PER HAECO LCQ N/R 9290922/38922 GEN BY V798788ESFR COMPLETED IDENTIFIED RH WING FUEL TANK PANEL 640MB ELONGATED HOLES F, G, K , AND P. REAMED HOLES TO DIA: .328?, REPAIRED FSDR IXXA20250410001Access Panel · corrodedRIGHT WING LOWER ACCESS PANEL 632AB IS WORN AND CORRODEDSDR EE4Y2025040722149Skin Panel · corrodedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-572178-01-1-001 SECONDARY FINDING LH WING BOX TOP SKIN TEOH UPPER SURFACE WITH CORROSION BETWEEN WX= 4010,2 AND WX= 4390,2. PERFORMED BLEND OUT REPAIRON LH WING TOP SKIN PANEL 2 UPPER SURFACE BETWEEN WX 3494,5 ASDR EE4Y2025040722148Skin · corrodedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-572178-01-1-001 LEFT WING BOX TOP SKIN TRAILING EDGE OVERHANG LOWER SURFACE SKIN WITH CORROSION AT WX=3654,5. PERFORMED BLEND OUT REPAIR ON LH WING TOP SKIN PANEL 2 LOWER SURFACE BETWEEN WX 3494,5 AND WX 4010,2 SDR EE4Y2025040722147Skin Panel · corrodedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-572178-01-1-001 LEFT WING TOP SKIN LOWER SURFACE OVERHANG AREA AT WX 4274 WITH CORROSION WAS FOUND. PERFORMED BLENT OUT REPAIR ON LH WING TOP SKIN PANEL 2 LOWER SURFACE BETWEEN WX 3494.5 AND WX 4490.52 (AREA 2) SDR EE4Y2025040722146Skin Panel · corrodedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-572179-01-1-001 LEFT WING REAR SPAR TOP SKIN LOWER SURFACE OVER HANG AREA 11 AND 12 SEAL PLATE BULGED WAS FOUND. PERFORMED BLEND OUT REPAIR ON LH WING TOP SKIN PANEL 2 LOWER SURFACE BETWEEN RIB 11/12 (AREA 6) ISDR JGVR202504007006Panel · corrodedMECHANICALLY REMOVED 2 AREAS OF CORROSION FROM LH WING TRAILING EDGE PANEL 532GB, PERFORMED NDT, REPORTED FOR REPAIR DISPOSITION, CLEANED, TREATED, AND, PRIMED PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.SDR SWAA2025050722201Access Panel · crackedCRACK AROUND HOLES ACCESS PANEL 661BB TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661BB TRAILING EDGE AT RT WING IAW SRM 51-70-05-2R-6 REPAIR 6.SDR R61A2025040900174Skin · crackedDURING OVERNIGHT INSPECTION FOUND RH WING LOWER SKIN CRACKED INBD OF RIB 17 JUST AFT OF FWD SPAR, LENGTH 20 MM. REPAIRED IAW ETD2025-170-905482 ALSO REF VP-008365-2025 FOR WORK ACCOMPLISHED.SDR DALA2025040802714Access Panel · corroded(LOG 0898624) WEAR MARKS IN RT OUTBD WING FUEL TANK ACCESS HOLE CUTOUT INBD SIDE BETWEEN RIB 17 AND RIB 18. MATERIAL REMOVED .004" MAX ALLOWABLE .050" FOUND TO BE WITHIN LIMITS IAW B737 SRM 57-20-01-1A AND REPAIRED AREA IAW B737 SRM 57- 20-01-2R-1- ASSET#SA000SDR SWIA202507160405Access Panel · damagedRIGHT WING HAS 1 ELONGATED HOLE AT THE LANDING FOR ACCESS PANEL 698AT. REPAIRED ELONGATED HOLE AT RH WING ON THE LANDING FOR ACCESS PANEL 698AT IAW REO# 690-57-51-419, REV --. COMPLIED WITH TASK CARD 51-900-1002-SKYSDR SWAA2025050521876Access Panel · damagedELONGATED HOLES ON PLATE LOCATED ACCESS PANEL 644BB AT RT WING 2025-232389<[01] REPLACED PLATE LOCATED ACCESS PANEL 644BB AT RT WING IAW B737-700 SRM 51-40-02-0G-0.;[02] REPLACED PLATE LOCATED ACCESS PANEL 644BB AT RT WING IAW B737-700 SRM 51-40-02-0G-0.SDR SWAA2025050538272Access Panel · elongatedELONGATED HOLES ON PLATE LOCATED ACCESS PANEL 644BB AT RT WING 2025-232389<[01] REPLACED PLATE LOCATED ACCESS PANEL 644BB AT RT WING IAW B737-700 