JASC 5730
Service difficulty reports · 27,255
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 FDEA202507031101Skin · crackedDURING PERFORM UT & OPEN HOLE HFEC INSPECTION OF THE LEFT UPPER WING SKIN COMMON TO FASTENERS 0-5 AND FOUND 02EA CRCAK AT HOLE #5. LEFT WING UPPER SKIN #5 HOLE 02EA CRACKS REPAIRED AS PER B777 SRM 51-40-05-0G, SRM 51-40-04-0G, SRM 51-40-02-0G REV47.6 AND ESDR FDEA202507031100Skin · crackedDURING PERFORM UT & OPEN HOLE HFEC INSPECTION OF THE RIGHT UPPER WING SKIN COMMON TO FASTENERS 0-5 AND FOUND 02EA CRCAK AT HOLE #5. RIGHT WING UPPER SKIN #5 HOLE 02EA CRACKS REPAIRED AS PER B777 SRM 51-40-02-0G, SRM 51-40-04-0G, SRM 51-40-05-0G REV47.6 ANDSDR COEA2025103008919Panel · corrodedWO 264878 NR 600034 HEAVY CHECK COE/MAJOR REPAIR DISCREPANCY: PANEL 622CT HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIRED PER SRAS ES_00265302_01...25924 ISSUE A, DATED 8/6/2025.SDR COEA2025103004919Landing · corrodedWO 264878 NR 500045 HEAVY CHECK COE/MAJOR REPAIR DISCREPANCY: L/H WING FWD SPAR UPPER STRIP SLAT HAS LEVEL 2 CORROSION ON LANDING FOR PANEL 513 RIBS 13-21. CORRECTIVE ACTION: REPAIRED PER SRAS S572K0048...25988 ISSUE A, DATED 9/24/2025.SDR SWIA20251002702Skin · crackedCOMPLY WITH LATEST REVISION SB NO. 601R-57-044 TITLE: WINGS - LOWER WING PLANK - COLD WORK OF FASTENER HOLES IN THE LOWER WING PLANK PART C LEFT SIDE AT BL45.00, PART D LEFT SIDE AT WS 65.75, PART F RIGHT SIDE AT BL45.00, AND PART G RIGHT SIDE AT WS65.75. (FISDR IXXA20250809011Skin · corrodedLEFT WING, UPPER SURFACE SKIN IS CORRODED APPROX 7" OUTBD OF THE FUSELAGE STA 960SDR CALA2025070706260Panel · wornL/H WING PANEL S521UBX. PANEL CUT OUT AT INBD LA TCH AREA LAND STRUCTURE WORN. REPAIR WAS PERFORMED ON LH WING L/E PANEL 521UBX, PANEL CUTOUT A T INB IAW WORK PER UAL EC/RA#:5740-03399 AND VT MAE EA 757-5740- 13-A3987 REV- AND SRM 51-40-02-0G-0.SDR JR2R20250702065Screw · stuckL/H WING O/B AFT FLAP LOWER SKIN HAS A STUCK SCREW.SDR IPXA2025080816542Skin · damagedLH WING-ZONE500: LH WINGTIP LWR AFT CORNER DAMAGED. VERIFIED REPAIR ACCOMPLISHED IAW EO-94606-REQ1 AND VT-MAE EA 300-5730-27-A4061, REV.-.SDR SWAA2025081187405Access Panel · debondedDEBONDED SEAL LOCATED ACCESS PANELS 632KB 632JB AT RT WING. INSTALLED SEAL LOCATED ACCESS PANELS 632KB 632JB AT RT WING IAW B737-700 AMM 28-11-11-900-801.SDR SWAA2025072487030Panel · delaminatedLEFT WING LEADING EDGE PANEL 521DB; CORNER DELAMINATED AT ANTI-ICE DUCT CUTTOUT. REPAIRED CORNER DAMAGE TO PANEL 521DB IAW SRM 57-41-01-1A-1; SRM 51-70-08-0G-0 AND SRM 51-70-14-2R-3.SDR SWAA2025072487032Panel · delaminatedLEFT WING LEADING EDGE PANEL 521KB; 2 EACH CORNERS DELAMINATED ON FORWARD EDGE. REPAIRED LEFT WING LEADING EDGE PANEL 521KB 2EA CORNERS DELAMINATED IAW SRM 51-70-04-2R-13.SDR SWAA2025072887029Panel · delaminatedRIGHT WING LEADING EDGE PANEL 621HB AFT CORNER DELAMENATED. REPAIRED CORNER DAMAGE TO PANEL 621HB IAW SRM 57-41-01-1A-1, SRM 51-70-08-0G-0, AND SRM 51-70-14-2R-3.SDR GTIA2025063038977Skin Panel · corrodedCORROSION UPPER SURFACE