JASC 5712
Service difficulty reports · 6,959
Reports filed under 5712 · Wing, Rib/Bulkhead, 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 = '5712' 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 = '5712' 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 DALA2026020900920Rib · corrodedDEEP PITTING CORROSION FOUND THE RT RIB 6 FWD LUG. REPAIRED IAW ERA 631631-14AD REV ORIGINAL. (1441167)SDR SWIA2026013075742Rib · corrodedLEFT WING BATTERY RIB AT WS58.88, FWD LOWER ANGLE IS CORRODED THROUGH (601R10205-7). REMOVED AND REPLACED FWD LOWER ANGLE ON WS 58.8 LT BATTERY RIB REF. SRM 51-42-21 AND DWG. 601R10205 REV. -F.SDR R61A2026012800031Rib · crackedWHILE IN HEAVY CHECK, A CRACK WAS FOUND ON LT WING WHEEL WELL OPENING ON THE FWD EDGE, BETWEEN RIB 3 AND 4.SDR VNAA20260329036Rib · crackedCRACK ON RIB OF LEADING EDGE STA WS 58.00 AT RT WING. RIB OF LEADING EDGE STA WS 58.00 AT RT WING WAS REPAIRED PER REO 690-57-41-240 REV-.SDR VNA2026F00006Rib · crackedCRACK ON RIB OF LEADING EDGE STA WS 58.00 AT LH WING. RIB OF LEADING EDGE STA WS 58.00 AT LH WING WAS REPAIRED PER REO 690-57-41-240 REV. - -.SDR SWIA2026012675098Rib · damagedDAMAGE ON THE LT WING CANTED RIB LOCATED AT WS398.93 WAS FOUND TO BE OUT OF LIMITS PER SRM 57-21-12. DAMAGE IS OUT OF LIMITS AND THE REPLACEMENT OF THE STRUCTURALLY SIGNIFICANT ITEM IS CLISSIFIED AS A MAJOR REPAIR. REMOVED AND REPLACED THE LT CANTED RIB AT SDR JR2R20260122099Rib · damagedRIB 42 ON RT WING UNDER THE ENHANCED FAIRING HAS ENLARGED AND ELONGATED HOLE ON LOWER SIDE. REPAIREDSDR SWIA2026012175097Rib · damagedRIGHT WINGLET CANTED RIB DAMAGED AND REQUIRES REPLACEMENT. DAMAGE CONSIDERED MAJOR REPAIR PER GMM 3-26. REPLACED RT WINGLET CANTED RIB IAW SRM 51-42-21 & 51-42-22.SDR JR2R20260121173Rib · corrodedLEFT WING INBD MAIN FLAP TORQUE TUBE SUPPORT STRUCTURE RIB 1 HAS CORROSION IN MULTIPLE LOCATIONS. REPLACED PER SRM.SDR COEA2026041613801Rib · corrodedWO 269490 NR 600027 HEAVY CHECK COE/MAJOR REPAIR: R/H WING UPPER RIB 13 JUNCTION BOLT HOLE #1 HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIR PER SRAS ES_00278483_01...27237 ISSUE A, DATED 3/4/2026.SDR REXA2026030900225Rib · crackedCRACK ON MACHINED RIB OF LEADING EDGE SS57.16 AT RIGHT WING. MACHINED RIB OF LEADING EDGE SS57.16 AT RIGHT WING WAS REPAIRED PER REO 690-57-41-240 REV --SDR VNAA20260303016Rib · crackedCRACKED MACHINED WING RIB, LEADING EDGE SS58.41, RT WING. THE RIB WAS REPAIRED IAW REO 690-57-41-240, REV -.SDR VNAA20260303007Rib · crackedCRACKED LT WING L/E RIB SS 15.50. THE RIB WAS REPAIRED IAW REO 690-57-41-580, REV-.SDR IPXA2026021200615Rib · crackedLT WING 475AL HAS CRACKED RIB 7TH FROM FWD END AT BOTTOM-QC 109-VWV REMOVED CRACKED RIB ON 475AL PANEL IAW A300-600F SRM 51-40-21. INSTALLED RIB 7 AND DOUBLER AT RIB 7 USING FASTNERS P/N NAS1097DD-6 