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.

SDR SWIA2026032075561Skin · damagedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA105760-REO 601R-57-51-1083 N976SW MXCODEID116263-PR - COMPLY WITH PERMANENT REPAIR ON RA ID: 105760. MISDRILLED HOLE AND MISSING RIVET ON WING T/E UPPER SKIN AT SS 241.80, LT. COMPLIED WITH TEMP REPAIR IAW REO 601R-57-Mar 20, 2026 · N976SW · Cndair CL6002B19SDR CALA2026032314744Skin · crackedLEFT WING LOWER SKIN CRACKED, AFT OF PANEL 543BB CUTOUT. CRACK IS FROM AFT EDGE OF PANEL 543BB TO THE AFT FASTENER ROW IN REAR SPAR. REPAIR PERFORMED ON LT WING LOWER SKIN ON IAW ECRA 5720-03630.Mar 20, 2026 · N14115 · Boeing 757224SDR SWIA2026062676323Skin · corrodedLBL 45 LT WING LOWER PLANK TRAILING EDGE AREA, CORRODED & CHAFED FROM THE WING TO BODY FAIRING. REPAIRED LBL 45 LT WING LOWER PLANK TRAILING EDGE AREA IAW GREO 601R-57-21-880, REV-D. NOTES/STEPS 1, 2, 3,5,6,7,9 AND10.,COMPLIED WITH 51-900-1003-SKY, FUEL LEAK CMar 19, 2026 · N951SW · Cndair CL6002B19SDR SWAA2026042281589Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 661AB TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661AB TRAILING EDGE AT RT WING IAW B737-700 SRM 51-70-04-2R-10.Mar 19, 2026 · N927WN · Boeing 7377H4SDR SWAA2026042281591Access Panel · elongatedELONGATED HOLES ON ACCESS PANEL 661BB TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661BB IAW SRM 51-70-04-2R-10 REPAIR 10.Mar 19, 2026 · N927WN · Boeing 7377H4SDR AALA202604212747Access Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING FUEL TANK ACCESS PANEL 640NB COUNTERSINK HOLE. MAINENANCE REPLACED FUEL TANK ACCESS PANEL PER TASK CARD 26C64057007.Mar 19, 2026 · N194UW · Airbus A321211SDR SWAA2026033081537Panel · crackedLEFT WING INBD FIXED T/E LOWER PANEL CRACKED AROUND FASTNER LOCATION. REPAIRED IAW SRM 57-51-01-2R-1-D00001, REPAIR 1. WING FIXED TRAILING EDGE SKIN PANELS MADE OF COMPOSITE MATERIALS CATEGORY A REPAIR.Mar 19, 2026 · N1804U · Boeing 7378SDR 2026FA0000225Stiffener · crackedLH WING TOP I/B FWD SKIN, AFT STIFFENER CRACKED. REPLACED WITH NEWMar 19, 2026 · N243G · Piper PA28181SDR DALA2026032301944Skin · crackedDURING HCK AT QRO, WHILE PERFORMING A RIGHT-WING FUEL TANKS INSPECTION PER WC 5700-2472, A CRACK WAS FOUND AFFECTING THE RH WING LOWER SURFACE SKIN PANEL, BETWEEN WSTA 564.5 & 591.5 AND AT S-9R. CRACK WAS REPAIRED PER ERA 600704-14.Mar 19, 2026 · N376DA · Boeing 737832SDR 2026F00038Skin · corrodedFOUND 1 AREA OF CORROSION ON RH WING UPPER SKIN, OUTBOARD OF #7 SPEED BRAKE IN ZONE 642. MECHANICALLY REMOVED 1 AREA OF CORROSION ON RH WING UPPER SKIN, JUST OUTBOARD OF #7 SPEED BRAKE IN ZONE 642 IAW CESSNA 680 SRM 51-70-02. FOUND CORROSION BLEND TO BE BEYONDMar 19, 2026 · N339QS · Cessna 680ASDR 2026F00034Skin · corrodedFOUND 9 AREAS OF CORROSION OF RH WING UPPER SKIN, FWD OF AILERON IN ZONE 652. MECHANICALLY REMOVED 9 AREAS OF CORROSION LOCATED ON RH WING UPPER SKIN, FWD OF AILERON IN ZONE 652 ON WING SKIN TRAILING EDGE IAW CESSNA 680 SRM 51-70-02. FOUND 8 CORROSION BLENDS TMar 19, 2026 · N339QS · Cessna 680ASDR 2026FA0000219Skin · crackedR/H