LOC RIB 5 SPAR AREA ON LH WING RAF-01 3425498-01 GENERATED-PERFORMED PERMANENT REPAIR ON UPPER SURFACE LOC. RIB 5 REAR SPAR AREA ON LH WING I.A.W EA # 57-0060-25. THIS REPAIR IS CATEGORY A AND NOT REQUIRED INSPECTION.SDR GTIA2025063038976Skin Panel · corrodedCORROSION UPPER SURFACE BOTTOM SKIN LOC BTW RIB 5 AND RIB 5A DATUM ON RH WING RAF-01 3425500-01 GERNERATED-PERFORMED PERMANENT REPAIR LOC. BOTTOM SKIN LOC. BTW RIB 5 AND RIB 5A DATUM ON RH WING IAW EA #57-0059-25 THIS REPAIR IS CATEGORY A INSPECTION NOT REQUIRSDR GTIA2025063038975Skin Panel · corrodedCORROSION LOWER SURFACE BOTTOM SKIN LOC BTW RIB 11 AND RIB 12 FRONT SPAR ON RH WING RAF-01 3425499-02 GENERATED-PERFORMED PERMANENT REPAIR LOC LOWER SURFACE BOTTOM SKIN LOC. BTW RIB 11 AND RIB 12 FRONT SPAR ON RH WING IAW EA #57-0058-25 THIS REPAIR IS CATEGORYSDR VNAA20250629001Skin Panel · damagedLH WING UPPER WING PLANK LANDING FOR PANEL 542 AT HAS MUTIPLE DRILL STARTS. REPAIRED LH WING UPPER WING PLANK LANDING COMMON TO PANEL 542AT IAW MHIRJ REO 690-57-21-512 REV-A DATED 2025-05-20SDR AALA202507041641Skin · damagedAIRCRAFT IN BASE MAINTENANCE: CORROSION TRAILING EDGE ON TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 14 ON LH WING. MAINTENANCE PERFORMED INTERIM REPAIR LOC. ON TRAILING EDGE OVERHANG AREA AT LEVEL RIB 14 IAW EA 364685.SDR UIEA2025062500803Repair · debondedRIGHT WING INBD FORE FLAP UPPER INBD PANEL EXISTING REPAIR DOUBLER DISBOND. PERFORM PERMANENT REPAIR - UPGRADE THE EXISTING REPAIR ON TOP PANEL OF RH WING INBD FORE FLAP IAW EGAT EI NR. T2025A57M-1096 REV 1. CONDITION CHECK IS SATISFACTORY.SDR UIEA2025062500804Skin · corrodedCORROSION ON R/H WING UPPER SKIN UPPER SURFACE NEAR WBL 1193. BLEND OUT THE CORROSION AREA IAW SRM 51-10-02-0G-0 REV 62. ACCOMPLISHED REPAIR AREA IAW EI NR: T2025A57M-1057 REV 2. COMPLETED JOB AND CONDITION CHECK NORMAL.SDR UIEA2025062500805Skin · corrodedCORROSION ON LT WING UPPER SKIN UPPER SURFACE NEAR WBL 1217.133. . REPAIRED CORROSION AREA IAW EI NR: T2025A57M-1060 REV 2. COMPLETED JOB AND CONDITION CHECK NORMAL.SDR SWIA20251002627Skin · crackedTRANSFER FROM EAML 1639970 : TRANSFERRED FROM CAMP 30382930. REFERENCE CP 30339577 "DURING REQUESTED EDDY CURRENT OF THE LH WING PLANK (SEE CP 30339238-1), FOUND CRACK INDICATION IN FASTENER HOLE FORWARD OF THE LH MLG TEMINATING AFT IN THE MIDDLE LAYER.THIS NESDR SWAA2025073085564Panel · delaminatedPANEL 521CB FWD I/B CORNER DELAMINATED. REPAIRED PER [SRM 51-70-05-2R-6-A00737 (REPAIR 6 - REPAIR OF DAMAGE TO THE EDGEBAND OF A HONEYCOMB PANEL - AIRFRAME - PERMANENT) VERIFIED COMPLETE.SDR 2025FA0000488Skin · crackedRIGHT WING FWD WING WALK CORRUGATED SKIN CRACKED, REPLACED SKIN ASSY WITH NEW.SDR DALA2025063004851Skin · corrodedSHIP 9572 CORROSION ON WING UPPER TRAILING EDGE SKIN APROX. BTW XRS=353 - XRS=383 AT LH WING. CORRECTIVE ACTION: CORROSION LEVEL 2. AREA ON WING UPPER TRAILING EDGE SKIN APROX. BTW XRS=353 - XRS=383 AT LH WING WAS REPAIRED PER ERA 626626-14 REV ORIGINAL (10478SDR YENA2025062700653Skin · damagedDURING HEAVY