JASC 5730
Service difficulty reports · 27,210
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 FDEA202610201614Doubler · crackedLEFT WING, LEADING EDGE COMPARTMENT BEADED DOUBLER AT XOS 764 FOUND CRACKED ABOUT 0.2 INCH.SDR FDEA202610201613Doubler · crackedRIGHT WING, LEADING EDGE COMPARTMENT BEADED DOUBLER AT XOS 746 FOUND CRACKED ABOUT 0.2 INCH.SDR FDEA202610201612Doubler · crackedRIGHT WING, LEADING EDGE COMPARTMENT BEADED DOUBLER AT XOS 740 FOUND CRACKED ABOUT 0.2 INCH.SDR FDEA202610201611Doubler · crackedRIGHT WING, LEADING EDGE COMPARTMENT BEADED DOUBLER AT XOS 728 FOUND CRACKED ABOUT 0.2 INCH.SDR FDEA202610201610Skin · crackedRIGHT WING, NR 16 SLAT TRACK CUTOUT AT WS XOS 1005, FOUND CRACKED ABOUT 0.5".SDR R61A2026101800305Skin · crackedFOUND CRACK ON RT WING LOWER SKIN, INBOARD OF RIB 17 AND AFT OF SPAR 1. PERFORMED PERMANENT REPAIR AT RT WING LOWER SKIN RIB 17 IAW ETD2026-170-017594, REV A.SDR CALA2026102120497Skin · crackedRT WING SKIN UNDER ACCESS PANEL 643BB CRACKED AT HOLE 5. CRACK LOCATION IS AT THE 6 AND 12 0'CLOCK LOCATION. (FWD AND AFT)SDR FXGA202610140001Skin · crackedFOUND 2 CRACKS ON LT WING UPPER SKIN. 1ST CRACK 2.3" LONG BETWEEN RIBS AT LBL 142.3 & 157.95, APPROXIMATELY 17.5 INCHES FORWARD OF WING TRAILING EDGE. 2ND CRACK 4.5" LONG BETWEEN RIBS AT LBL 157.95 & 173.6, APPROXIMATELY 14.25 INCHES FORWARD OF WING TRAILING ESDR JR2R20261012532Skin · chafedRH WING FIXED LEADING EDGE OVER PYLON HAS CHAFES. REPAIREDSDR JR2R20261012537Skin · chafedLEFT WING FIXED LEADING EDGE OVER PYLON HAS CHAFES. REPAIRED.SDR YENA2026101500971Skin · corrodedDURING HEAVY MAINTENANCE, REF AEROMAN WO# 2026-228/1. NR# 2026-450562. CORROSION ON RH WING TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 7 ( CPCP FINDING ).; "(RESOLVED ON W/O: 1486589 TASKCARD: NR-00043 ) REF AEROMAN WO# 2026-228/1. NR# 2026-450562. ACCOMPLISDR YENA2026101500970Skin · damagedDURING HEAVY MAINTENANCE, WEIGHT VARIANT UPGRADE FOR A/C N558JB - SRM REPAIR SURVEY, DEFECT 4400 62-29919 ; "(RESOLVED ON W/O: 1486589 TASKCARD: NR-00047 ) REF AEROMAN WO 2026-228/1 NR # 2026-450636 COMPLISHED REPAIR OF THE LH WING TOP SKIN PANEL 2 TEOH LOWERSDR YENA2026101500969Skin · crackedDURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 17 PLUS 16 INCH ES LH WING (CPCP FINDING); "(RESOLVED ON W/O: 1486589 TASKCARD: NR-00049 ) REF AEROMAN WO # 2026-228/1 NR # 2026-450566 ACCOMPLISHED REPAIR OF THE LH WING TOP SKSDR YENA2026101500968Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 11 ON LH WING ( CPCP FINDING ); "(RESOLVED ON W/O: 1486589 TASKCARD: NR-00050 ) REF AEROMAN 2026 228/1 NR2026-450552 ACCOMPLISHED REPAIR OF THE LH WING TOP SKIN PANEL 2 TEOH LOWESDR YENA2026101500967Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 10 LH WING (CP CP FINDING ); "(RESOLVED ON W/O: 1486589 TASKCARD: NR-00051 ) REF AEROMAN WO # 2026-228/1 NR # 2026-450544 ACOMPLISHED REPAIR OF THE LH WING TOP SKIN PANEL 2 TEOH SDR YENA2026101500966Skin · corrodedDURING HEAVY MAINTENANCE, REF AEROMAN WO# 2026-228/1. NR# 2026-450569. CORROSION ON RH WING TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 13 PLUS 3 INCHES. (CPCP FINDING).; "(RESOLVED