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.

SDR IPXA2025031180414Skin · cracked**SUPPLEMENTAL SDR** Z600 STR FAULT: RH WING FIXED LE SKIN UNDER SLAT #7 HAS A CRACK ON OB SIDE OF SKIN. INSTALLED RH WING FIXED LE SKIN REPAIR UNDER SLAT #7 IAW SREO-11855-REQ002 STEPS 1 THROUGH 31 WITHOUT DEVIATIONS. ACCCOMPLISH SREO-11855-REQ002 (APPX B)Mar 11, 2025 · N473UP · Boeing 75724APFSDR IPXA2025040180414Skin · crackedRH WING FIXED LE SKIN UNDER SLAT #7 HAS A CRACK ON OB SIDE OF SKIN VERIFIED STEPS 31 TO 33 OF SREO-11855-REQ002 (APPX B) ARE COMPLETED.<BR>RIGGING OF SLATS WILL BE ACCOMPLISHED ON TASK CARDS T3F18E0068H5E & T3F18E0068KDC.Mar 11, 2025 · N473UP · Boeing 75724APFSDR EE4Y2025031021945Skin Panel · crackedDURING THE MAINTENANCE INSPECTION, DURING SEALANT REMOVAL FOR A FUEL LEAK CORRECTION, A CRACK AT THE R/H WING, REAR SPAR AREA, LOWER SKIN NEAR TO RIB20 WAS FOUND. THE DAMAGE WAS CORRECTED IN ACCORDANCE WITH THE REPAIR INSTRUCTIONS OUTLINED IN ETD2025-190-90313Mar 10, 2025 · N228JB · Emb ERJ190100IGWSDR EE4Y2025031021944Skin Panel · damagedDURING THE MAINTENANCE INSPECTION, WERE FOUND 7 HOLES ALREADY OVERSIZED COMMON TO THE EMBRAER SB 190-57-0056 COVER AREA, THE ISSUE WAS CORRECTED IN ACCORDANCE WITH THE REPAIR INSTRUCTIONS OUTLINED IN ETD2025-190-900584 AND THE COOPESA ENGINEERING ORDER COO-EO-Mar 10, 2025 · N228JB · Emb ERJ190100IGWSDR EE4Y2025031021919Skin Panel · damagedDURING THE MAINTENANCE INSPECTION, WERE FOUND 8 OVERSIZED HOLES COMMON TO THE EMBRAER SB 190-57-0056 COVER AREA, THE ISSUE WAS CORRECTED IN ACCORDANCE WITH THE REPAIR INSTRUCTIONS OUTLINED IN ETD2025-190-900055-A AND THE COOPESA ENGINEERING ORDER COO-EO-2025-2Mar 10, 2025 · N228JB · Emb ERJ190100IGWSDR EE4Y2025031021942Skin Panel · damagedDURING THE MAINTENANCE INSPECTION, WERE FOUND 7 HOLES ALREADY OVERSIZED (5/16 2ND OVERSIZE) COMMON TO THE EMBRAER SB 190-57-0056 COVER AREA, THE ISSUE WAS CORRECTED IN ACCORDANCE WITH THE REPAIR INSTRUCTIONS OUTLINED IN ETD2025-190-900473 AND THE COOPESA ENGINMar 10, 2025 · N228JB · Emb ERJ190100IGWSDR EE4Y2025031021941Skin Panel · damagedDURING THE MAINTENANCE INSPECTION, WAS IDENTIFIED EIGHT (8 EA) EXISTING FASTENER HOLES WITH OVERSIZED DIAMETERS COMMON TO LOWER SKIN AND SPAR I, BETWEEN RIB 9-10 AND WITHIN THE AREA COVERED BY EMBRAER SB190-57-0056 REV 00, THE ISSUE WAS CORRECTED IN ACCORDANCEMar 10, 2025 · N228JB · Emb ERJ190100IGWSDR AALA202506119064Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TOP SKIN PANEL UPPER SURFACE AT WS 3059 AND RIB 6. REPAIRED SKIN PANEL PER EA 363237.Mar 7, 2025 · N172US · Airbus A321211SDR AALA202506113261Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TOP SKIN PANEL UPPER SURFACE AT WX 4010 AND RIB 8. REPAIRED SKIN PANEL PER EA 363237.Mar 7, 2025 · N172US · Airbus A321211SDR AALA202506116281Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TOP