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 CALA2025022600452Skin · corrodedL/H WING UPPER SURFACE CORROSION AT SKIN APROX 3 INCHES FWD OF I /B FWD CORNER OF #1 SPOILER.SDR JR2R20250224686Access Panel · damagedPANEL 522DB HAS A DAMAGED FASTENER HOLE.SDR SWIA2025040400223Access Panel · crackedDURING "OK TO CLOSE" INSPECTION OF THE LEFT WING FUEL PNLS, DISCOVERED A POSSIBLE CRACK IN THE LEFT WING RIB AT LBL 22.50. (MARKED) (C-CHECK RO 04/04/2025)COMPLIED WITH ALL THE STEPS OF REO 670-57-11-226 REV -- DATED 2025-03-24. INSTALLED -1 REPAIR ANGLE - SHSDR SWAA2025032698925Skin · pulled(147-73 ) R/H WING L/E INBOARD OF THE NACELLE STRUT SKIN HAS PULLED FASTENERS (MARKED) AFT END<[01] 04 - REPAIRED PER [SRM 57-41-01-2R-7-A01177 (REPAIR 7 - WING INBOARD FIXED LEADING EDGE SKIN - LOOSE OR MISSING FASTENER REPAIR - CAT A REPAIR - PERMANENT)];[02SDR SWAA2025032698926Skin · pulled(147-74) R/H WING L/E SKIN INBOARD OF THE NACELLE STRUT HAS PULLED FASTENER (MARKED) AFT AND I/B END<[01] 01 - REMOVED AND REPLACED PER [SRM 57-41-01-2R-7-A01177 (REPAIR 7 - WING INBOARD FIXED LEADING EDGE SKIN - LOOSE OR MISSING FASTENER REPAIR - CAT A REPAIRSDR YENA2025022500198Access Panel · damagedDURING HEAVY MAINTENANCE: ELONGATED HOLES ON FUEL ACCESS PANEL 640MB CUT OUT BTW RIB 17 TO RIB 18 ON RH WING (2 EA); (RESOLVED ON W/O: 1348393 TASKCARD: NR-00025 ) REF AEROMAN WO 2025 13/1 NR 2025-29526; PERFORMED PERMANENT REPAIR ON BOTTOM SKIN CUT-OUT BTW RISDR SWIA20250312221Skin · damagedTRANSFER FROM EAML 1541896 : REF EAML 1539813 INSPECTED RT WING AND FOUND MULTIPLE AREAS OF DAMAGE TO THE RT WING TIP FAIRING AND RT WING NAV LIGHT ASSEMBLY. ALSO FOUND UNDERLYING INSTALLATION STRUCTURE DAMAGE AS LISTED IN REO 601R-57-00-201 TABLE 1, SHEET 6. SDR CALA2025022400431Skin · crackedPER ECRA 5725-01156 PART 1, STEP 3 - AFTER MAY 18, 2026, BUT BEFORE JUNE 18, 2026, PLANNING TO CONTACT ENGINEERING FOR THE INSPECTION REQUIREMENTS OF THE INTERIM REPAIR INSTALLED ON THE RIGHT WING OUTBOARD LOWER SKIN PANEL BETWEEN WSTA 564.5 & 591.5 AT STR L-9SDR DALA2025022301383Skin · damagedSHIP 3230 DISC: RT WING TIP DAMAGED ON TOW UP FROM REMOTE PARKING. ACFT OOS. C/A: RT WING TIP FENCE PREVIOUSLY REMOVED. INSTALLED NEW WINGTIP FENCE IAW A320AMM 57-31-22-400-001-A. CDL AND PLAC REMOVED. M PROCEDURES REVERSED. (LP: 6367904)SDR SIMA20250220002Skin · chafedCHAFE ON UPPER EXTERNAL SKIN OF RH WING FIXED LEADING EDGE JUST OUTBD OF #4 SLAT OUTBD WAI HARNESS TUBE (MAJOR REPAIR) RAR RH WING FIXED LEADING EDGE SKIN JUST OUTBOARD OF #4 SLAT OUTBOARD WAI HARNESS TUBE IAW EMB 175 SRM 51-40-08.SDR SIMA20250218003Skin · gouged3 GOUGES ON LH WING RIB 32 FIXED L/E. (MAJOR REPAIR) REMOVED AND REPLACED L/H WING FIXED L/E AT RIB 32 IAW EMB 170 SRM 51-40-08.SDR SIMA20250218001Skin · gougedRH WING L/E GOUGED (3EA) INBD OF RIB 20. (MAJOR REPAIR) REMOVED AND REPLACED RH WING FIXED L/E INBD OF RIB 