B# 0004244840, P/N MS20426DD5-7 B# 0004372118 IAW A300-600-SRSDR IPXA2026011563643Rib · crackedMAJOR REPAIR, LT WING, CENTER FLAP, TOP SKIN RIB FLANGE, 1 CRACK INDICATION NOTED AT RIB 13. CIRCLED IN RED. REMOVE RIB 25 STIFFENER A57960437205 BETWEEN STRINGER 2.8 AND REAR SPAR BY APPLICATION OF AN INCISION MIDWAY EXISTING FASTENER POSITIONS AS PER FIGUSDR SWAA2026020960949Rib · wornRIGHT WING TRAILING EDGE, DEFLECTION CONTROL RIB UPPER TRAILING EDGE ATTACH BOLTS, SHIM PLATE AND FASTENER HOLES ARE WORN. REMOVED DAMAGE FROM DEFLECTION CONTROL RIB UPPER TAB IAW SRM 51-10-02. MEASURED DAMAGE DEPTH TO BE .016". DAMAGE FOUND TO BE WITHIN ASDR R61A2026012700017Rib · crackedCRACK AT AFT RIB, LT WHEEL WELL. RIB HAS BEEN REMOVED AND REPLACED IAW SRM 51-41-01.SDR UIEA2025123001362Rib · corrodedLH WING FIXED LEADING EDGE RIB CORROSION. REMOVED CORROSION AT LH WING FIXED LEADING EDGE RIB AS PER SRM 57-41-13-1A-1 ILES 338.33-ILES 375.50 L: 1.1"" W: 16.15"", ILES 375.50 - ILES 414.50 L: 1.1"" W: 29.92". PERFORMED SURFACE HFEC INSPECTION AT LH WING FIXESDR REXA2026030900183Rib · crackedCRACK ON MACHINED RIB OF LEADING EDGE ON SS57.16 SIDE LEFT WING CRACK ON MACHINED RIB OF LEADING EDGE ON SS57.16 SIDE LEFT WING WAS REPAIRED REO 690-57-41-240 REV.-SDR REXA2026030900168Rib · crackedCRACK ON MACHINED RIB LEADING EDGE SS57.16 AT RIGHT WING. CRACK ON MACHINED RIB LEADING EDGE SS57.16 AT RIGHT WING WERE REPAIRED PER GREO 690-57-41-240 REV--SDR SWIA2025121975902Rib · crackedRIGHT WING L/E RIB AT WS 58.41 CRACKED. PERFORMED REPAIR ON RT WING L/EDGE RIB AT WS58.41 IAW SRM 51-42-15, AMM 57-41-32, REO 690-57-41-582 REV--(P1), REO 690-57-41-582, REV-. PERFORMED INSPECTION.SDR SWIA2025121975900Rib · crackedLEFT L/E RIB AT WS 58.41 CRACKED. PERFORMED REPAIR AT LT LE RIB IAW SRM 53-24-15, 51-25-16, AMM 57-41-32, &REO 690-57-41-581, REV -. PERFORMED NDT INSPECTION.SDR SWIA2025121776360Rib · crackedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA93275-601R-57-51-1052 REV -. COMPLY WITH PERMANENT REPAIR ON RA ID: 93275THE LHS WING TE RIB AT WS130.10 HAS BEEN REPAIRED DUE TO BEND AND CRACK DAMAGE PER REO 601R-57-51-1052 REV -- DATED 2024-08-29. PERMANENT REPAIRSDR VNAA20251216016Rib · crackedCRACK ON RIB LEADING EDGE SS57.16 WAS FOUND AT LH WING. CRACK ON RIB LEADING EDGE SS57.16 WAS FOUND AT LH WING WAS REPAIRED PER REO 690-57-41-240 REV-.SDR VNAA20251216017Rib · crackedCRACK ON RIB LEADING EDGE SS57.16 WAS FOUND AT RH WING. CRACK ON RIB LEADING EDGE SS57.16 WAS FOUND AT RH WING WAS REPAIRED PER REO 690-57-41-240 REV-.SDR SWIA2025121575798Rib · corrodedRH BATT RIB AT APPROX WS 53.60 BEHIND LH MLG TIRE BURST PANEL HAS EVIDENCE OF CORROSION. (MARKED) (C-CHECK RO 04/17/2026)REMOVED CORROSION FROM THE RIGHT-HAND BATT RIB AT APPROX. WS 53.60, BEHIND THE LEFT-HAND MAIN LANDING GEAR TIRE BURST PANEL, AND EVALUATESDR CALA2025122912457Rib · crackedLEFT WING, UPPER OUTBOARD TRAILING EDGE FIXED PANEL WITH CRACK ON THE INBOARD WALL. CRACK LENGTH: 8 IN APPROX.