SKIN PANEL UPPER SURFACE BETWEEN RIB 7 AND 8. REPAIRED SKIN PANEL PER EA 363162.Mar 7, 2025 · N172US · Airbus A321211SDR AALA202506110771Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TOP SKIN PANEL UPPER SURFACE BETWEEN RIB 5 AND 6. REPAIRED SKIN PANEL PER EA 363162.Mar 7, 2025 · N172US · Airbus A321211SDR AALA202506110770Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TOP SKIN PANEL UPPER SURFACE AT WX 5091.4 AND RIB 10. REPAIRED SKIN PANEL PER EA 363237.Mar 7, 2025 · N172US · Airbus A321211SDR VNAA202503070006Skin · wornWEAR ON AREA OF SETTLEMENT OF FAIRINGS 686AB AND 692AB AT RH WING LOWER SKIN. REPAIRED PER REO 690-57-21-508 REV. -.Mar 7, 2025 · N594NN · Cndair CL6002D24SDR EE4Y2025030721919Skin Panel · crackedDURING THE MAINTENANCE INSPECTION, IT WAS FOUND ON RH WING FIXED LEADING EDGE THE SKIN CRACKED AT LEADING EDGE SLAT TRACK #5 OUTBD TRACK UPPER CORNER AREA. THE DAMAGE WAS CORRECTED IN ACCORDANCE WITH THE REPAIR INSTRUCTIONS OUTLINED IN ETD2025-190-900948 AND TMar 7, 2025 · N228JB · Emb ERJ190200IGWSDR EE4Y2025030721918Skin Panel · crackedDURING THE MAINTENANCE INSPECTION, IT WAS FOUND ON LH WING FIXED LEADING EDGE THE SKIN CRACKED AT LEADING EDGE SLAT TRACK #5 OUTBD TRACK UPPER CORNER AREA. THE DAMAGE WAS CORRECTED IN ACCORDANCE WITH THE REPAIR INSTRUCTIONS OUTLINED IN ETD2025-190-900947AND THMar 7, 2025 · N228JB · Emb ERJ190100IGWSDR VNAA202503070001Panel · damagedELONGATED HOLE TO RH WING FIXED L/E PANEL THE SUBJECT CONDITION IS STRUCTURALLY ACCEPTABLE FOR 4900 FLIGHT HOURS FROM TIME OF INCORPORATION OF THIS REO AT REV "- -". REF REO 690-57-41-386-D ** REF REO 690-57-41-387 FOR PERM REPAIR INSTRUCTIONS. ELONGATED HOLMar 7, 2025 · N594NN · Cndair CL6002D24SDR EE4Y2025030721916Skin · damagedDURING THE MAINTENANCE INSPECTION IT WAS DISCOVERED THAT THERE IS AN EXISTING REPAIR ON THE L/H WING LOWER SKIN AT RIB 10, WITH NO MATERIAL TRACEABILITY, THE ISSUE WAS CORRECTED IN ACCORDANCE WITH THE REPAIR INSTRUCTIONS OUTLINED IN ETD2025-190-900721 AND THE Mar 7, 2025 · N228JB · Emb ERJ190100IGWSDR SWAA2025040702662Skin · corrodedCORROSION ON WING CENTER SECTION UPPER SKIN LOC. AT STA 663.75 AND LBL 45.57 2025-168032<[01] TOOL USED ON STEP 4:EDDY CURRENT FLAW DETECTOR P/N:NORTEC 600D; S/N:220272512; DUE DATE:05-FEB-26.;[02] TOOL USED ON STEP 5:EDDY CURRENT FLAW DETECTOR P/N:NORTEC 600DMar 6, 2025 · N287WN · Boeing 7377H4SDR SWAA2025040214240Skin · corrodedCORROSION ON WING CENTER SECTION UPPER SKIN LOC. AT STA 663.75 AND LBL 45.57 2025-168032 <[01]. TOOL USED ON STEP 4: EDDY CURRENT FLAW DETECTOR P/N:NORTEC 600D; S/N:220272512; DUE DATE:05-FEB-26.; [02] TOOL USED ON STEP 5: EDDY CURRENT FLAW DETECTOR P/N:NORTEMar 6, 2025 · N287WN · Boeing 7377H4SDR SWIA202503260006Skin · dentedRH WING LEADING EDGE AT APPROX. WS127 DENTED ON BOTTOM SURFACE, APPROX. 