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 SWAA2025121146102Panel · pulledPANEL 561CB HAS SEVERAL PULLED THROUGH HOLES. DAMAGE OUTSIDE OF ALLOWABLE LIMITS, SANDED AND CLEANED AREAS OF PANEL IN PREPARATION FOR REPAIR IAW SRM 57-51-01-1A-1, SRM 57-51-01-2R-1, AND SRM 51-70-05-2R-8. REPAIRED AREAS WHERE DAMAGED IAW SRM 57-51-01-2RSDR UIEA2025111801308Skin · corrodedCORROSION ON LT WING UPPER SKIN LOWER SURFACE AT WS 1538. REMOVED THE AFFECTED FASTENER IAW SRM 51-40-02-0G-0 REV 62. BLENDED OUT THE DAMAGED AREA IAW SRM 51-10-02-0G-0 REV 62. PERFORMED NDT INSPECTION, REFER TO DATA SHEET 11633434-1 & DATA SHEET 11633434-2SDR SWIA2025112400019Winglet · dentedRIGHT WINGLET AFT DENT ABOVE RIB 9 MEASURING APPROXIMATELY 7.0" LONG 2.5" WIDE AND .070 DEEP.CREATED FROM FORWARD DISCREPANCY. REPAIRED RIGHT WINGLET ABOVE RIB 9 IAW ETD 2025-170-932587 REV. A,SDR AALA202511202545Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TOP SKIN PANEL OVERHANG LOWER SURFACE BETWEEN RIB 7A AND RIB 9. REPAIRED SKIN PANEL PER EA 368796.SDR 2025FA0000772Skin · corrodedCORROSION FOUND ON TOP OF BOTH WINGS FWD OF SPEED BRAKESSDR DALA2025111908458Skin · dentedDENT WAS FOUND ON LH WING PANEL 2 UPPER SURFACE AT RIB 22 AND STR 16LH. COMPLIED WITH ER/A 629925-14. (1310683).SDR AALA202511195066Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TOP SKIN PANEL OVERHANG LOWER SURFACE AT LEVEL RIB 15. REPAIRED SKIN PANEL PER EA 368796.SDR SWAA2025121847479Access Panel · elongatedELONGATED HOLES ON ACCESS PANEL 561CB TRAILING EDGE AT LT WING. REPAIRED THE ACCESS PANEL 561CB TRAILING EDGE AT LT WING IAW SRM 51-70-04-2R-10, REPAIR 10.SDR SWAA2025121835981Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 561CB TRAILING EDGE AT LT WING. REPAIRED ACCESS PANEL 561CB TRAILING EDGE AT LT WING IAW SRM 51-70-04-2R-10, REPAIR 10.SDR WX0A2025121032662Access Panel · damagedTHE ACFT WAS NOT GROUNDED. MAJOR REPAIR. PANEL 540KB MANHOLE COVER FASTENER AREA HAS 4 ELONGATED HOLES, IAW ERO A32X-STR-57ERO-00447. COMPLETED WORK STEPS PARA A. .REPAIRED MOUNTING HOLE NR 1 USING SRM 57-21-11-300-002. DAMAGED FULLY REMOVED. REPAIRED SDR JR2R20251117478Skin · chafedRIGHT HAND WING LEADING EDGE PANEL, ABOVE PYLON, HAS AN EXISTING REPAIR CHAFED OUT OF LIMITS.SDR JR2R20251117477Skin · chafedLEFT HAND WING LEADING EDGE PANEL, ABOVE PYLON, HAS AN EXISTING REPAIR CHAFED OUT OF LIMITS.SDR JGVR20251117005Doubler · corrodedBLENDED AREAS OF CORROSION ON RT WING FUEL FILLER ASSEMBLY DOUBLER PERFORMED NDT, AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED AREA PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.SDR JGVR20251117001Skin · corrodedMECHANICALLY REMOVED CORROSION LOCATED ON THE LT LOWER WING SKIN AT WS.294 PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED TREATED AND PRIMED REPAIR AREAS PER REQUEST FOR TECHNICAL SERVICES REPORT.SDR SWAA2025121847461Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 661AB AT RT WING. REPAIRED ACCESS PANEL 661AB AT RT WING IAW SRM 51-70-04-2R-10, REPAIR 10.SDR SWAA2025121835360Access Panel · elongatedELONGATED HOLES 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 SWAA2025121835359Access Panel · elongatedELONGATED HOLES ON ACCESS PANEL 661AB AT RT WING. REPAIRED ACCESS PANEL 661AB AT RT WING IAW SRM 51-70-04-2R-10, REPAIR 10.SDR IXXA03062026CC01Skin · corrodedRIGHT WING LOWER SURFACE (INSPAR) IS CORRODED