(REF AAR NR 1000063266) ESFR GENERATED. ESFR #2598 SUBMITTED AND UPLOADED TO AAR NR 1000063266. REMOVED AND REPLACED RIB ON LH WING O/B FIXED T/E BTWSDR SWIA2025120876572Rib · crackedRT WING BATTERY RIB IS CRACKED AT WS 14.50. INSTALLED NEW RT WING BATTERY RIB AT WS 14.50 . IAW SRM 51-42-21-001-001-A01, SRM 51-42-22-001-001-A01. AND DWG CC690-10610, REV. D. .SEE CONTINUE CARD FOR DETAILSCOMPLIED WITH TASK CARD 51-900-1002.SDR CALA2025120811926Rib · crackedACCOMPLISH INSPECTION ON THE RT WING I/B FIXED TRAILING EDGE AUX D RIB. REPAIRED RT WING I/B FIX T/E AUX D-RIB ASSEMBLY UPPER O/B FLANGE REPAIR IAW ECRA 5733-01054 REV A VERIFIED ECRA 5733-01054 IS ACCOMPLISHED IN ITS ENTIRETY TO BE DIPPED PER PART 1 INTERIMSDR REXA2026052700750Rib · crackedCRACK ON MACHINED RIB LEADING EDGE SS57.16 AT LEFT WING. CRACKED MACHINED RIB LEADING EDGE SS57.16 AT LEFT WING WAS REPLACED PER SRM 51-42-06-001-001-A01 AND SRM 51-42-10-001-001-A01SDR REXA2026052700749Rib · crackedCRACK ON WING RIB LEADING EDGE SS27.16 AT LEFT WING. CRACKED RIB LEADING EDGE SS27.16 AT LEFT WING WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND CRJ-900 SRM 51-42-10-001-001-A01 AND ELONGATE HOLES WERE REPAIRED PER EA NO. CRJ957-21136 REV A.SDR REXA2026052600655Rib · crackedCRACK ON WING RIB LEADING EDGE SS27.16 AT RIGHT WING. CRACK ON WING RIB LEADING EDGE SS27.16 AT RIGHT WING. WAS REPAIRED PER CRJ957-20951 REV IRSDR UIEA2025111801309Rib · corrodedCORROSION ON RIB OF LT WING FIXED TE PANEL SUPPORT AT B.STA 1294, WL 128.57. ACCOMPLISHED EI T2025A57M-2429 REV 1. CHECKED NORMAL.SDR SWIA2025112100017Rib · damagedDAMAGE ON THE RT WINGLET RIB LOCATED AT RIGHT SIDE WGLTS3.25 WAS FOUND TO BE OUT OF LIMITS PER SRM 57-31-14 . DAMAGE IS OUT OF LIMITS AND THE REPLACEMENT OF THE STRUCTURALLY SIGNIFICANT ITEM IS CLISSIFIED AS A MAJOR REPAIR. REPLACED RT WINGLET RIB P/N 600-1SDR SWIA2025111800007Rib · damagedDAMAGE ON THE RH WING PLUG RIB LOCATED BETWEEN WS353.00 AND WS 389.00 WAS FOUND TO BE OUT OF LIMITS PER SRM 57-21-12 . DAMAGE IS OUT OF LIMITS AND THE REPLACEMENT OF THE STRUCTURALLY SIGNIFICANT ITEM IS CLISSIFIED AS A MAJOR REPAIR. OPENSDR VNAA202601180008Rib · crackedCRACKED WING RIB FLS168.07 AT WING TRAILING EDGE STRUCTURE OF RH WING. WING RIB FLS168.07 AT WING TRAILING EDGE STRUCTURE OF RH WING WAS REPAIRED PER REO 690-57-51-492 REV - -SDR VNAA202601170015Rib · crackedCRACK ON MACHINED RIB OF LEADING EDGE SS57.16 AT RH WING. MACHINED RIB OF LEADING EDGE SS57.16 AT RH WING WAS REPAIRED PER REO 690-57-41-240 REV - -SDR JJBA20251120089Rib · damagedRIGHT HAND MIDDLE LEADING EDGE DAMAGED ON REMOVAL AND HAS DAMAGE ON INBOARD