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.
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 SWAA2025071783857Panel · damagedLH WING TRAILING EDGE PANEL 561AB HAS DAMAGED SCREW HOLES UPPER SURFACE. LOCATED AFT EDGE ROW FROM SCREWS PULLING THROUGH COMPOSITE PANEL. REMOVED DAMAGE AND ACCOMPLISHED REPAIR REF SRM 51-70-04-2R-9 SEE C/A 1-4. RESTORED FINISH TO REPAIR AREA REF AMM 51-21-99SDR SWAA2025071783858Panel · pulledLH WING TRAILING EDGE PANEL 561CB HAS DAMAGED SCREW HOLES UPPER SURFACE. LOCATED AFT EDGE ROW FROM SCREWS PULLING THROUGH COMPOSITE PANEL. REMOVED DAMAGE AND ACCOMPLISHED REPAIR REF SRM 51-70-04-2R-9 SEE C/A 1-4. RESTORED FINISH TO REPAIR AREA REF AMM 51-21-99SDR AALA202509031054Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON TRAILING EDGE TOP SKIN LOWER SURFACE EXACTLY LOCATION IS RIB 14 PLUS 16 INCHES LEFT WING L=7.540 INCHES W=2.000 INCHES D=0.030 INCHES. MAINTENANCE PERFORMED TIME LIMITED REPAIR (EXTERNAL DOUBLER) ON RIB 14 PLUS 16 INCSDR UIEA2025061200756Skin · crackedLEFT WING, INBOARD L/E (FIXED L/E) SKIN CRACKED AT KRAS 217.5 AROUND FASTENER HOLE (1EA) AND AT SEAL RIB (REF: KRAS 224.82) BETWEEN THE NOSE BEAM AND FIRST STRINGER (2EA).(<P>PERFORMED LH WING AT REF KRAS 224.82 AND REF KRAS 217.5 FIXED LEADING EDGE SKIN PANELSDR Y2PA2025061825006Skin Splice · corrodedDISCREPANCY: WHILE AT C-CHECK IN KBQK, STAMBAUGH AVIATION FOUND CORROSION ON THE L/H WING LOWER SURFACE AT STR. 17 (SKIN SPLICE) AND AT XCW 85. BLENDED OUT THE DAMAGED AREA, PERFORMED HFEC OPEN HOLE INSPECTION AND FABRICATED A REPAIR DOUBLER USING 2024T3 .12SDR SWAA2025072186072Access Panel · elongatedELONGATED HOLE ON ACCESS PANEL 551BB TRAILING EDGE AT LT WING. REPAIRED ACCESS PANEL 551BB TRAILING EDGE AT LT WING IAW SRM 51-70-04-2R-9 REPAIR 9.SDR CALA2025061805675Skin · corrodedRIGHT WING WINGLET ADAPTER PLUG T/E TOP SKIN INBD AREA WITH CORROSION. REPAIR ACCOMPLISHED PER EC/RA 5730-03596 AND VTMAE EA 5753-13-A3 935 REV - LP: 5221586SDR 2025FA0000404Skin · dentedACCOMPLISHED FR-700-0025-15113 - REV- DATED: 20MAY2025: FIELD REPAIR - DENT AND GOUGE, RH WING, LOWER SKIN, INBOARD OF RIB 2 AT STRINGER 03WL. PERFORM THE FOLLOWING INSPECTION AT 8000 HOURS AND THEN EVERY 4000 HOURS THEREAFTER. REMOVE ACCESS PANELS 612AB ASDR JR2R20250615812Skin · chafedRIGHT HAND WING LEADING EDGE PANEL, ABOVE PYLON, IS CHAFED OUT OF LIMITS. REPAIRED.SDR JR2R20250615811Skin · chafedLEFT HAND WING LEADING EDGE PANEL, ABOVE PYLON, IS CHAFED OUT OF LIMITS. REPAIRED.SDR 2025F00143Skin · dentedDISBOND ON