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 DALA2025040402587Access Panel · worn(LOG 0891555) RH WING FUEL TANK PANEL 632HB CUTOUT HAS WEAR SPOTS. REMOVED 0.009" MATERIAL FROM THE EDGE OF THE R/H WING FUEL TANK PANEL 632HB CUTOUT, MAX ALLOWED OF 0.050", FOUND TO BE WITHIN LIMITS IAW B737 SRM 57-20-01-2R REPAIR 1. RESTORED SURFACE FINISH ISDR EE4Y2025040222120Skin · crackedDURING THE STRUCTURE INSPECTION, WAS FOUND THE RH WING LEADING EDGE BETWEEN RIBS 19 AND 20 THE SKIN WITH CRACK. THE DISPREPANCIE WAS REPORTED TO EMB AND REPAIRED IAW ETC2025-190-901654 REV. A AND COOPESA ENGINEERING ORDER COO-EO-2025-21705 DTD FEB 11 2025SDR EE4Y2025040222119Skin · damagedDURING ACCOMPLISHING THE SB 190-57-0056, THE REMOVAL OF THE LH WING FORWARD INBOARD FITTING IT WAS FOUND A FASTENER HOLE OVERSIZED TO 12.62MM. DUE TO IT, THE CNDITION WAS REPAIRED IAW ETD2025-190-902373 AND COOPESA ENGINEERING ORDER COO-EO-2025-21765 DTD FEB 2SDR NACA2025040100002Skin · corrodedCORROSION FOUND AT RH WING UPPER SKIN UPPER SURFACE WS.135 , STR-9. PERFORMED REPAIR AS PER EO NO 737-57-0052 CAT B REPAIR, REF FAA 8100-9, EO 202504160065-0003SDR SWIA2025052700401Access Panel · corrodedL/H WING, LOWER WING PLANK FUEL ACCESS PANEL CUTOUT HAS MINOR CORROSION AT THE OUTBOARD AND INBOARD EDGES. (540BB) (C-CHECK RO 05/27/2025)COMPLIED WITH REPAIR TO 540BB HOLE#1 LOCATION LOWER WING PLANK CUTOUT IAW REO 601R-57-21-030 REV L DATED 2014-02-05. COMPLSDR R61A2025042500214Skin · crackedWHILE IN HEAVY CHECK - CK UNDER WING LH AT RIB 4A PASS 2 RIVETS. REMOVED CRACK AND INSTALLED FILLER AND DOUBLER ON LH WING AT RIB 4A REF ETD2025-170-905414 REV ASDR SWAA2025043055798Access Panel · crackedCRACK AROUND HOLES ACCESS PANEL 561CB TRAILING EDGE AT LT WING 2025-238153<[01] TOOL USED ON STEP 12:ULTRASONIC EQUIPMENT P/N:EPOCH 650; S/N:190984811; DUE DATE:24-FEB-26;[02] TOOL USED: HUMIDITY/TEMPERATURE CHART RECORDER P/N: TH800; S/N: 08193228; DUE DATE: SDR DALA2025040302540Access Panel · worn(LOG 0887767) RH WING FUEL TANK PANEL 632KB CUTOUT HAS WEAR SPOTS. REMOVED EDGE DAMAGE FROM R/H WING FUEL PANEL 632KB CUTOUT IAW B737 SRM 51-10-02-OG. REMOVED 0.014" MATERIAL FROM THE EDGE OF THE R/H WING FUEL TANK PANEL 632K CUTOUT, MAX ALLOWED OF 0.050", FOUSDR DALA2025040302539Access Panel · worn(LOG 0887757) RH WING FUEL TANK PANEL 632LB CUTOUT HAS WEAR SPOTS. REMOVED EDGE DAMAGE FROM R/H WING FUEL PANEL 632LB CUTOUT IAW B737 SRM 51-10-02-OG. REMOVED 0.008" MATERIAL FROM THE EDGE OF THE R/H WING FUEL TANK PANEL 632LB CUTOUT, MAX ALLOWED OF 0.050", FOSDR DALA2025040302538Access Panel · worn(LOG 0887747) RH WING FUEL TANK PANEL 632MB CUTOUT HAS WEAR SPOTS. REMOVED EDGE DAMAGE FROM R/H WING FUEL PANEL 632MB CUTOUT IAW B737 SRM 51-10-02-OG. REMOVED 0.011" MATERIAL FROM THE EDGE OF THE R/H WING FUEL TANK PANEL 632MB CUTOUT, MAX ALLOWED OF 0.050", FOSDR CALA2025040303497Skin · gougedFOR THE INTERIM REPAIR AT RH WING LOWER SKIN EDGE GOUGE DAMAGE AT WSTA 585, ACCOMPLISH PERMANENT REPAIR PER PART 3 OF THE LATEST REVISION OF ECRA #: 5720-03512 ON OR BEFORE 30-SEPT-2026. FOR THE INTERIM REPAIR AT RH WING LOWER SKIN EDGE GOUGE DAMAGE AT WSTA 58SDR DALA2025040202487Skin · crackedSHIP 