MAINTENANCE: SECONDARY FINDING ELONGATED HOLES ON REFORCING PLATE LOC. AFT LOWER SK IN BTW RIB7 AND RIB8 ON RH WING; REF AEROMAN N/R 2025-373108, REMOVED AND REPLACED MOUNTING PLATE (REFORCING PLATE) LOC. AFT LOWER SKIN BTW RIB7 AND RIB8 ON RH WINSDR FDEA202506261051Access Panel · damagedRIGHT WING - FUEL TANK ACCESS PANEL 636AB CUTOUT NUMBER 28 HOLE REPAIR BUSHING FOUND MISSING. RIGHT WING - FUEL TANK ACCESS PANEL 636AB CUTOUT NUMBER 28 HOLE REPAIR BUSHING FOUND MISSING AT STATION XORS 696. RIGHT WING FUEL TANK ACCESS PANEL 636AB CUTOUT SDR SWAA2025071585572Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS236 AT LT WING 2025-390053 <[01]. REPLACED CORRUGATED PLATE AND FASTENERS LOCATED ORSS236 AT LT WING IAW B737-700 SRM 51-40-02 AND DWG: 115A2001 SHEET: 49; REV: - TOOK LENGTH OF CRACK ON CORRUGATED IS 0.765 INCHSDR 2025FA0000482Stiffener · crackedRIGHT WING FWD LWR I/B SKIN. FWD STIFFENER CRACKED.SDR 2025FA0000481Stiffener · crackedRIGHT WING FWD LWR I/B SKIN. AFT STIFFENER CRACKED.SDR CALA2025062705991Access Panel · missingRIGHT WING LEADING EDGE PANEL 621DB IDENTIFIED AS AN OUTBOARD LE SLAT MECHANISM LUBRICATION ACCESS DOOR/PANEL. DISCREPANCY PLACED ON CDL 57F LOG 5326724SDR DALA2025062604790Doubler · leakingSHIP 9546 FUEL LEAK FOUND DURING INSPECTION OF LH WING AFT LOWER SKIN DOUBLER AT XRS=164. CORRECTIVE ACTION: FUEL LEAK REPAIRED ON ERA 621176-14AD REV C (1044305)SDR JGVR20250625002Skin · corrodedMECHANICALLY REMOVED 3 AREAS OF CORROSION FROM LH WING LOWER SKIN, INBOARD OF THE INBOARD FLAP, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAIRED CORROSION BLENDS NETJETS REQUEST FOR TECHNICAL SERVICES BY CLEANING, TREATING AND PRIMING REPAIR AREA.SDR COEA2026012106816Access Panel · corrodedRIGHT WING LANDING ACCESS DOOR PANEL 622CT HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIRED PER SRAS DO/TS-3018/09...05261 ISSUE H, DATED 10/22/2025.SDR COEA2026012104816Access Panel · corrodedLEFT WING ACCESS DOOR PANEL LANDING 521DT HAS LEVEL 2 CORROSION. REPAIRED PER SRAS DO/TS-3018/09...05261 ISSUE H, DATED 10/22/2025.SDR COEA2026012103816Access Panel · corrodedLEFT WING ACCESS DOOR PANEL LANDING 522CT HAS LEVEL 2 CORROSION. REPAIRED IAW SRAS DO/TS-3018/09...05261 ISSUE H, DATED 10/22/2025.SDR COEA2025103009919Skin · corrodedLEFT WING LANDING ACCESS DOOR CUTOUT FOR 522CT HAS FRETTING. LEVEL 2 CORROSION. REPAIRED PER SRAS ES 00265302- 01-25924, ISSUE A.SDR COEA2025103006919Access Panel · corrodedWO 264878 NR 600028 HEAVY CHECK COE/MAJOR REPAIR DISCREPANCY: R/H WING LANDING ACCESS DOOR CUTOUT FOR 622CT HAS FRETTING. LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIRED PER SRAS ES_00265302_01...25924 ISSUE A, DATED 8/6/2025.SDR COEA2025103002919Skin · corrodedWO 264878 NR 500042 HEAVY CHECK COE/MAJOR REPAIR DISCREPANCY: L/H WING LANDING ACCESS DOOR CUTOUT FOR 521DT HAS FRETTING. LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIRED PER SRAS ES_00265302_01...25924 ISSUE A, DATED 8/6/2025.SDR IPXA2025070795201Skin · crackedLEFT WING / FOUND CRACKED LE SKIN AT SLAT TRACK #14. 