THE UPPER WING BETWEEN THE OUTBOARD END OF STRINGER 2 (P/N 6922460-1) AND THE WAFFLE DOUBLER (P/N 7422087-5). A DENT IN THE WING UPPER SKIN (P/N 7422087-1). THE STRINGER IS DISBONDED A LENGTH OF 2.6 IN THE INBOARD AND OUTBOARD DIRECTION. THE DENT HSDR CALA2025061705613Skin · crackedLT WING FIXED L/E SKIN HAS A CRACK, 6'IN LENGTH UNDER SLAT #4. REMOVED REPAIRED AND REINSTALLED L/H WING FIXED L/E SKIN UNDER S LAT #4 IAW B757-300 SRM 51-40-02, SRM 51-70-07-0G-0.SDR YENA2025061700626Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE TOP SKIN LOWER SURFACE BTW RIB20 TO RIB21 ON RH WING IAW (CPCP FINDING); REF AEROMAN WO 2025-180/1 WCC#2025-298913 FOR WORK PERFORMED; PERFORMED REPAIR TRAILING EDGE TOP SKIN LOWER SURFACE BTW RIB20 TO RIB21 ONSDR YENA2025061700625Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE TIP SKIN LOWER SURFACE BETWEEN RIB 21 TO RIB 22 ON RH WING (CPCP FINDINGS); (RESOLVED ON W/O: 1389906 TASKCARD: NR-00042) AEROMAN WO# 2025 180/1 WCC 2025-2984859 FOR WORK PERFORMED; PERFORMED REPAIR TRAILING SDR YENA2025061700624Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE TOP SKIN LOWER SURFACE BETWEEN RIB 18 (PLUS 10") TO RIB 19 ON LH WING (CPCP FINDING); (RESOLVED ON W/O: 1389906 TASKCARD: NR-00044) AEROMAN WO 2025-180/1 NR 2025-298902 FOR WORK PERFORMED; PERFORMED BLEND OUT SDR YENA2025061700623Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE TOP SKIN LOWER SURFACE BETWEEN RIB 16 TO RIB 17 ON LH WING (CPCP FINDING); (RESOLVED ON W/O: 1389906 TASKCARD: NR-00053) AEROMAN WO 180/1 NR# 2025-298901 FOR WORK PERFORMED; PERFORMED PERMANENT REPAIR LOCATED SDR YENA2025061700622Skin · corrodedDURING HEAVY MAINTENANCE: AEROMAN WO# 180/1 NR# 2025-298911 FOR WORK PERFORMED: PERFORMED PERMANENT REPAIR LOCATED ON TRAILING EDGE, TOP SKIN, LOWER SURFACE OVERHANG AREA, BTW RIB 14 (PLUS 17 INCHES) TO RIB 15, LH WING AND FOUND WITHIN ALLOWABLE DAMAGE LIMITSSDR YENA2025061700621Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE TOP SKIN LOWER SURFACE BETWEEN RIB 15 (PLUS 16") TO RIB 16 ON LH WING; (RESOLVED ON W/O: 1389906 TASKCARD: NR-00055) REF TASK CARD 72179-01-1-575 JB WO# 1389906 PERFORMED REPAIR TRAILING EDGE TOP SKIN LOWER SUSDR YENA2025061700620Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE TOP SKIN LOWER SURFACE BETWEEN RIB 18 (PLUS 10 INCHES) TO RIB 19 ON LH WING; TASK CARD 572179-01-1-575 JB WO# 1389906 PERFORMED REPAIR LOCAION TRAILING EDGE TOP SKIN LOWER SURFACE RIB 18 PLUS 10 INCHES TO RIBSDR YENA2025061700619Skin · corrodedDURING HEAVY