6712 LEFT UPPPER WING SKIN AT FASTENER HOLE #8 HAS A CRACK INDICATION LOCATED AT THE 4 OCLOCK POSITION (VERIFIED WITH HFEC HOLE SCAN). CORRECTIVE ACTION: REPAIRED HOLE IAW ER/A 625378-14 REV O PRI REV O AND ER/A 625378 -14 REV O PRI REV 1. (0888221)SDR JGVR20250331001Skin · corrodedREPAIRED CORRODED AREA OF THE RIGHT WING LOWER SKIN JUST OUTBOARD OF THE MAIN JACKPOINT BY BLENDING AREA, PERFORMING NDT, REPORTING FOR REPAIR DISPOSITION, CLEANING, TREATING, AND PRIMING REPAIR AREA PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.SDR DALA2025040102413Access Panel · corroded(LOG 0885923) CORROSION AROUND RT OUTBD WING FUEL TANK ACCESS HOLE CUTOUT BETWEEN RIB 12 AND RIB 13. REPAIRED IAW B737 SRM 57-20-01-2R-1.SDR DALA2025040102412Access Panel · corroded(LOG 0885910) CORROSION AROUND RT OUTBD WING FUEL TANK ACCESS HOLE CUTOUT BETWEEN RIB 12 AND RIB 13. REPAIRED AREA ORIG MAT .200" MAT REMOVED .003" MAT REMAINING .197" IAW B737 SRM 57-20-01-2R-1.SDR DALA2025040102411Access Panel · corroded(LOG 0885898) CORROSION AROUND RT OUTBD WING FUEL TANK ACCESS HOLE CUTOUT BETWEEN RIB 14 AND RIB 15. REPAIRED AREA ORIG MAT .200" MAT REMOVED .011" MAT REMAINING .189" IAW B737 SRM 57-20-01-2R-1.SDR DALA2025040102410Access Panel · corroded(LOG 0885889) CORROSION AROUND RT OUTBD WING FUEL TANK ACCESS HOLE CUTOUT BETWEEN RIB 5 AND RIB 6. REPAIRED AREA ORIG MAT .200" MAT REMOVED .013" MAT REMAINING .187" IAW B737 SRM 57-20-01-2R-1.SDR DALA2025040102409Access Panel · corroded(LOG 0885853) CORROSION AROUND RT OUTBD WING FUEL TANK ACCESS HOLE CUTOUT BETWEEN RIB 20 AND RIB 21. REPAIRED AREA ORIG MAT .200" MAT REMOVED .046" MAT REMAINING .154" IAW B737 SRM 57-20-01-2R-1.SDR DALA2025040102408Access Panel · corroded(LOG 0885840) CORROSION AROUND RT OUTBD WING FUEL TANK ACCESS HOLE CUTOUT BETWEEN RIB 21 AND RIB 22. REPAIRED AREA ORIG MAT .200" MAT REM .035" MAT REM .165" IAW B737 SRM 57-20-01-2R-1.SDR 2025FA0000221Skin · debondedLH UPPER WING STRINGER 8 (P/N 6922470-5) WAS FOUND TO BE DEBONDED FROM THE LH UPPER WING SKIN (P/N 7422087-1) AND UPPER OUTBD AFT WAFFLE DOUBLER (P/N 6922387-5) AT CWS 218.00. THE DEBOND AFFECTS THE OUTBOARD MOST 3.05 INCHES OF STRINGER 8. THE UPPER WING SKISDR 2025FA0000220Skin · debondedDISBONDS ON THE UPPER WINGS BETWEEN THE OUTBOARD END OF THE STRINGERS AND THE COMMON SKIN DOUBLERS. THE SKIN AND COMMON DOUBLERS MAY ALSO EXHIBIT A GRADUAL DEVIATION FROM CONTOUR IN THESE REGIONS. THE EXTENT OF THE DEFECT IS LOCATED USING ULTRASONIC INSPECTISDR DALA2025040102437Skin · damagedSHIP 685 CRACK UPPER SKIN ON FIX L/E BTW WS 400-420 AT RH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00053: UPPER SKIN ON FIX L/E BTW WS 400-420 AT RH WING. WAS REPAIRED PER B757-200 SRM 51-70-17-0G PAR. 3. IN REFERENCE B757-200 SRM 57-41-01-2R PROCEDURE 1 REPAIRSDR SWIA20250613328Access Panel · corrodedLH WING FUEL CELL ACCESS PANEL (510AB) LANDING HAS TWO SPOTS OF MINOR CORROSION AT THE 12 O'CLOCK & 3 O'CLOCK POSITION, MEASURING APPROX 2.75 INCHES AND 3 INCHES RESPECTIVELY. (C-CHECK RO 06/12/2025)REPAIRED LH WING FUEL CELL ACCESS PANEL LANDING(510AB) LANDSDR DALA2025041102827Access Door · missingFOUND THAT THE RT WING