WING FWD WING WALK SKIN CRACKED ON CORRUGATED SKIN. REPLACED WING WALK SKIN ASSY WITH NEWMar 18, 2026 · N243G · Piper PA28181SDR SWAA2026042280783Access Panel · crackedCRACK ON ACCESS PANEL 551GB AT TRAILING EDGE LT WING. REPAIRED ACCESS PANEL 551GB AT TRAILING EDGE LT WING IAW SRM 51-70-04-2R-10 REPAIR 10.Mar 17, 2026 · N927WN · Boeing 7377H4SDR IPXA2026032010352Hinge Fitting · crackedCRACKED SKIN, RT WING T/E NR 10 SPOILER INBD LWR FITTING. REPLACED DAMAGED FITTING IAW SRM 51-40-02-0G, REV 94, & DWG 112T1000, SH 14, REV B, 113T1422, SH 1, REV D, 112T1001, SH 45, REV -, 113T1653, SH 1, REV J, & 113TT1678, SH 1, REV A.Mar 17, 2026 · N317UP · Boeing 76734AFSDR IPXA2026031710375Skin · erodedERODED SKIN, LT WING UPPER PANEL OLES 1318.65~OLES 1453 P/N:65B10870-39. INSTALL L/H WING LEADING EDGE UPPER FIXED PANEL OLES1318.65 - OLES 1453 I.A.W SRM 51-40-02-0G REV.106 AND BOEING DWG NO.65B14961 SH1 REV.E AND 65B14961 SH2 REV.C AND 65B10652 SH4 REV.F ANMar 17, 2026 · N574UP · Boeing 74744AFSDR FDEA202603170356Skin · crackedDURING PERFORM WORK CARD:EG-5710-E0376285G P12 STEP 3.B.(1) & STEP 5.A.(2) THEN FOUND 02EA CRACK ON UPPER WING SKIN FASTENER NR 5. RH WING UPPER SKIN #5 HOLE CRACK REPAIRED AS PER B777 SRM 51-50-02-0G FIGURE 1, SRM 51-40-02-0G FIGURE 12, SRM 51-10-01-0G FMar 17, 2026 · N854FD · Boeing 777FS2SDR 2026F00030Skin · corrodedFOUND 9 AREAS OF CORROSION OF RIGHT WING UPPER SKIN, FWD OF AILERON. MECHANICALLY REMOVED 9 AREAS OF CORROSION LOCATED ON RT WING UPPER SKIN, FWD OF AILERON ON WING SKIN TRAILING EDGE IAW SRM 51-70-02. FOUND 8 CORROSION BLENDS TO BE WITHIN LIMITS IAW SRM 51-70Mar 17, 2026 · N339QS · Cessna 680ASDR FDEA202603160354Skin · crackedDURING PERFORM WORK CARD:EG-5710-E0376285G P11 STEP 3.B.(1)& STEP 5.A.(2) THEN FOUND 01EA CRACK ON UPPER WING SKIN FASTENER #5. LT WING UPPER SKIN #5 HOLE CRACK REPAIRED AS PER B777 SRM51-40-05-0G FIGURE 4 TABLE C, SRM51-40-02-0G FIGURE 12, SRM51-40-04-0G Mar 16, 2026 · N854FD · Boeing 777FS2SDR JR2R20260315943Skin · chafedRH WING UPPER FIXED LE PYLON PANEL CHAFED. REPAIREDMar 15, 2026 · N93305 · Emb ERJ170200LLSDR JR2R20260315052Skin · chafedLEFT WING UPPER FIXED LE PYLON PANEL CHAFED. REPAIREDMar 15, 2026 · N93305 · Emb ERJ170200LLSDR CALA2026033014890Skin · crackedCRACK IN RT LWR WING SKIN FOUND DURING EA 5720-03614 REV 'A' INSPECTION PERFORMED IN SFO BY UAL. AIRCRAFT FERRIED TO GSO FOR REPAIR. MAJOR REPAIR. REMOVED, LOCATED, DRILLED AND INSTALLED NEW RT WING LOWER OUTBD SKIN PANEL AND RESTORED COATINGS REF SRM 51-40Mar 14, 2026 · N58101 · Boeing 757224SDR AALA202603206158Access Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING FUEL ACCESS PANEL 540LB. REPLACED FUEL ACCESS PANEL 540LB PER SRM 57-27-11-283-002.Mar 14, 2026 · N126UW · Airbus A320214SDR CALA2026031714620Access Panel · mechanic errorLEFT WING FUEL PANEL 540PB HAS A MISDRILLED HOLE. REPAIRED LT WING HOLE 694 AT FUEL PANEL 540PB IAW SRM 57-21-11-300-002. NOMINAL HOLE SIZE IS 1/4IN WITH A BUSH DIAMETER INSTALLED OF 0.374IN. THIS REPAIR REQUIRES INSPECTION IAW TABLE 007 OF SRI 57-21-11-205-Mar 13, 2026 · N440UA · Airbus A320232SDR CALA2026031614592Skin · crackedLEFT WING CRACKED. R & R THE SKIN PANEL IAW SRM 51-40-02-0G -0. ACCOMPLISHED REPAIR INSTRUCTIONS PER VT MAE EA 757-5720-13-A 4851. REV. EC/RA: 5720-03631 MAJOR REPAIR ACCOMPLISHED AND ALL RII STEPS C/W.Mar 13, 2026 · N17104 · Boeing 757224SDR IXXA2026031301Skin Panel · damagedREPAIRED CORRODED LEFT WING REAR SPAR UPPER PANEL SUPPORT LIP AND SKIN.Mar 13, 2026 · N752CX · Boeing 7572G5SDR 2026FA0000178Skin · 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 ANDMar 12, 2026 · N933QS · Cessna 680ASDR 2026FA0000175Skin · debondedDISBANDS 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 ANDMar 12, 2026 · N933QS · Cessna 680ASDR 2026FA0000171Skin · corrodedRH WINGTIP SKIN UNDER OTBD STATIC WICK BASE IS HEAVILY CORRODED. COMPLIED WITH NETJETS RFTS-116596 REV.0 TITLE: N678QS (560-5616) WING TIP STATIC WICK BASE CORROSION DATED 11MAR26. THIS IS A PERMANENT MINOR REPAIR.Mar 11, 2026 · N678QS · Cessna 560XLSDR 2026FA0000168Skin · 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 ANDMar 11, 2026 · N571QS · Cessna 680ASDR 2026F00026Door · no discrepancyDURING A RETURN FLIGHT FROM KMLK TO KBIL, THE MED CREW NOTICED THAT THE LEFT WING LOCKER HAD OPENED. THE CREW CONTINUED TO KBIL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND LEFT WING LOCKER DOOR AND FOUND NO DEFECTS.Mar 10, 2026 · N680TW · Beech B200SDR EE4Y2026030924074Skin · crackedCRACKS (2EA) AND ONE ELONGATED HOE WERE FOUND AFFECTING THE LH WING LOWER SKIN AFT SPAR 2 BTWN RIB 10/11. SRM PART II 57-10-01 REP. 54 WAS EVALUATED. THE CRACK #1 IS NOT REPAIRABLE DUE TO THE LOCATION OF THE CRACK AND CRACK #2 IS REPAIRABLE PER SRM AND THE ELOMar 9, 2026 · N304JB · Emb ERJ190100IGWSDR SWAA2026041677808Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 561BB AT LT WING. REPAIRED ACCESS PANEL 561BB AT LT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.Mar 8, 2026 · N7729A · Boeing 73776NSDR IPXA2026031705369Skin · crackedCRACKED SKIN, LOWER FACE OF LT WING T/E INBD MID FLAP T/E UPPER FIXED PANEL , WBL 438. RII COMPLETED FOR THE PIN BETWEEN NR 5 SWING ARM AND SPINDLE OK TO INSTALL.Mar 8, 2026 · N574UP · Boeing 74744AFSDR 2026FA0000162Access Panel · corrodedCORROSION WAS FOUND ON THE LH AND RH WING ACCESS PLANK OPENINGS AND THERE WERE SEVERAL AREAS OUT OF LIMITS PER THE CL350 SRM WHICH REQUIRED ENGINEERING DISPOSITION.Mar 8, 2026 · N749QS · Bombdr BD1001A10SDR SWAA2026041777390Access Panel · damagedELONGATED HOLE ON ACCESS PANEL 661AB AT RT WING. REPAIRED THE ACCESS PANEL 661AB AT RT WING IAW SRM 51-70-04-2R-10, REPAIR 10.Mar 7, 2026 · N8638A · Boeing 7378H4SDR SWAA2026041677529Access Panel · crackedCRACK ON INTERNAL SKIN OF ACCESS PANEL 544BB, LT WING. REPAIRED THE ACCESS PANEL 544BB IAW EA 26-157-00726-WIP1.Mar 7, 2026 · N7729A · Boeing 73776NSDR SWIA2026030676833Skin · crackedFOUND CRACK ON RT WING, RIBS 22 & 23. FABRICATED & INSTALLED RT FWD LOWER SKIN DOUBLER AND TRIPLER IAW ETD2026-170-004072, REV-. WEIGHT AND BALANCE AFFECTED: WEIGHT INCREASE: 10.3 LBS, ARM: 75, MOMENTS: 772.5, TEMPORARY REPAIR, NO ADDITIONAL