JASC 5730
Service difficulty reports · 27,254
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 F3LA202603020374Access Panel · missingAIRCRAFT GROUNDED DUE TO EVENT-REFERENCE LP664307, ITEM 1. PANEL MISSING UNDER LEFT WING (AILERON PANEL). INSTALLED NEW ACCESS PANEL (575KB), PER AMM 57-51-37-400-005-A.SDR R61A2026030200055Skin · crackedDURING OVERNIGHT INSPECTION FOUND RH WING LOWER SKIN CRACKED BETWEEN RIB 16 AND RIB 17 JUST AFT OF FWD SPAR APROX 27.94 MM LONG.REPAIRED IAW EMB ETD2026-170-003614,INSTALLED FILLER,DOUBLER AND TRIPLER. ALSO REF VP-005555-2026 FOR WORK ACCOMPLISHED.SDR SWAA2026031373999Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 561BB, LT WING. REPAIRED THE ACCESS PANEL 561BB IAW SRM 51-70-04-2R-10, REPAIR 10.SDR SWIA2026022376132Skin · chafedRT LOWER WING PLANK IS CHAFED AT RBL45. COMPLIED WITH REPAIR TO LOWER WING PLANK CHAFE AT RBL45 IAW REO 601R-57-21-880 REV -D DATED 2017-03-06.SDR SWIA2026022376121Skin · chafedLEFT LOWER WING PLANK IS CHAFED AT LBL45. COMPLIED WITH BLEND REPAIR TO LOWER WING PLANK CHAFE AT LBL45 IAW REO 601R-57-21-880 REV -D DATED 2017-03-06.SDR R61A2026031100061Skin · crackedWHLE ON HEAVY CHECK - RH WING LOWER INTERNAL AND EXTERNAL SKIN WAS FOUND CRACKED AT RIB 12 BETWEEN SPEAR 1 AND STRINGER 18-19. SEEN THROUGH PANEL 631 AB AND WAS CONFIRMED WITH HFEC.SDR JR2R20260222854Panel · corroded633FB HAS EVIDENCE OF CORROSION. REPAIREDSDR MAS2026F00002Panel · corroded633FB HAS EVIDENCE OF CORROSION. REPAIRED.SDR SWAA2026031972755Access Panel · damagedELONGATED HOLE ON LT WING ACCESS PANEL 561AB. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-10, REPAIR 10.SDR HNAA2026032600238Skin · corrodedLEFT MAIN LANDING GEAR BAY LOWER SKIN FWD OF MAIN LANDING GEAR MAIN SIDE STRUT CORRODED. R & R THE LT MAIN LANDING GEAR BAY LOWER SKIN FWD OF THE MAIN LANDING GEAR SIDE STRUT IAW SRM 51-40-02.SDR REXA2026080601511Access Panel · corrodedCORROSION ON ACCESS PANELS 542AZ, 542BZ, 642BZ AND 642AZ (BOTH SIDES) CORROSION ON ACCESS PANELS 542AZ, 542BZ, 642BZ WAS REMOVED PER CRJ900 SRM 51-21-06-001-001-A01 AND WERE EVALUATED WITHIN LIMITS PER CRJ-900 SRM 57-22-32-101-001-A01, AND PANEL 642AZ WAS REPLSDR SWAA2026031972060Access Panel · damagedELONGATED HOLE ON THE RT WING T/E ACCESS PANEL 661AB. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-9, REPAIR 9.SDR SWAA2026031972061Access Panel · damagedELONGATED HOLE ON THE RT WING ACCESS PANEL 661CB TRAILING EDGE. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-9, REPAIR 9.SDR JR2R20260218666Skin · chafedLEFT WING FIXED LEADING EDGE JUST OTBD OF WING, LANDING LIGHT FAIRING HAS SEVERAL CHAFES . REPAIREDSDR JR2R20260218600Skin · chafedLEFT WING FIXED LEADING EDGE OVER PYLON CHAFED. REPAIREDSDR 2026FA0000132Skin · debondedDISBONDS ON THE UPPER WINGS BETWEEN THE OUTBOARD END OF 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 INSPECTION ANDSDR CALA2026021813859Cover · missingDURING WALK AROUND FOUND PANEL COVER MISSING FROM RT WING LEADING EDGE. OTBD OF RT ENGINE. OPEN.SDR JR2R20260217541Panel · chafedWING PANEL 651AB HAS CHAFING AT EDGE OF PANEL. REPAIRED.SDR JR2R20260217608Skin · chafedRIGHT WING FIXED LEADING EDGE OVER PYLON CHAFED. REPAIREDSDR SWIA2026021675842Skin · gougedRH WING INBOARD FLAP UPPER INTERNAL SKIN HAS MULTIPLE GOUGES UNDER PANEL 684AB. REMOVED MULTIPLE GOUGES AND RESTORED AREA AT RH WING INBOARD FLAP UPPER INTERNAL SKIN UNDER PANEL 684AB REF SRM 51-12-00, COMPLIED WITH ALL THE STEPS OF THE REO 601R-57-52-2543 RESDR SWAA2026032371280Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 661BB AT RT WING T/E. REPAIRED THE ACCESS PANEL 661BB IAW SRM 51-70-04-2R-10, REPAIR 10 .SDR SWAA2026032371282Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 561BB AT LT WING. REPAIRED ACCESS PANEL 561BB AT LT WING IAW SRM 51-70-04-2R-10 REPAIR 10.SDR SWAA2026032371375Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 661BB AT RT WING. REPAIRED THE ACCESS PANEL 661BB AT RT WING IAW SRM 51-70-04-2R-10 REPAIR 10.SDR GTIA2026021639283Skin Panel · corroded"CORROSION LOWER SURFACE EXTERNAL SKIN LOCATED RIB18 TO RIB19 ON LH WING RAF 6000549-01 CREATED-PERFORMED REPAIR LOC LOWER SURFACE EXTERNAL SKIN LOCATED AT LEVEL RIB 18 TO RIB 19 AT LH WING IAW EA # 57-0013-26. THIS REPIAR AN INTERIM APPROVAL WITH NO REPAIR CASDR GTIA2026021639282Access Panel · corrodedCORROSION INTERNAL AREA THE OF ACCESS PANEL 574AB LOCATED RIB 5 TO RIB B6 ON LH WING (CPCP FINDING ) RAF 6000549-02 CREATED-PERFORMED PERMANENT REPAIR INTERNAL AREA OF ACCESS PANEL 574AB AT LEVEL RIB5 TO RIB6 AT LH WING IAW EA # 53-0016-26SDR YENA2026021800211Skin · damagedDURING HEAVY MAINTENANCE: ELONGATED HOLE EXTERNAL SKIN LOWER SURFACE OF CUT OUT FUEL TANK AREA BT W RIB16 TO RIB17 ON RH WING; REF AEROMAN NR 2026-39866 WO 2026 25/1 JB NR-0042 WO 1441774 FUR A320-57-02978.SDR YENA2026021800210Skin · damagedDURING HEAVY MAINTENANCE: ELONGATED HOLES AT 2 LOCATION, BOTTOM SKIN EXTERNAL SURFACE OF CUT OUT FUEL TANK AREA BTW RIB 16 TO RIB 17 ON RT WING; REF AEROMAN NR 2026-40034 WO 2026 25/1 JB NR-0043 WO 1441774 FUR A320-57-02979.SDR SWAA2026032370182Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 661BB AT RT WING. REPAIRED ACCESS PANEL 661BB IAW SRM 51-70-04-2R-10, REPAIR 10.SDR SWIA2026021275427Skin · crackedSUSPECTED SKIN CRACK L/H WING AT WHEEL WELL CUTOUT FORWARD EDGE AT WHEEL WELL RIB 3 LOCATION REPAIRED DAMAGE BY CUTTING OUT THE DAMAGE AND INSTALLING TRIPLER/ DOUBLER TO L/H WING AT WHEEL