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 YENA2026101500951Skin · corrodedDURING HEAVY MAINTENANCE, EA 26-873-01 WING / RH WING / TOP SKIN PANEL #2 / TEOH LWR SURFACE / RIB 7 AND 13 / CORROSION - TIME-LIMITED REPAIR (CONSIDERED A MAJOR REPAIR)SDR IPXA2026102964528Panel Latch · damagedLEFT WING PANEL 511CB HAS 2 PULLED THRU SCREW HOLES. REPAIR MULTIPLE DAMAGES ON LT WING LEADING EDGE LOWER SKIN PANEL BETWEEN ISS 144 AND ISS 171 IAW EI F2026A57M-2376, REV 0, & EO-99090-REQ1 REV 1. CONDITION CHECK IS SATISFACTORY.SDR IPXA2026102964575Panel · damagedRIGHT WING PANEL 611CB HAS 1 PULLED THRU SCREW. REPAIR MULTIPLE DAMAGES ON RT WING LEADING EDGE LOWER SKIN PANEL BETWEEN ISS 144 AND ISS 171 I.A.W EGAT EI F2026A57M-2379 REV 0, AND EO-99088-REQ1 REV. 1. CONDITION CHECK IS SATISFACTORY.SDR FDEA202610081495Doubler · crackedRIGHT WING, FIXED LEADING EDGE RIB DOUBLER AT STATION XOS 667 FOUND CRACK ABOUT 0.2". RIGHT WING FIXED LEADING EDGE CRACKED RIB DOUBLER AT STATION XOS 667 REMOVED AND INSTALLED WITH FABRICATED RIB DOUBLER AS PER MD-11 SRM 51-31-01-0G.RIB DOUBLER FABRICATESDR FDEA202610081494Doubler · crackedLEFT WING, FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 705 FOUND CRACK ABOUT 0.3". LEFT WING FIXED LEADING EDGE CRACKED BEADED DOUBLER AT STATION XOS 705 CARRIED OUT REPAIR AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR ISDR FDEA202610081493Doubler · crackedLEFT WING, FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 682 FOUND CRACK ABOUT 0.2". LEFT WING FIXED LEADING EDGE CRACKED BEADED DOUBLER AT STATION XOS 682 CARRIED OUT REPAIR AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJSDR FDEA202610081492Doubler · crackedRIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 705 FOUND CRACK ABOUT 0.2". RIGHT WING FIXED LEADING EDGE CRACKED BEADED DOUBLER AT STATION XOS 705 CARRIED OUT REPAIR AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS SDR R61A2026102800333Skin · crackedDURING C-CHECK CRACK FOUND ON LT WING FIXED LEADING EDGE SLAT TRACK NR 4 CUTOUT BETWEEN, RIB 14-15. CRACK REPAIRED IAW ETD 2026-170-017565.SDR COEA2026101212767Skin · crackedDURING A POST FLIGHT INSPECTION, DISCOVERED A CRACK ON THE RT UPPER WING SKIN BETWEEN WS 224.32 AND WS 241.68. OPENSDR COEA2026101211767Skin · crackedDURING A POST FLIGHT INSPECTION, DISCOVERED A CRACK IN THE LT UPPER WING SKIN BETWEEN WS 157.95 AND WS 142.30. OPENSDR UIEA2026100600955Skin · crackedDURING LFEC INSPECTION AT LH WING FRONT SPAR UPPER SKIN BETWEEN WS621-WS637, FOUND 02 EA FASTENERS WITH CRACKED INDICATIONS.(<P>REFER TO EN 3800-26 REV 0 FOR WORK PERFORMED. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026100600956Skin · crackedDURING LFEC INSPECTION AT RH WING FRONT SPAR LOWER SKIN BETWEEN WS540-WS560 FOUND 01 EA FASTENER WITH CRACK.