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 7C7A2025081600038Access Panel · delaminatedRIGHT UPPER WING ACCESS PANEL 611KT FOUND DELAMINATED.SDR CALA2025082007983Skin · crackedON THE LH WING LOWER OUTBOARD SKIN PANEL EXTERNAL REPAIR LOCATED AT STRINGER L-9 AND WSTA 556, SKIN CRACK REPAIRED AT OTBD FASTENER OF STR 9. FLANGE. BETWEEN STA. 564.5 - STA. 537.5. PER ECRA: 5725-01165. ON THE LH WING LOWER OUTBOARD SKIN PANEL EXTERNAL REPASDR DALA2025081806175Skin · corrodedRIGHT WING TOP SKIN PANEL 2 LOWER SURFACE T/E OVERHANG AREA, AT RIB 17 +190MM SKIN WITH CORROSION. PERFORMED REPAIR AT TOP SKIN PANEL 2 LOWER SURFACE, T/E OVERHANG AREA AT RIB 17+410MM (AREA 10) I/A/W ER/A 627459-14AD. (1145846)SDR DALA2025081806174Skin · corrodedLEFT WING, TOP SKIN PANEL 2 LOWER SURFACE, TRAILING EDGE, OVERHANG AREA, WITH CORROSION AT RIB 11 + 115MM. PERFORMED REPAIR BY INSTALLED EXTERNAL REPAIR DOUBLER AT TOP SKIN PANEL 2, T/E OVERHANG AREA AT RIB 11+115MM (AREA 5) I/A/W ER/A 627460-14AD. (1145623)SDR DALA2025081806173Skin · corrodedLEFT WING TOP SKIN PANEL 2 LOWER SURFACE, TRAILING EDGE, OVERHANG AREA AT RIB 11+490MM WITH CORROSION. PERFORMED REPAIR BY INSTALLED EXTERNAL REPAIR DOUBLER AT TOP SKIN PANEL 2, T/E OVERHANG AREA AT RIB 11+490MM (AREA 6) IAW ER/ A NO. 627460-14AD. (1145536)SDR DALA2025081806172Skin · corrodedRIGHT WING TOP SKIN PANEL 2 LOWER SURFACE T/E OVERHANG AREA, AT RIB 14 +45MM SKIN WITH CORROSION. PERFORMED REPAIR AT TOP SKIN PANEL 2 LOWER SURFACE, T/E OVERHANG AREA AT RIB 14+45MM (AREA 6) I/A/W ER/A 627459-14AD. (1145496)SDR DALA2025081806171Skin · corrodedRIGHT WING TOP SKIN PANEL 2 LOWER SURFACE T/E OVERHANG AREA, AT RIB 17 SKIN WITH CORROSION. PERFORMED REPAIR AT TOP SKIN PANEL 2 LOWER SURFACE, T/E OVERHANG AREA AT RIB 17MM (AREA 9) I/A/W ER/A 627459-14AD. (1145479)SDR DALA2025081806170Skin · corrodedRIGHT WING TOP SKIN PANEL 2 LOWER SURFACE T/E OVERHANG AREA, AT RIB 11 +140MM SKIN WITH CORROSION. PERFORMED REPAIR AT TOP SKIN PANEL 2 LOWER SURFACE, T/E OVERHANG AREA AT RIB 11+140MM (AREA 4) I/A/W ER/A 627459-14AD. (1145475)SDR DALA2025081806169Skin · corrodedRIGHT WING TOP SKIN PANEL 2 LOWER SURFACE T/E OVERHANG AREA, AT RIB 11 +500MM SKIN WITH CORROSION. PERFORMED REPAIR AT TOP SKIN PANEL 2 LOWER SURFACE, T/E OVERHANG AREA AT RIB II + 500 (AREA 5) IAW ER/A NO. 627459-14AD. (1145453)SDR DALA2025081806168Skin · corrodedRIGHT WING TOP SKIN PANEL 2 LOWER SURFACE T/E OVERHANG AREA, AT RIB 16 +200MM SKIN WITH CORROSION. PERFORMED REPAIR AT TOP SKIN PANEL 2 LOWER SURFACE, T/E OVERHANG AREA AT RIB 16+200M (AREA 8) IAW ER/A 627459-14AD. (1145364)SDR R61A2025081800345Skin · crackedDURING A PHASE 2 HARD LANDING INSPECTION