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 AALA202503218592Skin Panel · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT WING SHROUD BOX LOWER SKIN PANEL, LOWER SURFACE WORN BETWEEN WX379 AND WX897.5. REPAIRED SKIN PANEL PER EA 503705.SDR 2025FA0000068Access Panel · damagedLOWER RIGHT WING ACCESS PANEL, ORIGINAL P/N LB57650007-1 REV- HAS A NACA AIR SCOOP AIR DUCT THAT CONNECTS TO FUEL SYSTEM VENT SYSTEM. THIS PANEL RECEIVED A MINOR ALTERATION , BY INSTALLING THE BENDIX KING KLR-10 AOA SYSTEM HEATED PITOT TUBE ASSY P/N 89000008SDR DALA2025012900682Skin · corrodedSHIP 3136 CORROSION INDICATION WAS FOUND IN TOP SKIN PANEL 2, TRAILING EDGE OVERHANG AREA, LH WING. CORRECTIVE ACTION: PERFORMED ZERO STRESS JACKING LOAD CHECK AS PER A319 SRM 51-51-10-911-001 AND AS PER ER/A 621980-14. (0785041)SDR DALA2025012900681Skin · corrodedSHIP 3136 CORROSION INDICATION WAS FOUND IN TOP SKIN PANEL 2, TRAILING EDGE OVERHANG AREA, LH WING. CORRECTIVE ACTION: PERFORMED ZERO STRESS JACKING LOAD CHECK AS PER A319 SRM 51-51-10-911-001 AND AS PER ER/A 621980-14. (0785036)SDR DALA2025012900686Skin · corrodedSHIP 3136 CORROSION AT TOP SKIN PANEL 2, LOWER SURFACE, RS, TEOH, RIBS 13-18, LEFT HAND WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 621980-14. (0784747)SDR DALA2025012900685Skin · corrodedSHIP 3136 CORROSION INDICATION WAS FOUND IN TOP SKIN PANEL 2. CORRECTIVE ACTION: REPAIRED PER ER/A 621980-14. (0784735)SDR DALA2025012900684Skin · corrodedSHIP 3136 LH WING TOP SKIN PANEL 2 TE OVERHANG CORROSION. CORRECTIVE ACTION: REPAIRED PER ER/A 621980-14. (0784719)SDR DALA2025012900683Skin · corrodedSHIP 3136 CORROSION LH WING TOP SKIN PANEL 2 TE OVERHANG. CORRECTIVE ACTION: REPAIRED PER ERA 621980-14. (0784702)SDR JR2R20250128173Skin · chafedLH WING FIXED LEADING EDGE OVER PYLON HAS CHAFE MARKS.SDR SWAA2025022692416Access Panel · corrodedCORROSION ACCESS PANEL 632RB FUEL TANK RING RT WING 2025-81639<[01] REPLACED ACCESS PANEL 632RB FUEL TANK RING RT WING IAW B737-800 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 110A0110 SHEET 41; REV-.<BR><BR>RING CLAMP INSTALLATION TO BE ACCOMPLISHED SEE: TTGSDR SWAA2025021890078Access Panel · crackedCRACKS ON HOLES ACCESS PANEL 661BB TRAILING EDGE AT RT WING 2025-91880<[01] TOOL USED: HOT BONDER PN: HCS9200B; SN: 18185847; DUE DATE: 01-OCT-25;[02] TOOL USED P/N: EPOCH 600; S/N: 120357005; CAL DUE: 10-JUN-25.;[03] TOOL USED: HUMIDITY/TEMPERATURE CHART RECOSDR SWAA2025021890079Access Panel · crackedCRACKS ON HOLES ACCESS PANEL 561BB TRAILING EDGE AT LT WING 2025-91878<[01] TOOL USED: HOT BONDER PN: HCS9200B; SN: 18185847; DUE DATE: 01-OCT-25;[02] TOOL USED P/N: EPOCH 600; S/N: 120357005; CAL DUE: 10-JUN-25.;[03] TOOL USED: HUMIDITY/TEMPERATURE CHART RECOSDR JR2R20250127172Skin · chafedRH FIXED WING LEADING EDGE OVER PYLON HAS CHAFE MARKSSDR ASAA2025012655932Skin · crackedDURING FUEL LEAK CHECKS FOUND RIGHT WING CRACKED AT WS578 LOWER SURFACE JUST FORWARD OF TANK ACCESS PANEL. GROUNDED - YES. REPAIRED CRACK IAW ASA EA # 800-57EA-28207. THIS IS A CATEGORY B REPAIR WITH STAGE 1 APPROVAL FOR STATIC STRENGTH ONLY. A NEW FAA FORM 81SDR SWAA2025020489897Panel · delaminatedPANEL 521UB HAS EDGE DAMAGE & DELAMINATION OF EDGE REINFORCING STRIPS (MARKED) <[01]. CORRECTIVE ACTION ACCOMPLISHED ON N/R# TTG8Q00YBXFZ.SDR P5CA2025012700003Skin · crackedOPEN HOLE INSPECTION CARRIED OUT AS PER WORKLOAD: SB777-57A0125 RO ON LHW UPPER SKIN COMMON TO MLG TAB OUT FASTENER HOLES 0T AND FOUND HOLE NO. 5 WITH 02EA CRACK INDICATION APPROX. 0.020-0.030 INCHES LENGTH, VIEW LOOKING DOWN AFT AT 11 AND 5 O'CLOCK POSITION.(SDR P5CA2025012700004Skin · crackedOPEN HOLE INSPECTION CARRIED OUT AS PER WC: SB 777-57A0125 RO ON RHW UPPER SKIN COMMON TO MLG TAB OUT FASTENER HOLES 0-6 AND FOUND HOLE #5 WITH OPEN CRACK IND APPROX 0.020-0.030 INCHES LENGTH,VIEW LOOKING DOWN AFT AT 1.2 & 7 O'CLOCK POSITION.(<P>CRACKS ON FASTSDR SWAA2025022689544Access Panel · elongatedELONGATED HOLE ACCESS PANEL 195CR LOCATED AT RT WING 2025-81556<[01] TOOL USED ULTRASONIC FLAW DETECTOR PN. EPOCH 650; SN. 201036102; DUE DATE 25-OCT-25;[02] TOOL USED: MULTIMETER P/N: FLUKE 87; S/N: 58430097; DUE DATE: 17-JUN-25; HUMIDITY/TEMPERATURE CHART RESDR SWAA2025020489552Panel · delaminatedLEFT WING L/E PANEL 521UB HAS AN EDGE DELAMINATION.<[01] REPAIRED PER SRM 51-70-06-2R-1.SDR R61A2025012900060Skin · crackedSUSPECTED CRACK AT RH WING UPPER SKIN N EAR SPOILER #3 INBOARD HINGE. INSTALLED REPAIR DOUBLER REF ETD 2025-170-900513SDR R61A2025012800059Skin · crackedDURING AN OVERNIGHT BI-WEEKLY INSPECTION FOUND RH WING CRACKED JUST INBD OF RIB 17 AND JUST AFT OF FWD SPAR APROX 1.5 INCHES LONG. REPAIRED IAW ETD2025-900491 ALSO REF VP-053430-2024 N/R #2 FOR WORK PERFORMED.SDR R61A2025012800058Skin · crackedDURING AN OVERNIGHT BI-WEEKLY INSPECTION FOUND LH WING CRACKED JUST INBD OF RIB 17 AND JUST AFT OF FWD SPAR APROX 2.685 INCHS LONG. REPAIRED IAW ETD2025-170-900491 ALSO REF VP-053430 N/R # 1 FOR WORK PERFORMED.SDR AALA202504082887Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE TOP SKIN PANEL #2 LOWER SURFACE AT RIB 14. REPAIRED SKIN PANEL PER EA 362006.SDR AALA202504082364Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE TOP SKIN PANEL #2 LOWER SURFACE AT RIB 7. REPAIRED SKIN PANEL PER EA 362006.SDR AALA202504080175Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE TOP SKIN PANEL #2 LOWER SURFACE AT RIB 10. REPAIRED SKIN PANEL PER EA 362006.SDR FDEA202501210110Skin · wornPER WORKCARD T1-5710-125557A P2, LEFT HAND LOWER SKIN PLANK CUT-OUT 