L/E SLAT MECHANISM LUBRICATION ACCESS DOOR PANEL #621KB WAS MISSING. MAINTENANCE DEFERRED IT TO CDL 57-41-04. ACCESS PANEL P/N 114T2401-10 PNL #621KB WAS NOT IN STOCK AT JFK. ON 03APR25 MAINTENANCE INSTALLED PANEL #621KB IAW B767-300 AMMSDR CALA2025040103397Skin · crackedLEFT WING OUTBOARD LOWER SKIN PANEL CRACK WSTA 564.5 & 591.5 AT STR. L-9 INTERIM REPAIR. INSTALLED REPAIR AT LEFT WING O/B LOWER SKIN PANEL BETWEEN WSTA 564.5 AND 591.5 AT STR L-9 REF.AAR ESR-WI 5-11609 REV. IR AND UNITED EC/RA 5725-01158, THIS IS AN ITERIM RESDR AALA202504011956Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TOP SKIN PANEL OVERHANG LOWER SURFACE AT LEVEL RIB 10. REPAIRED SKIN PANEL PER EA 361777.SDR FDEA202503280526Doubler · crackedRIGHT WING LEADING EDGE COMPARTMENT STATION XOS 627 (PRESSURE REFUEL AREA) BEADED DOUBLER FOUND WITH CRACKS. RIGHT WING LEADING EDGE COMPARTMENT STATION XOS 627 (PRESSURE REFUEL AREA) CRACKED BEADED DOUBLER REPAIR CARRIED OUT AS PER MD 11 SRM 57-40-02-2RSDR DALA2025032802325Skin · corrodedSHIP 3141 CORROSION WAS FOUND IN TOP SKIN PANEL 2, TRAILING EDGE OVERHANG AREA, RH WING. CORRECTIVE ACTION: REPAIRED PER ER/A 624232-14. (0881688)SDR DALA2025032802328Skin · crackedSHIP 5807 CRACK ON FIXED LEADING EDGE OSS 421 AT RH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00062: FIXED LEADING EDGE OSS 421 AT RH WING WAS REPAIRED PER B757-300 SRM 51-70-17-0G IN REFERENCE B757-300 SRM 57-41-01-2R PROCEDURE 1 REPAIR 1 TABLE I. (0879364)SDR CALA2025032803293Access Panel · damagedLEFT WING FUEL TANK ACCESS PANEL 540K B HAS ONE ELONGATED HOLE AT APPROX 7:00 POSTION. REWORKED AND REPAIRED LANDING IAW ECRA 5720-02626 ACP INITIAL RE QUIREMENTS PER PART 2 OF ECRA BEFORE ACFT REACHES 85800T OR 4290 0C WHICHEVER COMES 1ST. ACP REPEAT INSP PERSDR CALA2025032803289Skin · crackedRT WING, UPPER SKIN PANEL NR 1 TE WS 350.95 & WS 374.05, RIB 6 & 7 CRACKED FROM FASTENER HOLE TO TE. VERIFIED CRACK TERMINATES IN HOLE 14 AS IDENTIFIED ON ECRA 5725- 01157. ACCOMPLISHED NDT OF ADDITIONAL HOLES ADJACENT TO HOLE 14. NO DAMAGE PRESENT. PERFORMSDR AALA202503263510Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION RIGHT WING TOP SKIN PANEL OVER HANG LOWER SURFACE AT LEVEL RIB 16. REPAIRED SKIN PANEL PER EA 361778.SDR AALA202503267815Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION RIGHT WING TOP SKIN PANEL OVER HANG LOWER SURFACE AT LEVEL RIB 15. REPAIRED SKIN PANEL PER EA 361778.SDR AALA202504047774Access Panel · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND WING LEADING EDGE UPPER ACCESS PANEL JUST INBOARDOF ENGINE STRUT HAS WEAR MARKS, UPPER SURFACE. REMOVED AND REPLACED RIGHT HAND WING LEADING EDGE UPPER ACCESS (SKIN) PANEL JUST INBOARD OF ENGINE STRUT. PER B737NG SRM 51SDR IPXA2025042095015Skin · corrodedCONDITION EXIST ON RH WING UPPER SURFACE THAT NEEDS TO BE EVALUATED AT BETWEEN RIB 8 TO RIB10, (SPECIAL ATTENTION AT RIB9).REMOVED PAINT ON RH WING UPPER SURFACE BETWEEN RIB 8 TO RIB 10 AREA BY CHEMICAL METHOD USING PAINT STRIPPER P/N: E3000, BATCH: 4342177, ISDR AALA202507157805Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING REAR FALSE SPAR TRAILING EDGE OVERHANG AREA TOP SKIN PANEL