040-28 , ATA 51-00.HFEC SURFACE INSP. (ASST.#20-1204, CAL. DUE: 12/11/25) OF LH WING LE SKIN AT SLAT TRACK #14 CUTOUT PER NDT SPM 06-10-01.001. CRACK DETECTED AT IB EDGE OF TRACK CUTOUT TO NEAR EDGE AFT.FABRSDR CALA2025062605903Skin · crackedRIGHT WING, LE I/B-LOWER SIDE OF THE GAP PANEL HAS A CRACK. REMOVED SKIN IAW B757-200 SRM 51-40-02, FABRICATED NEW PART GAP PANEL IA SRM 57-41-01-01-01, LOCATED AND DRILLED IAW SRM 51-40-0 2-0G-, REMOVED FASTENERS FOR ACCESS IAW SRM 51-40-02-0G-0, INSTA LLED SDR CALA2025062605897Skin · crackedLEFT WING, LE, GAP PANEL, I/B SIDE HAS A CRACK. REMOVED SKIN IAW B757-200 SRM 51-40-02-OG-0,FABRICATED NEW PART GAP PANEL IAW SRM 57-41-01-02-01,LOCATED AND DRILLED IAW SRM 51- 40-02-OG-0, REMOVED FASTENERS FOR ACCESS IAW SRM 51-40-02-OG-0, INSTALLED NEW PARTSDR SIMA20250622003Skin · gougedRH & LH WING FIXED L/E SKIN IS GOUGED UPPER SIDE BETWEEN SLAT 2 ; 3 AND 4. (MAJOR REPAIR) REPAIRED RH & LH WING FIXED LEADING EDGE SKIN BETWEEN SLAT 2; 3 AND 4 AND # IAW ERS-EJ-57MR-1718SDR CALA2025062305823Skin · corrodedLEFT WING LOWER SKIN FWD AND AFT OF FUEL PANEL 534BB BETWEEN RIB 26 AND RIB 27 HAS CORROSION. REPAIRED LT LOWER SKIN CORROSION AFT AND O/B OF FUEL PANEL 534BB BETWEEN RIB 26 & 27 AT REAR SPAR IAW EC/RA 5720-03540 REV A.SDR SWAA2025073084042Access Panel · crackedCRACK ON HOLE ACCESS PANEL 561BB TRAILING EDGE AT LT WING. REPAIRED ACCESS PANEL 561BB TRAILING EDGE AT LT WING IAW B737-700 SRM 51-70-04-2R-9 REPAIR 9.SDR SWAA2025071783852Panel · pulledLH WING TRAILING EDGE PANEL 561BB HAS DAMAGED SCREW HOLES UPPER SURFACE. LOCATED AFT EDGE ROW FROM SCREWS PULLING THROUGH COMPOSITE PANEL. ACCOMPLISHED REPAIR TO AREA REF SRM 51-70-04-2R-9 PER CORRECTIVE ACTIONS 1 AND 2. RESTORED FINISH TO AREA REF AMM 51-SDR SWAA2025071783857Panel · damagedLH WING TRAILING EDGE PANEL 561AB HAS DAMAGED SCREW HOLES UPPER SURFACE. LOCATED AFT EDGE ROW FROM SCREWS PULLING THROUGH COMPOSITE PANEL. REMOVED DAMAGE AND ACCOMPLISHED REPAIR REF SRM 51-70-04-2R-9 SEE C/A 1-4. RESTORED FINISH TO REPAIR AREA REF AMM 51-21-99SDR SWAA2025071783858Panel · pulledLH WING TRAILING EDGE PANEL 561CB HAS DAMAGED SCREW HOLES UPPER SURFACE. LOCATED AFT EDGE ROW FROM SCREWS PULLING THROUGH COMPOSITE PANEL. REMOVED DAMAGE AND ACCOMPLISHED REPAIR REF SRM 51-70-04-2R-9 SEE C/A 1-4. RESTORED FINISH TO REPAIR AREA REF AMM 51-21-99SDR AALA202509031054Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON TRAILING EDGE TOP SKIN LOWER SURFACE EXACTLY LOCATION IS RIB 14 PLUS 16 INCHES LEFT WING L=7.540 INCHES W=2.000 INCHES D=0.030 INCHES. MAINTENANCE PERFORMED TIME LIMITED REPAIR (EXTERNAL DOUBLER) ON RIB 14 PLUS 16 INCSDR UIEA2025061200756Skin · crackedLEFT WING, INBOARD L/E (FIXED L/E) SKIN CRACKED AT KRAS 217.5 AROUND FASTENER HOLE (1EA) AND AT SEAL RIB (REF: KRAS 224.82) BETWEEN THE NOSE BEAM AND FIRST STRINGER (2EA).(<P>PERFORMED LH WING AT REF KRAS 224.82 AND REF KRAS 217.5 FIXED LEADING EDGE SKIN PANEL
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