20 IAW EMB 170 SRM 51-40-08.SDR SWAA2025032497293Access Panel · crackedCRACK INTERNAL CAVITY OF ACCESS PANEL 644BB AT RT WING 2025-139248<[01] PERFORMED PERMANENT REPAIR ON ACCESS PANEL 644BB AT RT WING IAW EA 25-157-00561. AND STEPS ARE DOCUMENTED ON FAULT TTG8Q00Z2CLP. SEE INDIVIDUAL SIGNOFFS BELOW.;[02] PERFORMED PERMANENT REPSDR 2025F00044Skin · debondedDISBOND AND CONTOUR DEVIATIONS, LH AND RH WING, UPPER SKIN BOND ASSEMBLIES, STRINGER ENDS. ACCOMPLISHED FR-680A-0229-14754 REV - DATED 2-13-2025 AND FAA FORM 8110-3 DATED 02/13/2025; FIELD REPAIR - DISBOND AND CONTOUR DEVIATIONS, WING, UPPER SKIN BOND ASSEMBLISDR 2025FA0000475Stiffener · crackedR/H WING FWD LWR I/B SKIN. AFT STIFFENER CRACKED.SDR AALA202505056630Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TOP SKIN PANEL LOWER SURFACE AT WMRX4567.249 AND RIB 14. REPAIRED SKIN PANEL PER EA 362466.SDR AALA202505059092Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TOP SKIN PANEL LOWER SURFACE AT WMRX5097.109 AND RIB 15. REPAIRED SKIN PANEL PER EA 362466.SDR AALA202505057776Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TOP SKIN PANEL LOWER SURFACE AT WS 3758 AND RIB 7. REPAIRED SKIN PANEL PER EA 362689.SDR SWAA2025032497121Access Panel · crackedCRACK ACCESS PANEL 667BT OB FOREFLAP AT RT WING 2025-136944<[01] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26.;[02] REPLACED RH WING ACCESS PANEL 667BT OB MAIN FLAP IAW EA-25-157-00562 WIP1 ; EA-25-157-00562 WIP2; SDR 2025FA0000111Skin · debondedDEBONDING OF LH AND RH WING UPPER SKIN ASSEMBLY STRINGER ENDS: ACCOMPLISHED INJECTION OF ADHESIVE INTO DEBONDED AREA AND ADDED FASTENERS TO THE END OF THE AFFECTED STRINGERS. VERIFIED NO CRACK INDICATIONS EXIST IN THE UPPER WING SKIN IN THE DEFECT AREAS AND RESDR 2DYA2025F00043Skin · separatedFLIGHT FROM AFW TO YYZ, AFTER LANDING MECHANIC DURING POST FLIGHT INSPECTION DISCOVERED THAT THE S51MT (ATA 57 - INBOARD WING TRAINING EDGE) PANEL HAD PARTIALLY DEPARTED THE AIRCRAFT. APPEARS THE PANEL FASTENERS WERE NOT PROPERLY INSTALLED.SDR JR2R20250215470Skin · chafedR/H WING FIXED LEADING EDGE OVER PYLON HAS CHAFE MARKS.SDR JR2R20250215460Skin · chafedL/H WING FIXED LEADING EDGE OVER PYLON HAS CHAFE MARKS.SDR JR2R20250215363Skin · chafedL/H WING FIXED LEADING EDGE UPPER/LOWER SKIN ARE CHAFED/SHOWING BARE METAL AT MULTIPLE PLACES.SDR SWAA2025030696222Panel · crackedR/W T/E PANEL 651FB HAS A CRACKED L-CLIP ON FWD SIDE 27' FROM O/B END<[01] REMOVED CRACKED L-CLIP AND REPLACED WITH NEW IAW SRM 51-40-02-0G-0 AND DWG 115A2710 REV. B.;[02] VERIFIED CORRECTIVE ACTION 1SDR CALA2025021700370Access Panel · crackedR/W T/E ACCESS PANEL 651GB FWD SEAL RETAINER CRACK REF AAR N/R 9937701 REMOVED AND REPLACED R/W T/E ACCESS PANEL 651GB FWD ACCESS PANEL 651GB FWD SEAL RETAINER PER SRM 51-40-02-0G-0 AND IPC 27-51-00-15.SDR R61A2025021400085Skin · crackedDURING OVERNIGHT INSPECTION FOUND RH