(<P>REFER TO EN#3799-26 REV 0 FOR WORK PERFORMED. NO FURTHER DEFECTS NOTED.</P>)SDR CALA2026100820218Access Panel · damagedDURING REMOVAL OF ACCESS PANEL 540KB, ACFT SKIN WAS DAMAGED. EXCEEDED LIMITS OF SRM 57-21-11-300-002, INTERIM REPAIR PERFORMED TO FUEL ACCESS PANEL 540KB IAW PART 1 OF ECRA 5721-01445. ACCOMPLISH PERMINATE REPAIR AT LT WING BOTTOM FUEL ACCESS PANEL 540KB HOSDR SWAA2026102743637Access Panel · damagedELONGATED HOLES ON LT WING ACCESS PANEL 561BB, REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-9, REPAIR 9.SDR CALA2026101320350Access Panel · crackedRIGHT WING INTERSPAR 2 EACH CRACKS NOTED WHILE ACCOMPLISHING EA5720-03647 (A) AT HOLES NR 6 & 27 AT PANEL ACCESS 643BB. ACCOMPLISHED INTERIM REPAIR PER PART 1 OF ECRA 5720-03684 AND ST ENGINEERING EA757-5720-13-A4616 WITH NO DEVIATIONS. DIP REQUIR ED AS FOLLSDR JR2R20261006891Panel · chafedR/H WING OVER PYLON L/E PANEL IS CHAFED. REPAIRED PER SRM.SDR JR2R20261006890Panel · chafedL/H WING OVER PYLON L/E PANEL IS CHAFED. REPAIRED PER SRM.SDR SWAA2026102643403Access Panel · crackedRIGHT WING ACCESS PANEL 632CB WAS CRACKED. R & R RT WING FUEL MAIN TANK ACCESS PANEL IAW AMM 28-11-11. OK TO INSTALL PERFORMED ON CARD TTG8Q01E7ACY. C/W INSPECTION.SDR DALA2026100605529Vane · dentedDENT ON LOWER SURFACE OF RT FWD MOVABLE VANE WAS FOUND AT RT WING. WD MOVABLE VANE AT RT WING WAS REPAIRED IAW SRM 57-53-01-2R, PROCEDURE 1, REPAIR 1. AND SRM 51-70-02-0G. (1848375) AIRCRAFT WAS GROUNDED.SDR SWAA2026100721957Winglet · delaminatedUPPER SPLIT SCIMITAR WINGLET LEADING EDGE DELAMINATED. IAW SRM 57-30-01-2R-6, PROCEDURES BY COMPLETING REPAIR 6, TYPE 1. TEMPORARY REPAIR FOR RT WINGLET EROSION TAPE. ENGINEERING CONCURS WITH SRM.SDR SWAA2026102335706Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 651GB AT RT WING. REPAIRED ACCESS PANEL 651GB AT RT WING IAW SRM 51-70-04-2R-9, REPAIR 9.SDR R61A2026100100290Skin · crackedFOUND CRACK ON RT WING MAIN BOX, LOWER SKIN, AT SPAR II RIB 4A JUNCTION. REPAIRED PER ETD 2026-170-016493.SDR R61A2026102800334Doubler · crackedDURING C-CHECK CRACK FOUND ON RT WING FIXED LEADING EDGE TRACK NR 7 CUTOUT DOUBLER. REMOVED AND REPLACED DOUBLER IAW SRM 51-41-02 AND 51-43-04.SDR COEA2026100109708Skin · crackedEVIDENCE OF A CRACK ON THE R/H WING AFT SIDE TOWARDS THE OUTBOARD PORTION OF THE FLAP. OPENSDR DALA2026100105450Skin · gougedGOUGES ON FIXED LEADING EDGE BTW XOS=390 TO XOS=410 AT LT WING, COMPLIED WITH ER/A 637059-14. (1841449) (AIRCRAFT GROUNDED).SDR IPXA2026100181758Access Panel · crackedLEFT WING BELOW KRUGER FLAP ACCESS PANEL 513AB STRUCTURE (RING) CRACKED. INTERNAL DOUBLER WAS REMOVED AT LH WING BELOW