LOWER SURFACE AT RIB 19. REPAIRED SKIN PANEL PER EA 363449.SDR AALA202507154344Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING REAR FALSE SPAR TRAILING EDGE OVERHANG AREA TOP SKIN PANEL LOWER SURFACE BETWEEN RIB 17 AND RIB 18. REPAIRED SKIN PANEL PER EA 363449.SDR AALA202507155132Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING REAR FALSE SPAR TRAILING EDGE OVERHANG AREA TOP SKIN PANEL LOWER SURFACE BETWEEN RIB 13 AND RIB 14. REPAIRED SKIN PANEL PER EA 363449.SDR GTIA2025032438812Skin · corrodedCORROSION ON TRAILING EDGE TOP SKIN LOWER SURFACE OVERHANG BTW RIB 5 TO RIB 9 ON RH WING. RAF-01 CREATED AND SDR 3563280-02 LENGTH 5.297"" AND WIDTH 2.383""-PERFORMED PERMANENT REPAIR ON TRAILING EDGE TOP SKIN LOWER SURFACE OVERHEANG BTW RIB 5 TO RIB 9 ON RH WSDR DALA2025032402184Access Panel · corrodedCORROSION ON CONTACT AREA OF FUEL ACCESS PLATE 620QB. ALSO, CORROSION ON FASTENER HOLES OF PLATE 620JB AT RH WING. SUMMARY OF NRC 00604: CORROSION LEVEL 2. ACCESS PLATE 620JB WAS REPLACED AND VERIFIED FOR A NEW ACCESS PLATE PER B717-200 AIPC 57-23-01-01 ITEM 2SDR DALA2025032402183Access Panel · corrodedCORROSION ON COUNTERSINK ON FUEL ACCESS PLATES 620GB, 620HB, 620CB, 620FT, 620DB, AND ARB0872-535 AT RH WING WAS FOUND. SUMMARY OF NRC 00602: CORROSION LEVEL 2. FUEL ACCESS DOORS 620FT AND 620DB WERE REPAIRED PER B717-200 SRM 57-10-01-2R PROCEDURE 2. FUEL ACCESDR AALA202503213918Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN LEFT WING UPPER SKIN AT IRSS 430. REPAIRED PER EA 358887.SDR AALA202507153268Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING REAR FALSE SPAR TRAILING EDGE OVERHANG AREA TOP SKIN PANEL LOWER SURFACE BETWEEN RIB 11 AND RIB 12. REPAIRED SKIN PANEL PER EA 363852.SDR AALA202507156328Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING REAR FALSE SPAR TRAILING EDGE OVERHANG AREA TOP SKIN PANEL LOWER SURFACE BETWEEN RIB 10 AND RIB 11. REPAIRED SKIN PANEL PER EA 363852.SDR AALA202507154452Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING REAR FALSE SPAR TRAILING EDGE OVERHANG AREA TOP SKIN PANEL LOWER SURFACE BETWEEN RIB 7 AND RIB 8. REPAIRED SKIN PANEL PER EA 363852.SDR AALA202507128400Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE OVERHANG TOP SKIN PANEL LOWER SURFACE AT RIB 14 AND THE REAR SPAR. REPAIRED SKIN PANEL PER EA 363852.SDR JGVR20250320006Skin · corrodedREPAIRED THE LH UPPER WING SKIN LOCATED UNDER AND ADJACENT TO THE AFT DRAG ANGLE (WING-TO-FUSELAGE FAIRING STRUCTURE) BY BLENDING CORROSION, PERFORMING NDT, AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS PER TEXTRON FIELD REPAIR BY CLEANING, TREATING, ANDSDR JGVR20250320004Skin · corrodedMECHANICALLY BLENDED CORROSION FROM LH OVER-WING FUEL ADAPTER LAND., PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT BY CLEANING, TREATING, AND PRIMING AREAS.SDR 2025FA0000476Stiffener · crackedRIGHT WING FWD LWR I/B SKIN. AFT STIFFENER CRACKED.SDR VNAA20250320077Access Panel · damagedHN00199778 DISCREPANCY: RH WING PANEL 698AT HAS AN ELONGATED SCREW HOLE. CORRECTIVE ACTION:COMPLIED WITH EA NO: A1-670-57-00075 REV.-- DATED 2024-11-24 REPAIR
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