MAINTENANCE: CORROSION TRAILING EDGE TOP SKIN LOWER SURFACE BETWEEN RIB 16 (PLUS 15 INCHES) TO RIB 17 ON LH WING; (RESOLVED ON W/O: 1389906 TASKCARD: NR-00057) TASK CARD 572179-01-1-575 JB WO# 1389906 PERFORMED REPAIR LOCATED TRAILING EDGE TOP SKSDR YENA2025061700618Skin · damagedDURING HEAVY MAINTENANCE: WINGS / LH WING / TOP SKIN PANEL 2 / TEOH BTWN RIB 15 - 19 / LOWER SURFACE / CORROSION - PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 57-0046-25 REV 0 (COVER AND PARTS 1 - 4) /2/ AIRBUS RDAF 81592930/005/2025#A /3/ AIRBUS DOSSIER 8159SDR FDEA202506130930Panel · damagedLEADING-EDGE SKIN PANEL ASSEMBLY 114T2800-273 DAMAGED. REPAIRED L/H WING L/E SKIN PANEL (MPN 114T2800-273) AT OSS 560- OSS 580 IN REF TO B767 SRM 57-41-01-2R FIG 201, SHEET 3 REPAIR 1 AND B767 SRM 51-70-07, PAR 5.G, FIG 14.SDR SWAA2025072180825Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 561BB ( 7EA). REPAIRED ACCESS PANEL 561BB IAW SRM 51-70-04-2R-10 REPAIR 10.SDR EE4Y2025061222514Skin Panel · corrodedDURING ACCOMPLISHMENT OF ALLEGIANT TASK A32X-575167-01-1-001, LH WING LOWER SKIN UPPER SURFACE AT ACCESS PANEL 574BB CORROSION WAS FOUND. REPAIRED LH WING LOWER SKIN UPPER SURFACE AT SKIN PANEL 574BB CUTOUT INTERNAL AREA IAW COOPESA EO # COO-EO-2025-22322-R01 SDR SWIA2025090200015Access Panel · corrodedLEFT WING FUEL CELL ACCESS PANEL LANDING HAS MULTIPLE AREAS OF MINOR SURFACE CORROSION. BLENDED CORRODED AREA OF LT WING FUEL ACCESS PANEL LANDING 510AB IAW REO 601R-57-21-030 REV. -L,. PERFORMED UT REMAINING THICKNESS INSPECTION WITH REFERENCE TO NDTM PART 4SDR SWI2025F00722Access Panel · corrodedLH WING FUEL CELL ACCESS PANEL LANDING (510AB) HAS MULTIPLE AREAS OF MINOR SURFACE CORROSION (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESSSDR 2025FA0000394Landing · corrodedCORROSION ON FUEL PANEL LANDSSDR FDEA202506100872Doubler · crackedRIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 706 FOUND CRACK ABOUT 0.2 INCH. RT WING FIXED LEADING EDGE CRACKED BEADED DOUBLER AT STATION XOS 706 TRIMMED OUT PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. FABRICATED REPAIR DOUBLER (-3), FILLER (-1SDR JR2R20250610795Skin · wornLH WING TIP UPPER SKIN I/B 3 EA SCREWS PULLING THRU THE SKIN. REPAIREDSDR CALA2025061605572Panel · crackedRIGHT WING LEADING EDGE GAP PAN EL HAS A CRACK. REPAIRED RT WING L/E GAP PANEL. IAW SRM 57-41-01-2R-3 REPAIR 3.SDR CALA2025061105458Skin · crackedCRACK INDICATIONS FOUND AT RH SIDE WING FIXED LEADING EDGE UPPER SKIN AT FASTENER HOLES #9, #10 & #11, WHICH HAD BEEN