ON W/O: 1486589 TASKCARD: NR-00052 ) REF AEROMAN WO# 2026-228/1. NR# 2026-45SDR YENA2026101500965Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 11 PLUS 17 INCH ES LH WING (CPCP FINDING ; "(RESOLVED ON W/O: 1486589 TASKCARD: NR-00053 ) REF AEROMAN WO # 2026-228/1 NR # 2026-450553 ACCOMPLISHED REPAIR OF THE LH WING TOP SKISDR YENA2026101500964Skin · corrodedDURING HEAVY MAINTENANCE, REF AEROMAN WO# 2026-228/1. NR# 2026-450551. CORROSION ON LH WING TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 10 PLUS 16 INCHES.; "(RESOLVED ON W/O: 1486589 TASKCARD: NR-00054 ) REF AEROMAN WO# 2026-228/1. NR# 2026-450551. ACCOMPLISHSDR YENA2026101500962Skin · crackedDURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 11 ON LH WING ( CPCP FINDING ); "REF AEROMAN 2026 228/1 NR2026-450552 ACCOMPLISHED REPAIR OF THE LH WING TOP SKIN PANEL 2 TEOH LOWER SURFACE RIB 9-18 IN ACCORDANCE WITH AEROMAN ESDR YENA2026101500961Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 17 PLUS 16 INCH ES LH WING (CPCP FINDING); "REF AEROMAN WO # 2026-228/1 NR # 2026-450566 ACCOMPLISHED REPAIR OF THE LH WING TOP SKIN PANEL 2 TEOH LOWER SURFACE RIB 9-18 IN ACCORDSDR YENA2026101500960Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 10 LH WING (CP CP FINDING ); "REF AEROMAN WO # 2026-228/1 NR # 2026-450544 ACOMPLISHED REPAIR OF THE LH WING TOP SKIN PANEL 2 TEOH LOWER SURFACE RIB 9-18 IN ACCORDANCE WITH AEROMSDR YENA2026101500959Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 11 PLUS 17 INCH ES LH WING (CPCP FINDING; REF AEROMAN WO # 2026-228/1 NR # 2026-450553 ACCOMPLISHED REPAIR OF THE LH WING TOP SKIN PANEL 2 TE OH LOWER SURFACE RIB 9-18 IN ACCORDANSDR YENA2026101500958Skin · crackedDURING HEAVY MAINTENANCE, EA A26-876-01 WING / LH WING / TOP SKIN PANEL #2 / TEOH LWR SURFACE / RIB 9-18 / CORROSION - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)SDR YENA2026101500954Skin · corrodedDURING HEAVY MAINTENANCE, EA 26-872-01 WING / RH WING / TOP SKIN PANEL #2 / TEOH LWR SURFACE / RIB 13 / CORROSION - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)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 FDEA202610081495Doubler · crackedRIGHT WING, FIXED LEADING EDGE RIB DOUBLER AT STATION XOS 667 FOUND CRACK ABOUT 0.2".SDR FDEA202610081494Doubler · crackedLEFT WING, FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 705 FOUND CRACK ABOUT 0.3".SDR FDEA202610081493Doubler · crackedLEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 682 FOUND CRACK ABOUT 0.2".SDR FDEA202610081492Doubler · crackedRIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 705 FOUND CRACK ABOUT 0.2".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 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 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 R61A2026100100290Skin · crackedFOUND CRACK ON RT WING MAIN BOX, LOWER SKIN, AT SPAR II RIB 4A JUNCTION. REPAIRED PER ETD 2026-170-016493.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 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 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.
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