EDGE. REMOVED AND REPLACED RH MIDDLE LEADING EDGE INBD RIB.SDR AALA202511105596Rib · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT HAND WING FIXED LEADING EDGE RIB, AT UPPER PANEL LANDING FLANGE, AT ISS 435. REPAIRED RIB PER EA 369548.SDR EE4Y2025110523420Rib · corrodedDURING THE ACCOMPLISHMENT OF TASK CARD 57-50-033-1295, AZORRA AVIATION IDENTIFIED CORROSION ON THE RH WING IINBOARD FLAP RIB 1 LOWER FLANGE. THIS CONDITION WAS REPORTED ANDREPAIRED IAW ETD2025-190-925075 DTD JUL 24 2025 AND DOCUMENTED BY COOPESA COO-EO-2025-22SDR EE4Y2025110523419Rib · corrodedDURING THE ACCOMPLISHMENT OF TASK CARD 57-50-033-1295, AZORRA AVIATION IDENTIFIED CORROSION ON THE RH WING INBOARD FLAP RIB 1 LOWER FLANGE. THIS CONDITION WAS REPORTED AND REPAIRED IAWETD2025-190-925074 DTD JUL 24 2025 AND DOCUMENTED BY COOPESA COO-EO-2025-227SDR REXA2025121201031Rib · crackedCRACK ON MACHINED RIB LEADING EDGE SS57.16 AT LEFT WING. MACHINED RIB LEADING EDGE SS57.16 AT LEFT WING WAS REPAIRED PER REO 690-57-41-240 REV - -SDR REXA2025121201027Rib · crackedCRACK ON MACHINED RIB LEADING EDGE SS57.16 AT RIGHT WING MACHINED RIB LEADING EDGE SS57.16 AT RIGHT WING WAS REPLACED PER CRJ 900 SRM 51-42-21-001-001-A01 AND SRM 51-42-10-001-001-A01SDR VNAA20251204018Rib · crackedCRACK ON OTBD MACHINED RIB OF WS 163.00 TRAILING EDGE AT LH AND RH WING CORRECTIVE ACTION: CRACK ON OTBD MACHINED RIB OF WS 163.00 TRAILING EDGE AT LH AND RH WING WERE REPAIRED PER REO 690-57-51-488 REV. - AND REO 690-57-51-487 REV. - -SDR HNAA2025112500821Rib · crackedLEFT WING, UPPER SECTION OF RIB 21 IS CRACKED. INSTALLED DOUBLER AND FILLER ON LH WING UPPER SECTION OF RIB 21. IAW EMB 145 SRM 57-20-07-RE, ITEM 4, FIG. 203, DET. C. AND E01-57-25-0425SDR SWAA2025111729694Tab · crackedRIGHT WING T/E DEFLECTION CONTROL RIB UPPER TAB CRACKED. REPAIRED RIGHT WING T/E DEFLECTION CONTROL RIB UPPER TAB IAW SRM 57-51-02-1A-1, SRM 57-51-02-2R-3, AND AMM 57-50-01-820-801.SDR REXA2025121201016Rib · crackedCRACK ON MACHINED RIB OF LEADING EDGE SS27.16 AT RIGHT WING. CRACK ON MACHINED RIB OF LEADING EDGE SS27.16 AT RIGHT WING WAS REPAIRED PER REO 690-57-41-569 REV - -SDR IXXA20251026005Rib · corrodedCORROSION ON THE FWD END OF THE RIB IN THE RIGHT WING L/E AT THE O/B SIDE OF #10 SLAT I/B AUX TRACKSDR IPXA2025103141487Rib · crackedFAULT: RH WING, CENTER FLAP, TOP SKIN RIB FLANGE, 1 EA CRACK INDICATION NOTED AT RIB 11. CIRCLED IN RED. ++PERFORM RIB 11 REPAIR IN ACCORDANCE WITH FIGURE 5, TAKING EXISTING FASTENER PATTERN INTO ACCOUNT INSTALLING SOLID RIVETS PER DRAWING REQUIREMENTS AT THESDR DALA2025102407794Rib · damagedHOUR GLASS PANEL LOWER WING RIB, UPPER ROW, FWD FASTENER HOLE DAMAGED. REPAIRED PER PRI 630032-14 REV. 0, 1 AND 2 AND ER/A 630032-14 REV ORIGINAL. (1267567)
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