FOUND LH WING UPPER SKIN CRACKED AT # 3 MULTI-FUNCTION SPOILER ACTUATOR UPPER HINGE POINT APROX 1 INCH IN LENGTH. REPAIRED IAW ETD2025-170-926670 ALSO REF VP-035109-2025 N/R #2 FOR WORK PERFORMED.SDR 7C7A1900010000030Skin · damagedRIGHT WINGTIP HAS LIGHTING STRIKE.SDR IPXA2025090571710Skin · cracked(STR) LH WING L.E. #19 SLAT TRACK CUT OUT O/B SIDE SKIN SURFACE HAS CRACKED AS MARKED.74-016 ATA CODE 57 AUDITED.CUT OUT AND REMOVED THE DAMAGE IN LH WING FIXED L/E AT #19 SLAT TRACK CUT OUT O/B SKIN SURFACE STA XOS=1160 REF. MD-11 SRM 57-40-01-2R-9.FABRICATEDSDR IPXA2025090276350Skin · ground damageFAULT-COMP-Z500- LH WING, SLAT 4 AREA, FIXED L/E SKIN, BY I/B MAIN TRACK, HAS COMPOSITE BROKEN. INSTALLED NEW PANEL ASSY-UPPER SKIN OTBD FIXED L/E. IAW B757-200PF, SRM 51-40-02. REVIEWEDSDR DALA2025081806161Repair · out of positionEXISTING REPAIR FOUND THAT IMPACTS INSPECTION ACCOMPLISHMENT. REPAIR INVESTIGATION REQUIRED PRIOR TO FURTHER FLIGHT. FOUND AT RT WING REAR SPAR INSPECTION AREA DURING ACCOMPLISHMENT OF AA EM 5720-01103. REPAIR PER ER/A 624368-14AD (1143045)SDR DALA2025081506114Skin · corrodedLEFT WING TOP SKIN PANEL 2 LOWER SURFACE, TRAILING EDGE, OVERHANG AREA AT RIB 10 CORRODED. COMPLIED WITH ER/A 627460-14AD.SDR DALA2025081506113Skin · corrodedLEFT WING TOP SKIN PANEL 2 LOWER SURFACE, TRAILING EDGE, OVERHANG AREA AT RIB 14 CORRODED. COMPLIED WITH ER/A 627460-14AD.SDR DALA2025081406089Skin · corrodedSHIP 3146 FOUND THE RH WING TOP SKIN PANEL 2, TRAILING EDGE OVERHANG AREA, LOWER SURFACE WITH CORROSION. CORRECTIVE ACTION: COMPLIED WITH ER/A 627459-14. (1142290).SDR DALA2025081406088Skin · corrodedSHIP 3146 RH WING TOP SKIN PANEL 2 WAS FOUND WITH CORROSION AT LOWER SURFACE TRAILING EDGE OVERHANG AREA. CORRECTIVE ACTION: COMPLIED WITH ER/A 627459-14. (1142287).SDR DALA2025081406087Skin · corrodedSHIP 3146 CORROSION FOUND AT THE RH WING TOP SKIN PANEL 2, TRAILING EDGE OVERHANG AREA, LOWER SURFACE. CORRECTIVE ACTION: COMPLIED WITH ER/A 627459-14. (1142277).SDR DALA2025081406085Skin · corrodedSHIP 3146 FOUND CORROSION AT THE RH WING TOP SKIN PANEL 2, TRAILING EDGE OVERHANG AREA, LOWER SURFACE. CORRECTIVE ACTION: COMPLIED WITH ER/A 627459-14. (1142264).SDR DALA2025081406084Skin · corrodedSHIP 3146 RH WING TOP SKIN PANEL 2, TRAILING EDGE OVERHANG AREA, LOWER SURFACE CORRODED. CORRECTIVE ACTION COMPLIED WITH ER/A 627459-14. (1142256).SDR DALA2025081406083Skin · corrodedSHIP 3146 RH WING TOP SKIN PANEL 2, TRAILING EDGE OVERHANG AREA, LOWER SURFACE FOUND WITH CORROSION. CORRECTIVE ACTION: COMPLIED WITH ER/A 627459-14. (1142252).SDR YENA2025081400836Skin · damagedDURING HEAVY MAINTENANCE: CORROSION OVERHANG LOWER SURFACE BTW RIB 8 