536AB BETWEEN STATION XORS 683.400 AND XORS 713.650 FOUND HOLE QUANTITIES (21) STATED IN STEP ON 1 NOT TALLY WITH STEP 1.A, 1.B AND 1C AND FASTENER HOLE #1 FOUND WITH NO BUSHING INSTALLESDR SWIA2025012200021Access Panel · corrodedLH WING FUEL CELL ACCESS DOOR LANDING AT PANEL 540EB HAS AN AREA OF MINOR CORROSION ON THE AFT EDGE MID POINT OF LANDING, APPROX 8" IN TOTAL.SDR GTIA2025011638687Access Panel · corroded"CORROSION FOUND ON LEFT WING FUEL ACCESS PANEL BETWEEN RIBS 14 AND 15 HOLE ""AB"" AT THE 12 O'CLOCK POSITION. LENGHT .4180 WIDTH .4180-REPAIRED FASTENER HOLE FOR LEFT WING FUEL MAN HOLE 540JB IAW A320 SRM 57-21-11-300-002 RDAF 81503198 / 0372024#B SRI 2800FC SDR GTIA2025011638682Skin · gouged"LEFT WING BOTTOM SKIN AT FUEL TANK ACCESS BETWEEN RIB 14-15 HAS GOUGE ON FWD SIDE OF ACCESS CUTOUT RAF-01 3292701-01 LENGTH 1.4 WIDTH .040 DEPTH .0655 SDR CREATED-REPAIRED LH WING SKIN AND FUEL ACCESS BETWEEN RIB 14-15 BOTTOM SKIN TOP SURFACE MAJOR REPAIR CATSDR FDEA202501210111Access Door · crackedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND WING SLAT OF ACTUATOR ACCESS DOOR FORWARD CORNER #5 FOUND 01 EACH CRACK APPROXIMATELY 0.5 . STATION XOS 490. CRACK AT RIGHT HAND WING SLAT OF ACTUATOR ACCESS DOOR FORWARD CORNER #5 STATION XOS 4SDR SWAA2025021387665Panel · debondedRIGHT WING L/E PANEL 621DB HAS DISBONDS AT I/B FWD CORNER AND FWD PANEL CUTOUT CORNERS<[01] RIGHT WING L/E PANEL 621DB WAS REPAIRED IAW SRM 51-70-05-2R-6;[02] JOB COMPLETE.SDR JR2R20250119796Skin · chafedLH WING FIXED LEADING EDGE OVER PYLON HAS CHAFE MARKSSDR JR2R20250119807Skin · chafedRH WING FIXED LEADING EDGE OVER PYLON HAS CHAFE MARKSSDR SWAA2025022887154Tail Cone · crackedR-WING FLAP FAIRING #6 AT TAILCONE IS CRACKED AND HAS A HOLE DOT# J148 <[01]. REPAIRED RH WING TAILCONE ON FLAP FAIRING #6 IAW 737-800 SRM 51-70-04-2R-1 REPAIR 1 AND APPLIED TOUCH UP PAINT IAW 737-800 AMM 51-21-99-300-802; [02] REPAIRED RH WING TAILCONE ON FLSDR SWIA202503260117Access Panel · corrodedRH WING FUEL CELL ACCESS PANE 650FB, LOWER WING PLANK ACCESS HOLE, HAS CORROSION PRESENT FROM 3 O'CLOCK POSITION TO 6 O'CLOCK POSITION. (C-CHECK RO 03/25/2024) (FILED CLOSED) BLENDED CORRODED AREA OF RH WING FUEL CELL ACCESS DOOR LANDING AT PANEL 650FB OSDR VNAA202501210016Access Panel · corrodedCORROSION ON SETTLEMENT AREA AT ACCESS PANEL 572AB OF LH WING CORROSION ON SETTLEMENT AREA AT ACCESS PANEL 572AB OF LH WING WAS REPAIRED PER REO 690-57-31-251 REV- -SDR SWIA2025012000017Access Panel · corrodedRH WING FUEL CELL ACCESS PANE 650FB, LOWER WING PLANK ACCESS HOLE, HAS CORROSION PRESENT FROM 3 O'CLOCK POSITION TO 6 O'CLOCK POSITION. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESSSDR DALA2025012000464Skin · corroded-AD- CORROSION ON UPPER SKIN BTW XRS 360 TO XRS 380 AT LH WING. SUMMARY OF NRC 0015: CORROSION LEVEL 2. CORROSION ON UPPER SKIN BTW XRS 360 TO XRS 380 AT LH WING WAS REAPAIRED PER PRI 623423-14 REV 2 AND ERA 623423-14AD REV ORIGINAL. ASSOCIATED ER/A 14-623423 SDR DALA2025012000441Skin · corrodedSHIP 3136 CORROSION UPPER SKIN LOWER SURFACE LOCATED BTW RIB20 TO RIB22 TRAILING EDGE AREA ON RH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS AS PER A319 SRM 57-21-11-283-026. (0766169)SDR JGVR20250117001Skin · corrodedMECHANICALLY BLENDED 3 AREAS OF CORROSION UNDER RH LOWER WING SKIN, AFT SIDE, INBD OF FLAP PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED BLENDED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.SDR DALA2025011700413Access Panel · damagedSHIP 3147 ELONGATED HOLE (2 E/A) ON ACCESS PANEL 640HB RH WING. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR LOC. ON WING CUT-OUT OF ACCESS PANEL 640HB ON RH WING AS PER A319 SRM 57-21-11-300-002. (0764719)SDR DALA2025011700411Skin · corrodedSHIP 3140 CORROSION IN 140 RH WING TOP SKIN PANEL #2 TRAILING EDGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 617851-14AD. (0764506)SDR DALA2025011700410Skin · corrodedSHIP 3140 OVERHANG / CORROSION IN RH WING TOP SKIN PANEL #2 TRAILING EDGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 617851-14AD. (0764502)SDR DALA2025011700409Skin · corrodedSHIP 3140 CORROSION WAS FOUND AT LOWER SKIN PANEL #2. CORRECTIVE ACTION: COMPLIED WITH ER/A 617851-14AD. (0764496)SDR UIEA2025011400059Skin · corrodedLH WING, UPPER SURFACE, BETWEEN REAR SPAR AND STGR L-10, WBL 97.9566 WITH CORROSION(<P>THE CORROSION AREA WAS REPAIRED BY INSTALLING 2 REPAIR DOUBLERS, 1 SKIN FILLER AND STRINGER SEGMENTS. THIS REPAIR INSTRUCTION WERE PROVIDED ON BOEING MESSAGE CMA-TLS-24 0218SDR VNAA20250115016Skin · gougedTHE LOWER WING SKIN IS GOUGED AFT OF FUEL PANEL 511AB, APPROXIMATELY 0.20" LONG AND 0.007" DEEP. CORRECTIVE ACTION REPAIRED IAW REO-670-57-21-997 REV-- DATED 10-17-24SDR VNAA20250115015Skin · corrodedTHE LOWER WING SKIN IS GOUGED AFT OF FUEL PANEL 611AB, APPROXIMATELY 0.25" LONG AND 0.018" DEEP. CORRECTIVE ACTION: REPAIRED IAW REO-670-57-21-997 REV-- DATED 10-17-24SDR R61A2025033000166Skin · corrodedLH WING SLAT #2 IB TRACK CUTOUT FOUND CRACK IN SKIN. MX REPAIRED SKIN IAW ETD 2025-904085SDR R61A2025033000165Skin · corrodedRH WING SLAT #2 IB TRACK CUTOUT FOUND CRACK IN SKIN. MX REPAIRED SKIN IAW ETD2025-904436.SDR UIEA2025011300043Skin · corrodedRIGHT WING, UPPER SKIN CORROSION ON SETTLEMENT AREA OF CAP FILL, OUTER FACE.(<P>RIGHT WING, UPPER SKIN CORROSION ON SETTLEMENT AREA OF CAP FILL OUTER FACE WAS REWORKED AND EVALUATED. FOUND WITHIN ALLOWABLE LIMITS IAW SRM 57-20-01-1A-1 TABLE 1 REV. 127 15-DEC-2
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