AROUND FASTENER AND RUNS UNDER PYLON RIGHT AT I/B SIDE OF PYLON APROX 5 INCHES AFT OF FWD SPAR AT STRINGER 14.SDR JGVR20251113002Skin · corrodedFOUND CORROSION ON THE UPPER INBOARD WING SKINS LOCATED ALONG AND UNDER THE DRAG ANGLES (FUSELAGE TO WING FARING ATTACH STRUCTURE), REMOVED THE DRAG ANGLES, BLENDED CORROSION, REPORTED FOR REPAIR DISPOSITION. REPLACED BLENDED FASTENERS AS REQUIRED, CLEANED TRESDR SWAA2025120234461Access Panel · elongatedELONGATED HOLES ACCESS PANEL 561BB AT LT WING. REPAIRED ACCESS PANEL 561BB TRAILING EDGE AT LT WING IAW SRM 51-70-04-2R-10 REPAIR 10.SDR AALA202511187841Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TOP SKIN PANEL UPPER SURFACE AT RIB 14. REPAIRED SKIN PANEL PER EA 368862.SDR AALA202511135613Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TOP SKIN PANEL UPPER SURFACE AT RIB 5 AND THE REAR SPAR. REPAIRED SKIN PANEL PER EA 368796.SDR JGVR20251112001Skin · corrodedFOUND 5 AREAS OF CORROSION ON THE UPPER SURFACE OF THE LH UPPER WING SKIN AND 2 AREAS ON THE UPPER SURFACE OF THE RH UPPER WING SKIN, MECHANICALLY BLENDED CORRODED AREAS, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. FABRICATED AND INSTALLED REPAIR DOUBLSDR SWAA2025120234034Access Panel · elongatedELONGATED HOLE ACCESS PANEL 661BB TRAILING EDGE RT WING. REPAIRED ACCESS PANEL 661BB TRAILING EDGE AT RT WING IAW SRM 51-70-04-2R-10 REPAIR 10.SDR DALA2025111208292Skin · damagedELONGATED HOLE FUEL TANK CUT OUT LOWER SURFACE LOC. BTW RIB17/18 (1E/A ) ON RT WING. PERFORMED PERMANENT REPAIR ON FUEL TANK CUT OUT LOWER SURFACE AS PER A319 SRM 57-21 -11-300-002. (1299055).SDR JGVR20251111001Skin · corrodedREPAIRED CORRODED AREA ON THE LOWER WING SKIN IN THE RH LANDING GEAR WELL, BY BLENDING, PERFORMING NDT, REPORTING FOR REPAIR DISPOSITION, FABRICATING AND INSTALLING REPAIR DOUBLER PER ENGINEERING ORDER.SDR JGVR20251110002Skin · corrodedBLENDED 7 AREAS OF CORROSION PLUS 1 ADDITIONAL AREA LOCATED ON RH UPPER WING SKIN AT WS 294 TO THE WING TIP, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED AND PRIMED AREAS NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.SDR JR2R20251110472Skin · chafedLEFT HAND WING LEADING EDGE PANEL, ABOVE PYLON, HAS A PREVIOUS REPAIR CHAFED OUT OF LIMITS. REPAIREDSDR SWAA2025121033221Access Panel · damagedELONGATED HOLE ACCESS PANEL 651FB TRAILING EDGE LOCATED ON STIFFENER RT WING. REPLACED BEAM ON ACCESS PANEL 651FB TRAILING EDGE LOCATED ON STIFFENER RT WING IAW SRM 51-40-02 AND SRM 51-10-02, PARAGRAPH 9, AND DWG 115A2710 SHEET 9, REV A.SDR DALA2025111108221Skin · corrodedCORROSION BOTTON SKIN LOWER SURFACE ON PYLON REINFORCING PLATE BTW RIB 7 AND RIB 8 AT STR 6, LT WING. COMPLIED WITH ER/A 630034-14AD REV.ORIGINAL MATCHES WITH ALL STEPS ON ER/A 630034-14AD PRI REV.0 AND ER/A 630034-14AD PRI REV .1IT HAS BEEN VALIDATED. PERFOSDR JR2R20251109473Skin · chafedRIGHT HAND WING LEADING EDGE PANEL, ABOVE PYLON, HAS A PREVIOUS REPAIR CHAFED OUT OF LIMITS. REPAIRED .SDR ABXA20251108293Skin · corrodedDURING C-CHECK AT AMES (TPA) CORROSION WAS OBSERVED ON THE RIGHT-WING UPPER SURFACE SKIN PANEL NUMBER 1 ON STA WS 616 , THE DAMAGE WAS REMOVED BY BLENDING AFFECTED AREA PER SRM 51-10-02 WITH MEASURED MATERIAL REMAINING OF 0.133¿ INCHES FROM INITIAL THICKNESS OSDR ABXA20251108292Skin · corrodedDURING C-CHECK AT AMES (TPA) CORROSION WAS OBSERVED ON THE LEFT-WING UPPER SURFACE SKIN PANEL