TO RIB 9 TRAILING EDGE AREA RH WING (CPCP RELATED); REF AEROMAN N/R 2025-458289, PERFORMED REPAIR OVERHANG LOWER SURFACE BTW RIB 8 TO RIB 9 TRAILING EDGE AREA RH WING IAW EC NO. A25-744-01 ANSDR DALA2025081406071Skin · corrodedSHIP 3146 CORROSION FOUND ON LHWING TOP SKIN PANEL 2, TEOH, UPPER AN LOWER SURFACES. CORRECIVE ACTION: COMPLIED WITH ER/A 627460-14. (1140343).SDR DALA2025081306062Skin · corrodedCORROSION FOUND ON LHWING TOP SKIN PANEL 2 TEOH, UPPER AN LOWER SURFACES. REPAIRED PER ER/A 31-627460.SDR DALA2025081306061Skin · corrodedCORROSION FOUND ON LH WING TOP SKIN PANEL 2 TEOH, UPPER AN LOWER SURFACES. REPAIRED PER ER/A 31-627460.SDR AALA202508132858Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE TOP SKIN PANEL LOWER SURFACE AT RIB 14. REPAIRED SKIN PANEL PER EA 366083.SDR AALA202508133705Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE TOP SKIN PANEL LOWER SURFACE AT RIB 14 PLUS 15 INCHES. REPAIRED SKIN PANEL PER EA 366083.SDR SWAA2025091199671Access Panel · damagedELONGATED HOLE ACCESS PANEL 561CB TRAILING EDGE AT LT WING REPAIRED ACCESS PANEL 561CB TRAILING EDGE AT LT WING IAW SRM 51-70-04-2R-9.SDR SWAA2025081999143Panel · debondedLEFT WING LEADING EDGE PANEL 521TB DISBONDED AT LEADING EDGE<[01] 04 - REPAIRED PER [SRM 51-70-05-2R-6-D00323 (REPAIR 6 - REPAIR OF DAMAGE TO THE EDGEBAND OF A HONEYCOMB PANEL - AIRFRAME - PERMANENT)]SDR ODAR2025080600001Skin · crackedDURING 100HR / ANNUAL INSPECTION FOUND RH INBOARD FLAP COVE SKIN CRACKED ALONG WITH FLAP TRACK RIVETS WORKING OUT. INSPECTED AREA AROUND FLAP AND FOUND THE INBD FLAP TRACK/RIB ASSEMBLY TO BE CRACKED THROUGH.SDR VNAA20251016015Landing · corrodedCORROSION ON SETTLEMENT AREA OF ACCESS PANELS 621AT AND 521AT AT LH/RH WING. CORROSION ON SETTLEMENT AREA OF ACCESS PANEL 621AT RH WING WAS ATTENDED WITH REO 690-57-41-543 REV. - - AND CORROSION ON SETTLEMENT AREA OF ACCESS PANEL 521AT AT LH WING WAS ATTENDEDSDR VGCA20250805028Skin · crackedCRACKED AT THE SLAT HOOK CUT-OUT IN THE AFT CORNER. AT WS 519 ON THE RIGHT WINGSDR FDEA202508051368Skin · puncturedRIGHT HAND WING: LOCATED ALONG OUTBOARD SIDE OF #12 SLAT TRACK, RIGHT HAND LEADING EDGE SKIN AREA FOUND PUNCTURED AND DENTED, ALONG XOS 780. REPAIR CARRIED OUT AT RIGHT HAND WING: LOCATED ALONG OUTBOARD SIDE OF #12 SLAT TRACK RIGHT HAND LEADING EDGE SKIN ASDR IXXA20250805001Skin · corrodedCORROSION ON LEFT WING UPPER SURFACE LOCATED AT WSTA 456.50SDR FDEA202508041384Doubler · no discrepancyEXISTING DOUBLER REPAIR FOUND ON RH O/B FLAP UPR SKIN BTW RIB3~4,S-1.2 ~ FRONT SPAR COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707, INSPSDR SWAA2025082698537Skin · damagedFASTENER HOLE COMMON TO THE FUEL