5 INCHES FROM TRAILING EDGE. (2.5 INCHES LONG X .5 INCHES WIDE.) (C-CHECK RO 03/25/2024)TEMP REPAIRED RH WING LEADING EDGE DENT AT APPROX WS127 APPROX 5.0" FROM TRAILING EDGE ON BOTTOM SURMar 6, 2025 · N946SW · Cndair CL6002B19SDR DALA2025030601764Skin · corrodedSHIP 3312 MTC TASK - TO PERFORM PERMANENT REPAIR AT RH WING UPPER SKIN FOR MINOR CORROSION. CORRECTIVE ACTION: COMPLIED WITH ERA 614678-14. (0843030)Mar 6, 2025 · N812NW · Airbus A330323SDR JGVR20250306002Skin · corrodedBLENDED CORRODED AREA ON THE RH UPPER WING SKIN, JUST AFT OF THE LEADING EDGE AND OUTBOARD OF THE WING WALK, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT BY CLEANING, TREATING, AND PRIMING Mar 6, 2025 · N323QS · Cessna 680CESDR JGVR20250306001Skin · corrodedBLENDED 6 AREAS OF CORROSION ON THE RH LOWER OUTBOARD WING SKIN, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT BY CLEANING, TREATING, AND PRIMING AREAS.Mar 6, 2025 · N323QS · Cessna 680CESDR VNAA202504130004Skin · wornWEAR ON SETTLEMENT AREA OF ACCESS PANELS 683AB, 686AB, 692AB 695AB AND 697AB. WEAR ON SETTLEMENT AREA OF ACCESS PANELS 683AB, 695AB AND 697AB WERE BLEND OUT PER CRJ-900 SRM 51-12-00-001-001-A01 EVALUATED WITHIN LIMITS PER CRJ-900 SRM 57-00-01-101-001-A03. WEMar 5, 2025 · N597NN · Cndair CL6002D24SDR N6WA2025030701Skin · damagedLH OTBD WING TRAILING EDGE DAMAGED. REPAIRED LH WING TRAILING EDGE DAMAGE IAW REO 670-57-21-1041.Mar 5, 2025 · N501GJ · Cndair CL6002C11SDR DALA2025030601756Skin · crackedSHIP 5816 CRACK ON FIXED LE APPROX WSTA 430 AT UPPER RH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00107: FIXED LE APPROX WSTA 430 AT UPPER RH WING WAS REPAIRED PER B757-300 SRM 51-70-17-0G. (0842478)Mar 5, 2025 · N596NW · Boeing 757351SDR JR2R20250305076Skin · chafedRH WING FIXED LEADING EDGE OVER PYLON HAS CHAFE MARKS OUT OF LIMITSMar 5, 2025 · N88326 · Emb ERJ170200LRSDR FDEA202503050332Skin · crackedOPEN HOLE HFEC INSPECTION ON THE RH WING WBL 262 THEN FOUND HOLE #6 CRACK IN UPPER WING SKIN AS MARKED. RH WING WBL 262 UPPER SKIN #6 HOLE CRACK REPAIRED AS PER B777 SRM51-10-01-0G, 51-20-01- 0G, 51-20-05-0G,51-20-06-0G, 51-20-07-0G, 51-40-08-0G, 51-40-02Mar 5, 2025 · N880FD · Boeing 777F28SDR VNAA202504130002Skin · scratchedSCRATCHES ON WINGS LOWER SURFACE RH WING REAR SIDE BTW WS294.50-WS343.50 AND LH WING REAR SIDE AT WS294.50. SCRATCHES ON WINGS LOWER SURFACE RH WING REAR SIDE BTW WS294.50-WS343.50 AND LH WING REAR SIDE AT WS294.50 WERE BLENDED PER CRJ-900 SRM 51-12-00-001-Mar 4, 2025 · N597NN · Cndair CL6002D24SDR SWAA2025032609560Doubler · damagedR WING DEFLECTION CONTROL RIB HAS 2EA ELONGATED FASTENER HOLE ON ATTACHMENT TAB.