KRUGER FLAP ACCESS PANEL 513AB IAW A300-600 SRM 51-40-21-001. INSTALLED INTERNAL DOUBLER ON LH WING BELOW KRUGER FLAP ACCESS PANEL 513AB IAW SDR COEA2026100108708Panel · dentedDENT UNDER LT SPONSON PANEL. OPENSDR SWAA2026102793792Access Panel · crackedCRACKED FLOAT ACCESS PANEL 632QB, FUEL TANK, RT WING. REPLACED FLOAT ACCESS PANEL 632QB IAW CMM 28-40-11, TASK 28-40-11-400-801-A01 ASSEMBLY PROCEDURE PAGE 7003 STEP 3.A.(2)(E)SDR SCNA20261014425Skin Panel · crackedINITIAL INSPECTION: CRACK WAS FOUND IN THE SKIN OF HOLE #6 SKIN AND COUNTERSINK BTW 12 O CLOCK POSITION AT LEADING EDGE SKIN PANEL KRAS 206, LEFT WINGS. (CONTACT ENGINEERING FOR FURTHER REPAIR INSTRUCTION) IN REFERENCE JOB # 581. CARD: ENG-57SCA-11486. CRACK OSDR SCNA20261014424Skin · crackedCRACKS WERE FOUND IN THE SKIN OF HOLE #4 SKIN & COUNTERSINK BTW 10 O CLOCK POSITION AND HOLE #5 SKIN & COUNTERSINK BTW 11 O CLOCK POSITION AT LEADING EDGE SKIN PANEL KRAS 206, RIGHT WING. (CONTACT ENGINEERING FOR FURTHER REPAIR INSTRUCTION) REF JOB 581. CARD: SDR SWIA2026092777276Skin · dentedLH WING TIP LEADING EDGE FOUND DENTED FILED CLOSEDDUE TO NO ALLOWABLE DENT DAMAGE TO THE WING TIP FIXED LEADING EDGE BEING SPECIFIED IN THE SRM, REMOVED AND REPLACED LH WING TIP FIXED LEADING EDGE IAW AMM 57-30-01SDR SWAA2026102765439Access Panel · crackedCRACK ON INTERNAL AREA AFT FAIRING ACCESS PANEL 542BB AT LT WING. REPAIRED ACCESS PANEL 542BB ON INTERNAL AREA AFT FAIRING AT LT WING IAW EA M-21-157-01063.SDR SWAA2026101619844Access Panel · elongatedELONGATED HOLES ON THE LT WING ACCESS PANEL 561CB. REPAIRED THE ACCESS PANEL 561CB IAW SRM 51-70-04-2R-10, REPAIR 10.SDR SWAA2026101639462Access Panel · damagedELONGATED HOLES ON LT WING ACCESS PANEL 561AB. REPAIRED THE ACCESS PANEL 561AB IAW SRM 51-70-04-2R-10, REPAIR 10.SDR SWAA2026101639003Access 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 SWAA2026101678960Access Panel · elongatedELONGATED HOLES ON ACCESS PANEL 661BB ON THE RT WING. REPAIRED THE ACCESS PANEL 661BB IAW SRM 51-70-04-2R-10, REPAIR 10.SDR SWAA2026101655716Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 661CB OF THE RT WING. REPAIRED THE ACCESS PANEL 661CB IAW SRM 51-70-04-2R-10, REPAIR 10.SDR SWAA2026101655801Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 661AB ON THE RT WING. REPAIRED THE ACCESS PANEL 661AB IAW SRM 51-70-04-2R-10, REPAIR 10.SDR SIMA20260924001Skin · crackedCRACK THROUGH FASTENER HEAD ON R/H WING LOWER EXTERNAL SKIN INBOARD OF RIB 6 AND AFT OF PANEL 621CB. (SSI#57-10-002). (MAJOR REPAIR) REPAIRED IAW ERS-EJ-57MR-1846.SDR SWAA2026102745912Access Panel · damagedELONGATED HOLES ON LT WING ACCESS PANEL 561BB. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-9, REPAIR 9.SDR DALA2026092505351Ring · corrodedCORROSION FOUND ON FUEL ACCESS PANEL 532AB RING. THE ACCESS PANEL 532AB RING WAS REPAIRED IAW SRM 57-20-01-2R, PROCEDURE 1, REPAIR 1. (1827971) AIRCRAFT WAS GROUNDEDSDR AALA202609246140Access Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING PANEL FUEL TANK ACCESS PANEL 540LB COUNTERSUNK FASTENER HOLES - MAINTENANCE REPLACED FUEL TANK ACCESS PANEL 540LBSDR REXA2026101601937Access Panel · chafedWORN WING ACCESS PANELS, 584FT, 599CB, 584BB, 599BB, 584GB, 584JB, 584EB, 584LB, 584AB, 584ET, 699BB, 699AB, 684ET, 684HT, 684BB, 684EB, 684GB, 684JB, & 684LB. ACCESS PANELS NBR 584FT, 599CB, 584BB, 599BB, 584GB, 584JB.584EB,584LB, 584AB,584ET, 699BB, 699AB, SDR REXA2026101601936Access Panel · wornWORN WING ACCESS PANELS, 584FT, 599CB, 584BB, 599BB, 584GB, 584JB.584EB, 584LB, 584AB, 584ET, 699BB, 699AB, 684ET, 684HT, 684BB, 684EB, 684GB, 684JB, & 684LB. THE ACCESS PANELS WERE BLENDED OUT IAW SRM 51-12-00-001-001-A01. NR 584EB, 684ET, & 684EB WERE EVASDR REXA2026101601935Access Panel · chafedWORN WING ACCESS PANELS, 584FT, 599CB, 584BB, 599BB, 584GB, 584JB.584EB, 584LB, 584AB,584ET, 699BB, 699AB, 684ET, 684HT, 684BB, 684EB, 684GB, 684JB, & 684LB. THE ACCESS PANELS WERE BLENDED OUT IAW SRM 51-12-00-001-001-A01, AND WERE EVALUATED WITHIN LIMITS IAWSDR SWAA2026101229421Access Panel · crackedCRACK BRACKET ACCESS PANEL 551FB AT LT WING. REPLACED BRACKET AND FASTENERS LOCATED ON ACCESS PANEL 551FB IAW SRM 51-40-02, SRM 51-10-02, ITEM 9. AND DWG 115A2710, SHEET 6, REV B.SDR FDEA202609221414Skin · crackedHIGH FREQUENCY EDDY CURRENT INSPECTION FOUND CRACK INDICATION APPROXIMATE 0.25" IN LENGTH AT RIGHT HAND WING FIXED LEADING EDGE SKIN ADJACENT TO CUTOUT AT CORNER NUMBER 5 SLAT ACTUATOR ACCESS DOOR FORWARD INBOARD CORNER AT APPROXIMATE STATION XOS 484.511SDR FDEA202609221413Skin · crackedHIGH FREQUENCY EDDY CURRENT INSPECTION FOUND CRACK INDICATION APPROXIMATE 0.15" IN LENGTH AT LEFT HAND WING FIXED LEADING EDGE SKIN ADJACENT TO CUTOUT AT CORNER NUMBER 13 SLAT TRACK CUTOUT #10 AFT INBOARD CORNER AT APPROXIMATE STATION XOS 659.7174.SDR FDEA202609221412Skin · crackedHIGH FREQUENCY EDDY CURRENT INSPECTION FOUND CRACK INDICATION APPROXIMATE 0.15" IN LENGTH AT LEFT HAND WING FIXED LEADING EDGE SKIN ADJACENT TO CUTOUT AT CORNER NUMBER 13 SLAT TRACK CUTOUT #10 AFT INBOARD CORNER AT APPROXIMATE STATION XOS 659.7174. CUTOSDR FDEA202609221410Skin · crackedRIGHT HAND WING- LEADING EDGE COMPARTMENT ANGLE AT XOS 1083 FOUND CRACK ABOUT 0.5 INCHES. RIGHT HAND WING LEADING EDGE COMPARTMENT CRACKED ANGLE AT XOS 1083 REMOVED PER MD-11 SRM 51-33-01-0G AND MD-11 SRM 51-35-01-0G. FABRICATED ANGLE PER DOUGLAS DRAWING
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