PREVIOUSLY REEMED TO 2ND OVERSIZE. REF AAR N/R 9981585 ESFR INFORMATION ENTERED. ACCOMPLISHED REPAIR AT RH WING UPPER SKIN REF UAL EC/RA 5741-SDR CALA2025061005424Skin · crackedCRACK INDICATIONS FOUND AT LH SIDE WING FIXED LEADING EDGE UPPER SKIN PANEL AT HOLES #12, #13 & #14 , WHICH HAD BEEN PREVIOUSLY REEMED TO 2ND OVERSIZE. ACCOMPLISHED REPAIR AT LH WING LE FASTENERS REF: EC/RA 5741-01655 AND AAR ESR 8-12317,SDR SWI2025F00863Skin · crackedSUSPECTED CRACK LH WING LOWER SKIN AT WHEEL WELL CUTOUT RIB 3 (C-CHECK RO 07/03/2025)REMOVED CRACK ON LH WING LOWER SKIN BY CUTTING AWAY DAMAGED AREA. FABRICATED, DRILLED AND INSTALL FILLER/DOUBLER/TRIPLER REPAIR ON LOWER SKIN. REF: ETD2025-170-922726 REV: A SDR AALA202508205145Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE TOP SKIN PANEL LOWER SURFACE AT RIB 15 PLUS 7 INCHES. REPAIRED SKIN PANEL PER EA 366034SDR AALA202508184933Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE TOP SKIN PANEL LOWER SURFACE AT RIB 15. REPAIRED SKIN PANEL PER EA 366077.SDR VNAA20250715002Skin · wornWEAR ON AREA OF SETTLEMENT OF FAIRINGS (583AB, 586AB, 592AB, 595AB, 597AB) AT LH WING LOWER SKIN. WEAR ON AREA OF SETTLEMENT OF FAIRINGS (583AB, 586AB, 592AB, 595AB, 597AB) AT LH WING LOWER SKIN. WAS BLENDED OUT PER CRJ-900 SRM 51-12-00-001-001-A01 AND SETTLESDR VNAA20250715001Skin · wornWEAR ON AREA OF SETTLEMENT OF FAIRINGS (683AB, 686AB, 692AB, 695AB, 697AB) AT RH WING LOWER SKIN. WEAR ON AREA OF SETTLEMENT OF FAIRINGS (683AB, 686AB, 692AB, 695AB, 697AB) AT RH WING LOWER SKIN WAS BLENDED OUT PER CRJ-900 SRM 51-12-00-001-001-A01 AND AREA OFSDR 2025FA0000387Closeout Panel · corrodedCORROSION UNDER LH AND RH AFT WING TO FUSELAGE FAIRING SUPPORT STRUCTURESDR GTIA2025060538942Skin Panel · damagedLEFT WING - TOP SKIN PANEL 2 - RIB 9-10 UPPER & STRG11, TE OH: RIB 8-9 UPPER/LOWER, RIB 11 & RIB 14 LOWER - CORROSION. RIB 8-9 L 2.577 W 2.463 D .113, RIB 11 L 2.546 W 2.074 D .118, RIB 9-10 L 1.592 W .362 D .028, RIB 14 L 5.010 W 2.363 D .143. PERFORMED PESDR R61A2025060500279Skin · gougedLH WING LEADING EDGE LOWER SURFACE BETWEEN RIBS 1 AND 3 FOUND TO BE GOUGED IN FIVE LOCATIONS. LH WING LEADING EDGE LOWER SURFACE BETWEEN RIBS 1 AND 3 GOUGES IN FIVE LOCATIONS REPAIRED IAW ERJ 175 ETD2025-170-921624 AND ERJ SRM57-49-01 AD3, FIG 102SDR FDEA202506050839Skin · crackedDURING PERFORM UT & OPEN HOLE HFEC INSPECTION OF THE LEFT UPPER WING SKIN COMMON TO FASTENERS 0-5 AND FOUND 01EA CRACK AT HOLE #5 AS MARKED. LH WING UPPER SKIN IN RIB BAY 10 TRAILING EDGE #5 HOLE REPAIRED