TANK AT STA.663 LBL 60 SHOWS INDICATION OF A DEFECT USING HFEC. (M). HFEC HOLE PROBE INSPECTION OF FASTENER HOLE COMMON TO THE REPAIR AREA PER BOEING NDT MANUAL PART 6;51-00-00 PROCEDURE 16 INDICATES DEFECT. FASTENER HOLE RSDR JR2R20250803057Splice · corrodedOUTBOARD SPLICE DOUBLER AT RH SHEAR PANEL BETWEEN FR87-FR88 AT RBL 36 IS CORRODED OUT OF LIMITS. REPLACEDSDR JR2R20250803908Skin · chafedLEFT HAND WING LEADING EDGE PANEL, ABOVE PYLON, HAS A PREVIOUS REPAIR CHAFED OUT OF LIMITS. REPAIREDSDR JR2R20250803916Skin · chafedRIGHT WING LEADING EDGE PANEL, ABOVE PYLON, HAS A PREVIOUS REPAIR CHAFED OUT OF LIMITS. REPAIRED.SDR IXXA20250803002Skin · corrodedCORROSION ON UPPER SURFACE LEFT WING STA 205.50SDR IXXA20250803001Skin · corrodedTWO AREAS OF CORRSION ON LEFT WING UPPER SURFACE AT WING STA 451.50,SDR SWIA2025102000802Landing · corrodedINDICATIONS NOTED AT LH WING ACCESS HOLE LANDING COMMON TO PANEL 550DB APPROX. 70% FULL SCREEN HEIGHT, FAILING NDT. INDICATION AREA MARKED ON A/C. (C-CHECK RO 10/19/2025)REMOVED CORROSION FROM 550DB LANDING IAW REO 601R-57-21-030 REV. L, DATED 2014-02-05 ANSDR SWIA20251002802Skin · dentedRH LEADING EDGE 620JL HAS DENT (4.5" X 2.5" X 5/32") ON NOSE @ APPROX. WS.96.34. (FILED CLOSED)REMOVED AND REPLACED THE RH WING LEADING EDGE SKIN FROM WS 86.450 TO WS 139.54 IN REFERENCE WITH THE SRM 51-42-06, SRM 51-40-11 AND SRM 57-41-31. COMPLIED WITH TASSDR AALA202508187422Access Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING FUEL TANK ACCESS PANEL 540KB. REPLACED FUEL TANK ACCESS PANEL 540KB.SDR SWIA2025102000801Skin · corrodedCORROSION AROUND WING PLANK OF ACCESS 510AB. CORRECT LOCATION OF CORROSION IS AROUND ACCESS PANEL 610AB. REMOVED CORROSION AROUND WING PLANK ACCESS PANEL 610AB IAW BOMBARDIER REO 601R-57-21-030. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORMSDR SWAA2025091197597Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 661AB TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661AB TRAILING EDGE AT RT WING IAW SRM 51-70-04-2R-10 REPAIR 10.SDR DALA2025080105757Skin · crackedCRACK FOUND IN HOLE 6 AT 7 O'CLOCK POSITION IN SKIN LAYER JUST ABOVE SHIM LAYER. FURTHER INSPECTION AND REPAIR REQUIRED PRIOR TO FURTHER FLIGHT. SEE NR FOR ADDITIONAL INFORMATION 010-0001:5720-01100-04B/001 00001, COMPLIED WITH E/RA 589741-14AD REV. D.SDR JJBA20251111059Access Panel · corrodedR/H WING FUEL ACCESS PANELS AND CLAMP RINGS:641BB, 631CB, 156CZ, 651AB, 641CB, 641EB, 641DB, 631DB, 631BB, 631AB, AND 641AB HAVE CORROSION AND FRETTING DAMAGE (PITTING). PERFORMED CORROSION REMOVAL PROCESS ON RH FUEL ACCESS DOOR PANEL 641CB, 641EB, 641DB, 631D
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