INSPECTIONS REQUMar 6, 2026 · N152SY · Emb ERJ170200LRSDR 2026FA0000222Stiffener · crackedRH WING LWR I/B FWD SKIN, BOTTOM FWD STIFFENER CRACKED. REPLACED WITH NEWMar 6, 2026 · N467A · Piper PA28181SDR 2026FA0000221Skin · crackedR/H WING AFT WING WALK SKIN CRACKED ON CORRUGATED SKIN. REPLACED WING WALK SKIN ASSY WITH NEWMar 6, 2026 · N467A · Piper PA28181SDR 2026FA0000220Skin · crackedR/H WING FWD WING WALK SKIN CRACKED ON CORRUGATED SKIN. REPLACED WING WALK SKIN ASSY WITH NEWMar 6, 2026 · N467A · Piper PA28181SDR FDEA202603050316Skin · crackedL/WING O/B LEADING EDGE SLAT # 3 O/B INTERNAL MAIN TRACK SLAT HAS COVER SKIN PANEL POSSIBLE CRACK REMOVED AND REPLACED COVE SKIN PANEL LOC AT SLAT # 3 LH WING O/B LEADING EDGE MAIN TRACK AREA IAW BOEING DWG # 114N4077 REV - PL # 114N4077 REV D AND B757 SRMar 5, 2026 · N794FD · Boeing 757222SDR DALA2026031001638Skin · damagedSHIP 9500 ELONGATED HOLE (1EA) AND TOOL MARKS (1EA ) ON INNER/OUTER SKIN FROM FUEL ACCESS PANEL 620JB AT RH WING. CORRECTIVE ACTION: REPAIRED PER PRI 632126-14 (1479482)Mar 4, 2026 · N949AT · Boeing 717200SDR SWAA2026032375867Access Panel · elongatedELONGATED HOLES ON ACCESS PANEL 561BB AT LT WING. REPAIRED THE ACCESS PANEL 561BB IAW SRM 51-70-04-2R-10 REPAIR 10.Mar 3, 2026 · N7889A · Boeing 73779LSDR CALA2026030314275Skin · crackedPERFORMING EA 5720-02922 REV A OP 001 FOUND FASTENER HOLES 1, 2, 3, 4, 5, 6, 7, 8, & 12 OUT OF LIMITS IAW SRM 57-41-01-2R-7. PERFORMED REPAIR ON ON LT WING LEADING EDGE UPPER SKIN PANEL, WORK WAW ACCOMPLISHED IAW SRM 57-41-01-2R-8, EO 260081, REV P1, 260081Mar 2, 2026 · N38268 · Boeing 737824SDR SWAA2026032375509Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 661BB AT RT WING T/E. REPAIRED ACCESS PANEL 661BB IAW SRM 51-70-04-2R-10, REPAIR 10.Mar 1, 2026 · N245WN · Boeing 7377H4SDR QXEA2026032600069Skin · damagedRIGHT WNG FIXED LEADING EDGE ABOVE PYLON IS CHAFED. REMOVED LEADING EDGE AND FABRICATED REPAIR IAW E175 SRM 57-49-01-02-07. RESTORED FINISH. INSTALLED FIXED LEADING EDGE.Feb 28, 2026 · N633QX · Emb ERJ170200LRSDR QXEA2026032600068Skin · damagedLEFT WING FIXED LEADING EDGE ABOVE PYLON IS CHAFED. REMOVED LEADING EDGE AND FABRICATED REPAIR IAW E175 SRM 57-49-01-02-07. RESTORED FINISH AND INSTALLED REPAIR/LEADING EDGE.Feb 28, 2026 · N633QX · Emb ERJ170200LRSDR DALA2026030201424Skin · crackedCRACKS (2 EA) ON INTERNAL SKIN OF INBRD BUTE DOOR (OUTBOARD EDGE) AT RH WING. CORRECTIVE ACTION: REPAIR ASSOCIATED ER/A 14-618696 (1472759)Feb 28, 2026 · N964AT · Boeing 717200SDR JGVR20260228001Skin · wrinkledREPAIRED LT WING WRINKLED SKIN 8 FEET OB OF FUSELAGE AFT OF LEADING EDGE DUE TO DISBONDED STRINGER 2, PER TEXTRON STANDARD REPAIR.Feb 28, 2026 · N960QS · Cessna 680ASDR UATA1750227265701Skin · crackedTWO CRACKS FOUND IN TRAILING EDGE OF LT LOWER INNER FLAP COVE AT APPROXIMATE WS 1800 & 2800. REMOVED 6 1/4 X 2 3/8 SECTION FROM OTBD CRACKED AREA & 4 1/4 X 2 3/8 SECTION FROM INBD CRACKED AREA. REMOVED RIVETS AS REQUIRED FROM UPPER FLAP COVE SKIN FOR ACCESS. Feb 27, 2026 · N348CA · Casa C212CC
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