(MARKED)<[01] WEAR DAMAGE ON RIGHT WING I/B FIXED T/E DEFLECTION CONTROL RIB UPPER TAB IS OUT OF LIMITS PER SRM 53-51-02-1A-1. CUT AND REMOVED THE DAMAGED PART OF THE DEFLECTION COMar 4, 2025 · N8689C · Boeing 7378H4SDR SWAA2025032404816Doubler · wornR WING FIXED TRAILING EDGE PANEL SUPPORT BEAM AT WBL 198.6(ATTACHED TO DEFLECTION CONTROL RIB) HAS WORN FASTENER HOLES.(MARKED)<[01] WEAR DAMAGE ON RIGHT WING FIXED T/E UPPER SUPPORT BEAM IS OUT OF LIMITS PER SRM 53-51-02-1A-1. CUT AND REMOVED DAMAGE FROM THE Mar 4, 2025 · N8689C · Boeing 7378H4SDR GTIA2025030638785Skin Panel · corrodedCORROSION ON LH WING TOP SKIN BTW RIB AND RIBS RAF-01 3577669-02 GENERATED.-PERFORMED PERMANENT REPAIR OF LH WING TOP SKIN PANEL 2 BTW RIB 4 TO RIB 5 ALONG REAR SPARK-UPPER SURFACE I.A.W. DOSSIER 81543621 AND EA #57-0013-25. THIS REPAIR IS CATEGORY A.Mar 4, 2025 · N667NK · Airbus A321231SDR SWIA202503050004Skin · ground damageTRANSFER FROM EAML 1548503 : TUG WITH NO DRIVER ROLLED ACROSS RAMP AND IMPACTED RIGHT WING DURING BOARDING. LARGE DENT IN LEADING EDGE. (FILED OPEN - FLIGHT 5449) THIS IS CURRENTLY A WORK IN PROGRESSMar 4, 2025 · N856AS · Cndair CL6002B19SDR JR2R20250304080Skin · chafedLH WING FIXED LEADING EDGE OVER PYLON HAS CHAFE MARKS OUT OF LIMITS.Mar 4, 2025 · N88326 · Emb ERJ170200LRSDR SWIA20250613303Skin · puncturedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA94069-REO 601R-57-31-1443 MXCODEID104781-PR - APPEARS TO BE A SMALL PUNCTURE ON TOP OF LEFT WINGLET.COMPLIED WITH REO 601R57-31-1443, COVERED DISCREPANT AREA WITH SPEED TAPE PER REO, PERMANENT REPAIR WITHIN 1600 FLIGHTMar 3, 2025 · N954SW · Cndair CL6002B19SDR IPXA2025032637187Doubler · puncturedFAULT - STR - Z600 - R/H WING, I/B FLAP LOWER SKIN, BETWEEN RIB 9 AND 10, AT 1.7 IN I/B OF RIB 10, 2 PUNCTURES AT 14 AND 15 IN OF TRAILING EDGE. DOT 73-036 VERIFIED APPLICATION OF TOP COAT AT EXTERNAL PLATE (DOUBLER) ON R/H WING, I/B FLAP LOWER INNER SKIN, BETMar 3, 2025 · N121UP · Airbus A300F4622RSDR JGVR20250303006Skin · corrodedBLENDED 6 AREAS OF CORROSION ON LH UPPER WING (INBOARD WING) PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT BY CLEANING, TREATING, AND PRIMING AREAS.Mar 3, 2025 · N323QS · Cessna 680CESDR JGVR20250303005Skin · corrodedBLENDED 15 AREAS OF CORROSION ON LH UPPER WING IN ZONES 551 AND 552 (OUTBOARD WING) PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. REPAIRED AREAS PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT BY CLEANING, TREATING, AND PRIMING AREAS.Mar 3, 2025 · N323QS · Cessna 680CESDR IPXA2025032623937Access Panel · crackedR/H WING, ACCESS 613AB, FWD R/H CORNER WITH CRACK. DOT 73-028. VERIFIED INSTALLATION OF REPAIR PARTS IAW SRM 53-15-63.Mar 2, 2025 · N121UP · Airbus A300F4622RSDR IXXA20250425003Access Panel · corrodedLEFT WING LOWER ACCESS PANEL 532AB IS WORN AND CORRODEDFeb 28, 2025 · N229AZ · Boeing 767323SDR IXXA202504211005Access Panel · corrodedLEFT WING LOWER ACCESS PANEL 531AB IS WORN AND CORRODED, HAECO WO 320011 AND NR 34514Feb 28, 2025 · N229AZ · Boeing 767323SDR SWAA2025040700922Access Panel · crackedCRACK ON HOLES LOCATED ACCESS PANEL 661CB AT RT WING 2025-167784<[01] STEP 12 TOOL USED ULTRASONIC FLAW DETECTOR P/N: EPOCH 600; S/N: 120357005; CAL DUE DATE: 10-JUN-25;[02] TOOL USED: MULTIMETER P/N: FLUKE 87-V; S/N: 65700125; DUE DATE: 09-JAN-26. TOOL USED HFeb 28, 2025 · N287WN · Boeing 7377H4SDR SWAA2025040214217Access Panel · crackedCRACK ON HOLES LOCATED ACCESS PANEL 661CB AT RT WING 2025-167784<[01] STEP 12 TOOL USED ULTRASONIC FLAW DETECTOR P/N: EPOCH 600; S/N: 120357005; CAL DUE DATE: 10-JUN-25;[02] TOOL USED: MULTIMETER P/N: FLUKE 87-V; S/N: 65700125; DUE DATE: 09-JAN-26. TOOL USED HFeb 28, 2025 · N287WN · Boeing 7377H4SDR AALA202502284250Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION LEFT WING TRAILING EDGE TOP SKIN PANEL #2 LOWER SURFACE AT RIB 11. REPAIRED SKIN PANEL PER EA 361177.Feb 27, 2025 · N163US · Airbus A321211SDR AALA202502281017Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE TOP SKIN PANEL #2 LOWER SURFACE AT RIB 10. REPAIRED SKIN PANEL PER EA 361177Feb 27, 2025 · N163US · Airbus A321211SDR DXTA202502270053Skin · debondedDEBONDING OF LH/RH WING UPPER SKIN ASSEMBLY AT STRINGER ENDS. ACCOMPLISHED FR-680A-0063-14759 REV - DATED 2-13-2025 AND FAA FORM 8110-3 DATED 02/13/2025; FIELD REPAIR - LOCAL DISBOND AND CONTOUR DEVIATIONS, LH/RH WING, UPPER SKIN BOND ASSEMBLIES, BETWEEN CWS 1Feb 27, 2025 · N525QS · Cessna 680ASDR SWAA2025022899827Panel · delaminatedWING-TO-BODY ACCESS PANEL 192BR LEADING EDGE HAS POSSIBLE DELAM <[01]. FOUND DAMAGE TO BE EROSION TO AT LEAST ONE OR MORE PLYS OF COMPOSITE. THERE ARE THREE AREAS OF CONCERN. AREA #1 IS 3.7? BY 1.45?; AREA #2 IS 2.7? BY 0.8?; AREA #3 IS 2.5? BY 0.6?.; [02] ACFeb 26, 2025 · N462WN · Boeing 7377H4SDR SWAA2025022899141Tail Cone · elongatedNUMBER THREE AFT FLAP FAIRING HAS THREE ELONGATED FASTENER HOLES THAT ATTACH THE AFT TAIL CONE <[01]. REMOVED AND REPLACED THE #3 AFT FLAP FAIRING IAW AMM 27-51-18.;[02] REMOVED AND REPLACED THE #3 AFT FLAP FAIRING IAW AMM 27-51-18.;[03] REMOVED AND REPLACED TFeb 25, 2025 · N8623F · Boeing 7378H4SDR P5CA2025022700008Skin · crackedOPEN HOLE INSPECTION CARRIED OUT AS PER EO CARD: 7757A025 PART 1, ON LHW UPPER SKIN COMMON TO MLG TAB OUT FASTENER HOLES 0-6 AND FOUND HOLE #5 WITH CRACK INDICATION APPROX 0.030" INCHES LENGTH, VIEW LOOKING DOWN AFT AT 6 O'CLOCK &11 O'CLOCK POSITION.(<P> CRACKFeb 25, 2025 · N777SA · Boeing 777FZBSDR P5CA2025022700009Skin · crackedOPEN HOLE INSPECTION CARRIED OUT AS PER EO CARD: 7757A025 PART 2, ON RHW UPPER SKIN COMMON TO MLG TAB OUT FASTENER HOLES 0-6 AND FOUND HOLE NO.5 WITH CRACK INDICATION APPROX 0.030" INCHES LENGTH, VIEW LOOKING DOWN AFT AT 6 O'CLOCK & 1 O'CLOCK POSITION. CRACKEDFeb 25, 2025 · N777SA · Boeing 777FZB
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