AS PER B777 SRM 51-40- 02-0G, SRM 51-40-04-0G, SRM SDR FDEA202506050838Skin · crackedDURING PERFORM UT & OPEN HOLE HFEC INSPECTION OF THE RIGHT UPPER WING SKIN COMMON TO FASTENERS 0-5 AND FOUND 01EA CRACK AT HOLE #5 AS MARKED. RH WING UPPER SKIN IN RIB BAY 10 TRAILING EDGE #5 HOLE REPAIRED AS PER B777 SRM 51-40- 02-0G, SRM 51-40-04-0G, SRSDR IXXA20250604006Skin · corrodedCORROSION ON LOWER SURFACE OF LEFT WING SKIN AT LONGERON L-8, WSTA. 208.5SDR IPXA2025062612503Panel · crackedCRACKS AT RH WING T/E UPPER FIXED PANEL FWD OF NO.2 SPOILER. DOT NO. 17-05 NOTE: THIS FAULT IS ALREADY DEFERRED. DO NOT CLOSE. <BR>CONTACT GWC TO UNASSIGN FROM WORK PACKAGE AFTER ALL THE DOCUMENTATION AND AUDIT REQUIREMENTS ARE SATISFIED.SDR SWAA2025061281011Skin · out of limitsFOUND IB WING LEADING EDGE SKIN REPAIR AT KRAS 166.23 TO BE COMMON TO 2 STRINGERS LOCATED FROM KRAS 150.82 TO KRAS 166.23 AND KRAS 166.23 TO KRAS 180; OUTSIDE OF SRM LIMITS. THE SKIN DENT COULD NOT BE REWORKED THEREFORE THE DAMAGE WAS REMOVED AND REPAIR WAS ASDR SWIA202507070602Skin · crackedR/H WING LOWER SKIN BETWEEN RIB 5 AND RIB 6 AT SPAT 2 HAS A SUSPECTED CRACK (C-CHECK RO 07/03/2025)REPAIRED R/H WING LOWER SKIN BETWEEN RIB 5-6 AT SPAR 2 BY APPLYING REPAIR EXTERNAL DOUBLER.SEE CONTINUATION CARD FOR WORK PERFORMED. REF ETD2025-170-922499SDR VNAA20250715038Skin · wornDURING INSPECTION OF THE RC TRFKE001VY3R WEAR ON SETTLEMENT AREA WAS DETECTED OF FAIRINGS (583AB,586AB,592AB,595AB,597AB) AT LH WING LOWER SKIN.ORRECTIVE ACTION: WEAR ON SETTLEMENT AREA OF FAIRINGS (583AB,586AB,592AB,595AB,597AB) AT LH WING LOWER SKIN WERE BLESDR VNAA20250715036Skin · wornDURING INSPECTION OF THE RC TRFKE001P4A1 WEAR ON SETTLEMENT AREA WAS DETECTED OF FAIRINGS (683AB,686AB,692AB,695AB,697AB) AT RH WING LOWER SKIN. CORRECTIVE ACTION: WEAR ON SETTLEMENT AREA WAS DETECTED OF FAIRINGS (683AB,686AB,692AB,695AB,697AB) AT RH WING LOWSDR VNAA20250715031Skin · wornDURING INSPECTION OF THE RC TRFKE001VY3R WEAR ON SETTLEMENT AREA WAS DETECTED OF FAIRINGS (583AB,586AB,592AB,595AB,597AB) AT LH WING LOWER SKIN. RRECTIVE ACTION: WEAR ON SETTLEMENT AREA OF FAIRINGS (583AB,586AB,592AB,595AB,597AB) AT LH WING LOWER SKIN WERE BLESDR VNAA20250715029Skin · wornDURING INSPECTION OF THE RC TRFKE001P4A1 WEAR ON SETTLEMENT AREA WAS DETECTED OF FAIRINGS (683AB,686AB,692AB,695AB,697AB) AT RH WING LOWER SKIN RECTIVE ACTION: WEAR ON SETTLEMENT AREA WAS DETECTED OF FAIRINGS (683AB,686AB,692AB,695AB,697AB) AT RH WING LOWER SK
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