WING LOWER SKIN CRACKED JUST INBD OF RIB 17 AND JUST AFT OF FWD SPAR APROX 1.2 INCHES LONG. REPAIRED IAW ETD2025-170-901928 ALSO REF VP-002193-2025 N/R #3 FOR WORK ACCOMPLISHED.SDR DALA2025030401653Access Panel · missingLH WING LANDING LIGHT TOOLING ACCESS COVER MISSING. MAINTENANCE DEFERRED IT TO MONITOR PER ERA 607941-14TR REV ORIGINAL. C/W TEMP REPAIR PER SECTION I. ENGINEERING APPROVED REPAIR PER DAL P.S. 900-5-1, #04. REPETATIVE CHECK DUE EVERY 50 FLIGHT HOURS, TERMINATISDR AALA202502288005Skin Panel · wornAIRCRAFT IN BASE MAINTENANCE: WEAR MARKS ALONG THE UPPER EXTERNAL SURFACE OF LEFT WING FIXED LEADING EDGE UPPER ACCESS PANEL JUST INBOARD OF ENGINE STRUT. REMOVED AND REPLACED NEW ASSEMBLY SKIN AT LEFT HAND WING FIXED LEADING EDGE UPPER ACCESS PANEL JUST INBOASDR IPXA2025021271069Skin · crackedLH WING LEADING EDGE UPPER SURFACE AT SLAT #4 LOCATION, HAS 1 CRACK. DOT 28-38. MADE A REPLACEMENT SKIN FROM 2024-T3 CLAD SHEET, 0.100''. PER E.A. #: 757-5741-27-A3790 PRELIMINARY 1, STEP 8. P/N: 2024-T3 .100C, BATCH: 0004322815. INSTALLED FASTENERS CODE A, B SDR CALA2025021100336Skin · gougedLEFT WING INBOARD LEADING EDGE, AT OUTBOARD LEADING EDGE FAIRING PANEL HAS DEEP GOUGE (INBOARD OF NACELLE STRUT) REF AAR N/R 9937057 REMOVED AND REPLACED PANEL 511A PN:116A4412-J AT LEFT WING INBOARD LEADING EDGE AT OUTBOARD LEADING EDGE FAIRING PANEL IAW B737SDR DALA2025021301134Skin · damagedSHIP 6809 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 616812-14AD REV A. CORRECTIVE ACTION: REF ERA 616812-14AD. (0803679)SDR SWAA2025030494420Skin Panel · delaminatedDELAMINATED FIXED TRAILING EDGE SKIN PANEL UPPER SURFACE AT LH WING 2025-93409<[01] TOOLS USED= CALIPER P/N: 500-197-30; S/N: B20189571; DUE DATE: 06-JUN-25;[02] TOOL USED= SCALE P/N: CR5200; S/N: 8342514625; DUE DATE: 24-FEB-25;[03] TOOL USED= HOT BONDER P/N:SDR SWIA20250331206Skin · chafedS/N 0412RIGHT WING LOWER WING PLANK ACCESS HOLE 640BB HAS CHAFING AND PIN HOLES AROUND IT'S CIRCUMFRANCE. FLAGGED (C-CHECK RO 03/30/2024)REPAIRED RH WING LOWER WING PLANK ACCESS HOLE 640BB IAW REO 601R-57-21-030 REV -L DATED: 2014-02-05 AND REO 601R-57-21-3899SDR IPXA2025022211516Skin · crackedRH WING XORS 372-402 L.E. EXTERNAL SURFACE LWR SIDE HAS CRACKED AS MARKED. 74-002 ATA CODE 57. ACCOMPLISHED REPAIR PER MD-11F- SRM 57-40-01-2R-17 REPAIR 17 FIGURE 201 REV 71.SDR YENA2025020600136Skin · corrodedDURING HEAVY MAINTENANCE: WINGS / RH WING / TOP SKIN PANEL 2 / REAR SPAR - TE OVERHANG RIBS 13-16 / EXISTING REPAIR PLATE / CORROSION – TEMPORARY REPAIR; REFERENCES: /1/ AEROMAN EA 57-0003-25 COVER & PARTS 1 THRU 3 /2/ AIRBUS RDAF 80004053/048/2024 ISSUE A /3/SDR FDEA202502060182Skin · crackedUT & OPEN HOLE HFEC INSPECTION ON THE RH WING WBL 262 THEN FOUND HOLE #5 CRACKS IN UPPER WING SKIN AS MARKED. RH WING UPPER SKIN WBL 262 #5 HOLE REPAIRED AS PER B777 SRM 51-40-02-0G. 51-10-01-0G. 51- 20-06-0G. 