NUMBER 1 AT WS 434 OVER UPPER RIB FLANGE P/N 113T1545-7, THE DAMAGE WAS REMOVED BY BLENDING AFFECTED AREA PER SRM 51-10-02 WITH MEASURED MATERIAL REMAINING OF 0.145¿ SDR SWAA2025121532658Access Panel · damagedELONGATED HOLE ON ACCESS PANEL 661CB TRAILING EDGE ON RT WING. REPAIRED THE ACCESS PANEL 661CB TRAILING EDGE IAW SRM 51-70-04-2R-10, REPAIR 10.SDR SWAA2025121532659Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 661AB ON RT WING. REPAIRED ACCESS PANEL 661AB IAW SRM 51-70-04-2R-10, REPAIR 10.SDR SWAA2025121532661Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 661BB ON RT WING. REPAIRED THE ACCESS PANEL 661BB IAW SRM 51-70-04-2R-10, REPAIR 10.SDR AALA202511072817Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE TOP SKIN PANEL UPPER SURFACE AT RIB 4 AND S17. REPAIRED SKIN PANEL PER EA 368862.SDR IPXA2025120726859Skin · damagedLEFT WING SKIN FASTENER HOLE COMMON TO UPPER DRAG FITTING HOLE DIAMETER NOT CONSISTANT THROUGH PART STACK UP , IDENTIFIED AS HOLE NR 3 . VERIFIED STEP 57 IAW GMM RII 04-02. ACCOMPLISH REPAIR IAW EO-95919-REQ1 AND VT-SAA EA 757-5700-01-B0643, REV. IR, PRIOR TOSDR AALA202511142117Access Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING FUEL TANK ACCESS PANEL 640JB. REPLACED ACCESS PANEL PER TASK CARD 26C64057020.SDR IXXA20251105002Skin · corrodedRIGHT WING LOWER SURFACE SKIN PANEL NO 1, WSTA 95.0-177.5 CORROSION GRID NR 2.SDR IXXA20251105001Skin · corrodedRIGHT WING LOWER INBD SURFACE, AFT OUTBD OF FUSELAGE HAS AREA OF CORROSION WSTA, 95.0-177.5SDR SWAA2025121531620Access Panel · crackedCRACKED ACCESS PANEL 561BB ON LT WING. REPAIRED THE ACCESS PANEL 561BB IAW SRM 51-70-04-2R-10, REPAIR 10.SDR SWAA2025121031762Access Panel · delaminatedDELAMINATED ACCESS PANEL 542EB AT LT WING. REPLACED BY A NEW ACCESS PANEL 542EB IAW AMM 27-51-18-400-802, STEP 5.G(5).SDR SWAA2025121046456Access Panel · delaminatedDELAMINATED ACCESS PANEL 542EB AT LT WING. REPLACED DELAMINATED ACCESS PANEL 542EB DUE TO WAS FOUND OUT OF LIMIT IAW AMM 27-51-18-400-802 STEP 5.G5.SDR JGVR20251104001Skin · corrodedREPAIRED CORRODED AREA OF LH LOWER WING SKIN NEAR CWS 537.40 BY BLENDING AREA, PERFORMING NDT, REPORTING FOR REPAIR DISPOSITION, FABRICATING AND INSTALLING REPAIR DOUBLER IN ACCORDANCE WITH ENGINEERING REPAIR ORDER.SDR CALA2025110610977Skin · crackedCRACK INDICATION AT THE MOST OTBD FASTENER HOLE AT STR 9 ON THE RT WING LOWER SKIN APPROX .75" IN LENGTH AT THE 6 O'CLOCK POSITION LOOKING AFT. REPAIRED RT WING LOWER SKIN IAW REO G25610, REV IR, AND EC/RA 5720-03575. MAJOR REPAIR.SDR R61A2025110600489Skin · crackedDISCOVERED LT WING LOWER SKIN CRACKED BETWEEN RIBS 16 & 17, JUST AFT OF FWD SPAR. REPAIRED IAW ETD2025-170-931566, REF VP-047362-2025 NR 2 FOR WORK ACCOMPLISHED.SDR SWIA2026031875545Skin · chafedRIGHT LOWER WING SKIN CHAFED UNDER PANEL 686AB. REPAIRED THE RIGHT LOWER WING SKIN CHAFED UNDER PANEL 686AB IAW REO 601R-57-21-4005, REV-.SDR SWAA2025112831022Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 561BB TRAILING EDGE AT LT WING. REPAIRED ACCESS PANEL 561BB TRAILING EDGE AT LT WING IAW SRM 51-70-04-2R-10 REPAIR 10.SDR AALA202511208039Access Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING FUEL TANK ACCESS PANEL 540JB COUNTERSUNK FASTENER HOLES. MAINTENANCE REPLACED LEFT WING FUEL TANK ACCESS PANEL 540JB PER SRM 57-27-11.
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