WELL CUT OUT FWD EDGE AT WHEEL WELL RIB 3. SEE CONTINUATION CARD FOR WSDR SIMA20260211001Skin · crackedAPPROXIMATELY TWO INCH CRACK ON RT WING LOWER SKIN, JUST AFT OF SPAR 1 AND INBD OF RIB 17. PERFORMED HFEC AND VERIFIED CRACK IAW NDTM ET0400-1. PERFORMED HFEC AND VERIFIED CRACK IAW ENVOY NDTM ET0400-1. (REF. NRWC# 794-MQT-02139) "TRANSFERRED FROM AML PAGE 1SDR SWAA2026021269501Winglet · delaminatedBULGE FOUND ON LT WINGLET, BLENDED THE WINGLET SKIN DELAMINATION, 36 INCHES FROM TOP EDGE AND 6 INCHES FROM L/E, MEASURES 12 IN X 4 IN; PROTRUDING 0.031 INCH. LOCATED IN HONEYCOMB SKIN PANEL ZONE 3, EXCEEDS ALLOWABLE DELAMINATION LIMITS IAW AP37.1-0632, SRSDR VNAA202602090001Access Panel · damagedA1-670-57-00012 (2,843.35FH PERM REPAIR - PANEL, ACCESS, FIXED L/E, TR 13 (RH) PANEL 622EB - SPEED TAPE APPLIED) WITHIN 2843.35 FLIGHT HOURS AFTER SECTION I, REPAIR, OR REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES CC670-10044 LWR WING PSDR SWAA2026031369628Access Panel · damagedELONGATED HOLES ACCESS PANEL 561BB AT LT WING. REPAIRED THE ACCESS PANEL 561BB IAW SRM 51-70-04-2R-10, REPAIR 10.SDR FDEA202602090152Skin · crackedDURING WORK CARD: EG-5710-E0376285F P12 STEP3.B(1) & 5.A.(2), FOUND TWO CRACKS ON RT UPPER WING SKIN FASTENER NR 5. RIGHT WING UPPER SKIN NR 5 FASTENER HOLE REPAIRED IAW SRM 51-40-05-0G, FIGURE 4, TABLE C, SRM 51-40-02-0G, FIGURE 12, SRM 51-40-04-0G, FIGURE 2SDR FDEA202602090151Skin · crackedDURING WORK CARD: EG-5710-E0376285F P12 STEP4.B(2).(B), THEN FOUND ONE CRACK ON RT UPPER WING SKIN FASTENER #6 AS MARKED. RIGHT WING UPPER SKIN NR 6 FASTENER HOLE REPAIRED IAW SRM 51-40-05-0G, FIGURE 4, TABLE C , SRM 51-40-02-0G, FIGURE 12, SRM 51-40-04-0G, SDR FDEA202602090150Skin · crackedDURING WORK CARD: EG-5710-E0376285F P11 STEP4.B(2).(B), THEN FOUND ONE CRACK ON LT UPPER WING SKIN FASTENER NR 6. THE LEFT WING UPPER SKIN #6 FASTENER HOLE CRACKED AREA REPAIRED AS PER B777 SRM 51- 20-07-0G FIGURE 2, SRM 51-50-02-0G FOGURE 1, SRM 51-40-02SDR FDEA202602090149Skin · crackedDURING WORK CARD: EG-5710-E0376285F P11 STEP3.B.(1) & 5.A.(2) THE FOUND TWO CRACKS ON LT UPPER WING SKIN FASTENER NR 5. THE LEFT WING UPPER SKIN NR 5 FASTENER HOLE CRACKED AREA REPAIRED IAW SRM 51- 20-07-0G, FIGURE 2, SRM 51-50-02-0G, FIGURE 1, SRM 51-40-02-0SDR YENA20260210001Skin · corrodedDURING HEAVY MAINTENANCE: RT WING TOP SKIN PANEL CORRODED /1/ - AIRBUS DOSSIER 81709907 /2/ - AIRBUS RDAF REF. & ISSUE.: 81709907/003/2025 ISSUE A /3/ - AIRBUS RI R572-44701 ISSUE B /4/ - AIRBUS RI R572-58616 ISSUE N /5/ - AIRBUS RI R572-58926 ISSUE E /6/ - ASDR SWIA2026020875711Skin · chafedLOWER WING PLANK ACCESS HOLE AT 510BB, AFT LANDING CHAFED(MARKED WITH TAPE). PERFORMED A MAJOR REPAIR BY BLENDING