51-40-05-0G. 51-20-01-0G. 51-50-02-0G. 51-40-08SDR DALA2025020600937Access Panel · corroded(LOG 0797654) CORROSION ON FUEL ACCESS PANELS RINGS 532AB, 532NB, 532FB, 532LB, 532CB,532JB (ALSO CORROSIOIN ON RING SETTLEMENT AREA), LH WING. FUEL ACCESS PANELS RINGS 532AB, 532NB, 532FB, 532LB, 532CB,532JB AND RING SETTLEMENT AREA LH WING WERE REPAIRED PER SDR DALA2025020600936Access Panel · corroded(LOG 0797653) CORROSION ON FUEL ACCESS PANEL RINGS 632HB, 632GB, 632EB, 632QB, 632NB, 632FB, 632KB, 632LB, 632JB RH WING. FUEL ACCESS PANEL RINGS 632HB, 632GB, 632EB, 632QB, 632NB, 632FB, 632KB, 632LB, 632JB RH WING WERE REPAIRED PER B737-800 SRM 57-20-01-2R RSDR AALA202502057216Access Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING ACCESS PANEL 640JB COUNTERSUNK FASTENER HOLES. REPLACED ACCESS PANEL 640JB PER SRM 51-72-11SDR DALA2025020500876Skin · crackedTHE #14 FASTENER HOLE SHOWS MULTIPLE CRACK INDICATIONS WITH BHEC IN SPAR AND SKIN LAYERS. RH WING REAR SPAR LOWER SURFACE. MARKED. SUMMARY SEE NRC 003-0001:0514-2001/025 00025: NR TRANSFERRED TO H-CK PKG#P-384718220250123 - NR# 32. (LP #0795831)SDR DALA2025020400821Skin · corrodedSHIP 3136 CORROSION LOWER SKIN LOCATED BTW RIB 15 TO RIB 16 T RAILING EDGE OF LH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS PER ER/A 621980-14. (0789351)SDR DALA2025020400820Skin · corrodedSHIP 3136 CORROSION ON LOWER SKIN LOCATED BTW RIB 8 TO RIB 9 TRAILING EDGE OF LH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS AS PER ER/A 621980-14. (0789347)SDR DALA2025020400819Skin · corrodedSHIP 3136 CORROSION ON LOWER SKIN LOCATED AT RIB 10 TRAILING EDGE OF LH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS AS PER ER/A 621980-14. (0789338)SDR DALA2025020400818Skin · corrodedSHIP 3136 CORROSION EXTERNAL SKIN UPPER SURFACE AT RIB 9 LH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS AS PER ER/A 621980-14. (0789330)SDR DALA2025020400817Skin · corrodedSHIP 3136 CORROSION ON LOWER SKIN LOCATED AT RIB 10 TRAILING EDGE OF LH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS AS PER ER/A 621980-14. (0789317)SDR DALA2025020400816Skin · corrodedSHIP 3136 CORROSION ON LOWER SKIN BTW RIB 16 TO RIB 17 TRAILING EDGE OF LH WING. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS AS PER ER/A 621980-14. (0789146)SDR R61A2025020300083Skin · crackedDURING OVERNIGHT BI WEEKLY INSPECTION FOUND LH WING LOWER SKIN CRACKED JUST INBD OF RIB 17 AND JUST AFT OF FWD SPAR APROX 3.75 INCHES LONG. REPAIRED IAW ETD2025-170-900813 ALSO REF VP-001195-2025 N/R #3 FOR WORK PERFORMED.SDR AALA202501312731Access Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING FUEL ACCESS PANEL 640HB FASTENER HOLE. REPLACED ACCESS PANEL PER TASK CARD 26C64057007SDR JR2R20250130134Skin · damagedLH SIDE BETWEEN UPPER SKIN AND WING UPPER SKIN - GAP CHECK FAILED AT WING TIP
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