SRM 51-40-02-0G-0.;[02] REPLACED PLATE LOCATED ACCESS PANEL 644BB AT RT WING IAW B737-700 SRM 51-40-02-0G-0.SDR CALA2025040703589Skin · crackedCRACK FOUND AND VERIFIED ON LOWER L/H SKIN SURFACE, SECOND FASTENER FROM THE END OF STRINGER 9 BETWEEN RIBS 18 AND 19. ON THE LH WING LOWER SKIN BETWEEN WSTA 564 AND WSTA 591, ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2 OF ECRA 5720-03513 ON OR BEFORE 04 OCTSDR SWAA2025050757002Skin · crackedCRACK LOWER SURFACE OF THE LEADING EDGE NOSE SKIN AT ACTUATOR RIB LOC. SLAT 4 LOWER SURFACE AT LT WING. INSTALLED PERMANENT REPAIR PARTS [1] DOUBLER ; [2] FILLER AND FASTENERS LOCATED LEADING EDGE NOSE SKIN LOWER SURFACE SLAT 4 AT LT WING IAW SRM 57-42-01-2RSDR R61A2025042500213Skin · crackedWHILE IN HEAVY CHECK - RH WING LOWER SKIN AT APPROX BIB 3, SKIN HAS A CRACK. REPAIRED RH WING LOWER SKIN RIB 3 AREA REF: ETD2025-170-905560.LSDR DALA2025041702980Skin · damagedSHIP 3276 DISC: DTE ER/A 624251-14AD. REPAIR AT RH WING TOP SKIN, TE OVERHANG REQUIRES DTE FOLLOW UP PRIOR TO 21SEP2025. C/A: REVISE / UPDATE ER/A 624251-14AD WITH DTE RESULTS PRIOR TO 21SEP2025. AIRBUS DOSSIER 81551722. ASSOCIATED ER/A 14-624251 ADDED FOR AC SDR DALA2025040802713Access Panel · corroded(LOG 0895191) WEAR MARKS IN RT OUTBD WING FUEL TANK ACCESS HOLE CUTOUT INBD SIDE BETWEEN RIB 17 AND RIB 18. REPAIRED AREA IAW B737 SRM 57- 20-01-2R-1.SDR DALA2025040702629Repair · noneSHIP 685 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 625151-14AD. CORRECTIVE ACTION: REF ERA 625151-14AD. (0895965)SDR IXXA202504030009Skin · crackedLH OB WING TIP HASBARE METAL, ERROSION AND SKIN IS CRACKED JUST OB OF #1 SLATSDR IXXA20250403003Skin · corrodedUPPER WING SKIN HAS CORROSION AT THE AFT AREA BY WING TO BODY SPLICESDR WRXR20250403001Access Panel · corrodedCORROSION UNDER PANEL 621BR AT INBOARD BOTTOM FLANGE AROUND FASTENER HOLES. WS45. REMOVED CORROSION AT R/H WS45 ON AREA OF WING UNDER ACCESS PANEL 621BR INBOARD BOTTOM FLANGE AROUND FASTENER HOLES AND CREATED GRID FOR NDT TO DETERMINE MATERIAL THICKNESS IAW CRSDR AALA202506273011Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE OVERHANG TOP SKIN PANEL UPPER SURFACE AT RIB 5. REPAIRED SKIN PANEL PER EA 363116.SDR SWIA20250613402Skin · damagedLH WINGLET FWD, IB SKIN FOUND TO HAVE PREVIOUSLY ELONGATED AND DENTED HOLE (C-CHECK RO 06/12/2025)REMOVED AND REPLACED LH WINGLET FWD IB SKIN WITH REFERENCE TO SRM 51-42-13, SRM 51-42-22 AND REO 601R-57-31-1450 REV "--" DATED 2025-04-10. COMPLIED WITH TASK SDR SWIA202504100002Doubler · damagedPER ISE-STR-25-026 REV. - A AND REO 601R-57-00-205 DATED: 2025-03-25 REV -- : DETERMINE SERVICABILITY OF THE ORIGINALLY REPORTED DAMAGED LH WING EXTENSION LOWER SKIN DOUBLER (DWG 600-10380) INSPECTED THE LH WING EXTENSION LOWER SKIN DOUBLER IN REFERENCE WITH TSDR DALA2025040702646Access Panel · worn(LOG 0891638) RH WING FUEL TANK PANEL 631AB CUTOUT HAS WEAR SPOTS. REMOVED EDGE DAMAGE FROM R/H WING FUEL PANEL 631AB CUTOUT IAW B737 SRM 51-10-02-OG. REMOVED 0.011" MATERIAL FROM THE EDGE OF THE R/H WING FUEL TANK PANEL 631AB CUTOUT, MAX ALLOWED OF 0.050", FOSDR DALA2025040702645Access Panel · worn(LOG 0891612) RH WING FUEL TANK PANEL 632AB CUTOUT HAS WEAR SPOTS. REMOVED EDGE