CORROSION ON LOWER WING PLANK ACCESS HOLE AT 510BB LANDING IAW REO 601R-57-21-030 REV L DATED 2014-02-05. COMPLETED SKYWEST TASK CARD 51-900-1SDR SWAA2026031369060Access Panel · crackedCRACKED ACCESS PANEL 644BB INNER SURFACE. REPAIRED THE ACCESS PANEL 644BB IAW 26-157-00475-WIP1.SDR SWAA2026031269045Access Panel · crackedCRACKED ACCESS PANEL 544BB, LT WING. REPAIRED THE ACCESS PANEL 544BB IAW EA 26-157-00484.SDR YENA2026021100174Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION UPPER SURFACE TRAILING EDGE LOWER AREA OF SKINAT LEVEL RIB 15 ON RH WING; REF AE WO # 2025-414/1 NR # 2025-716959 ACCOMPLISHED PERMANENT REPAIR ON RH WING/TOP SKIN PANEL 2 / TEOH LWR SURFACE / RIB 15 I.A.W EA 57-0135-25(COVESDR YENA2026021100173Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION UPPER SURFACE AT LEVEL RIB 8 TO RIB 9 TRAILING EDGE ON RH WNG; REF AEROMAN WO 2025-414/1 NR # 2025-716950 ACCOMPLISHED REPAIR OF CORROSION DAMAGE AT RH WING/TOP SKIN PANEL 2 / TEOH LWR SURFACE / RIB7-RIB9 I.A.W EA 57-0135-2SDR YENA2026021100172Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE UPPER SKIN LOWER AREA BTW RIB8 TO RIB 9 ON RH WING; REF AEROMAN WO # 2025-414/1 NR # 2025-717170 PERFORMED PERMANENT REPAIR ON TRAILING EDGE UPPER SKIN LOWER AREA ON RIB 8 RH WING IAW EA # 57-0135-25 (COVER ANDSDR YENA2026021100171Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION TE UPPER SKIN LOWER AREA SURFACE AT LEVEL RIB 7 ON RT WING; REF AEROMAN WO #2025-414/1 NR # 2025-717174, PERFORMED PERMANENT REPAIR ON TE UPPER SKIN LOWER AREA SURFACE AT LEVEL RIB 7 ON RT WING IAW EA 57-0135 -25 (COVER PARTSDR YENA2026021100169Skin · corrodedDURING HEAVY MAINTENANCE: RT WING TOP SKIN PANEL CORRODED /1/ - AIRBUS DOSSIER 81709907 /2/ - AIRBUS RDAF REF. & ISSUE.: 81709907/003/2025 ISSUE A /3/ - AIRBUS RI R572-44701 ISSUE B /4/ - AIRBUS RI R572-58616 ISSUE N /5/ - AIRBUS RI R572-58926 ISSUE E /6/ - ASDR SWAA2026031368844Access Panel · damagedELONGATED HOLE ON ACCESS PANEL 661BB, RT WING[01] STEP 12. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-10, REPAIR 10.SDR IPXA2026030564510Skin · crackedCRACK LEFT WING LEADING EDGE UPPER FIXED PANEL. REPAIRED I.A.W AMM 27-81-03-402-019 REV.115 STEP 3.A TO 3.F. INSTALLED THE L2 PDU CHECK OKSDR IXXA2026020605Skin · corrodedCORROSION ON THE UPPER EXTERIOR SURFACE OF THE RIGHT WING UPPER SKIN, LOCATED FWD OF THE RIGHT AILERON.SDR SWIA2026020576882Skin · dentedDENT 28.5" FROM RT WING IBD FLAP OTBD EDGE & 5.75" FROM TE ON UPPER SKIN. DENT FOUND TO BE 1.2" X 1" AT A DEPTH OF 0.028". REPAIRED THE RT WING INBD FLAP OTBD EDGE AND 5.75 FROM TE ON UPPER SKIN IAW REO 601R-57-52-2555, REV--. APPLIED SURFACE FINISH IAW S
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