DAMAGE FROM R/H WING FUEL PANEL 632AB CUTOUT IAW B737 SRM 51-10-02-OG. REMOVED 0.006" MATERIAL FROM THE EDGE OF THE R/H WING FUEL TANK PANEL 632AB CUTOUT, MAX ALLOWED OF 0.050", FOSDR DALA2025040702644Access Panel · worn(LOG 0891591) RH WING FUEL TANK PANEL 632FB CUTOUT HAS WEAR SPOTS. REMOVED EDGE DAMAGE FROM R/H WING FUEL PANEL 632FB CUTOUT IAW B737 SRM 51-10-02-OG. REMOVED 0.008" MATERIAL FROM THE EDGE OF THE R/H WING FUEL TANK PANEL 632FB CUTOUT, MAX ALLOWED OF 0.050" , FSDR DALA2025040702643Access Panel · worn(LOG 0891519) WEAR MARKS IN RT OUTBD WING FUEL TANK ACCESS HOLE CUTOUT INBD SIDE BETWEEN RIB 18 AND RIB 19. REMOVED WEAR MARKS IN RT OUTBD WING FUEL TANK ACCESS HOLE CUTOUT INBD SIDE BETWEEN RIB 18AND RIB 19. IAW B737 51-10-02, EVALUATED WEAR MARKS IN RT OUTBDSDR DALA2025040702642Access Panel · worn(LOG 0891270) WEAR MARKS IN RT OUTBD WING FUEL TANK ACCESS HOLE CUTOUT INBD SIDE BETWEEN RIB 16 AND RIB 17. COMPLIED WITH B737 57-20-01-2R REPAIR 1 AT WEAR MARKS IN RT OUTBD WING FUEL TANK ACCESS HOLE CUTOUT IB SIDE BETWEEN RIB 16 AND 17.SDR DALA2025040702641Access Panel · worn(LOG 0891248) WEAR MARKS IN RT OUTBD WING FUEL TANK ACCESS HOLE CUTOUT BETWEEN RIB 7 AND RIB 8 INBD SIDE. REMOVED DAMAGE AND WEAR MARKS IN RT OUTBD WING FUEL TANK ACCESS HOLE CUTOUT BETWEEN RIB 7 AND RIB 8 INBD SIDE.NO WEAR NOTED ON STRUCTURE ONLY PRIMER DAMAGSDR DALA2025040702640Access Panel · worn(LOG 0891208) RH WING FUEL TANK PANEL 632HB CUTOUT HAS WEAR SPOTS. REMOVED EDGE DAMAGE FROM R/H WING FUEL PANEL 632HB CUTOUT IAW B737 SRM 51-10-02-OG. REMOVED 0.009" MATERIAL FROM THE EDGE OF THE R/H WING FUEL TANK PANEL 632HB CUTOUT, MAX ALLOWED OF 0.050", FOSDR DALA2025040702639Access Panel · worn(LOG 0891174) RH WING FUEL TANK PANEL 632JB CUTOUT HAS WEAR SPOTS. REMOVED EDGE DAMAGE FROM R/H WING FUEL PANEL 632JB CUTOUT IAW B737 SRM 51-10-02-OG. REMOVED 0.011" MATERIAL FROM THE EDGE OF THE R/H WING FUEL TANK PANEL 63 JB CUTOUT, MAX ALLOWED OF 0.050", FOSDR DALA2025040402593Access Panel · worn(LOG 0891496) WEAR MARKS IN RT OUTBD WING FUEL TANK ACCESS HOLE CUTOUT INBD SIDE BETWEEN RIB 17 AND RIB 18. REMOVED WEAR MARKS IN RT OUTBD WING FUEL TANK ACCESS HOLE CUTOUT INBD SIDE BETWEEN RIB 17 AND RIB 18. IAW B737 51-10-02, EVALUATED WEAR MARKS IN RT OUTBSDR DALA2025040402590Access Panel · worn(LOG 0891625) RH WING FUEL TANK PANEL 631BB CUTOUT HAS WEAR SPOTS. REMOVED 0.013" MATERIAL FROM THE EDGE OF THE R/H WING FUEL TANK PANEL 631BB CUTOUT, MAX ALLOWED OF 0.050", FOUND TO BE WITHIN LIMITS IAW B737 SRM 57-20-01-2R REPAIR 1. RESTORED SURFACE FINISH ISDR DALA2025040402589Access Panel · worn(LOG 0891602) RH WING FUEL TANK PANEL 632EB CUTOUT HAS WEAR SPOTS. REMOVED EDGE DAMAGE FROM R/H WING FUEL PANEL 632EB CUTOUT IAW B737 SRM 51-10-02-OG. REMOVED 0.004" MATERIAL FROM THE EDGE OF THE R/H WING FUEL TANK PANEL 632EB CUTOUT, MAX ALLOWED OF 0.050", FOSDR DALA2025040402588Access Panel · worn(LOG 0891581) RH WING FUEL TANK PANEL 632GB CUTOUT HAS WEAR SPOTS. REMOVED EDGE DAMAGE FROM R/H WING FUEL PANEL 632GB CUTOUT IAW B737 SRM 51-10-02-OG. REMOVED 0.010" MATERIAL FROM THE EDGE OF THE R/H WING FUEL TANK PANEL 632GB CUTOUT, MAX ALLOWED OF 0.050", FO
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