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 FDEA202409121386Rib · corrodedTHE LWR BORE OF INBD JACK RIB WAS CORRODED ON L5 SPLR(LOCATION #3). ACCOMPLISHED THE REINFORCEMENT REPAIR AT LH #5 SPOILER INBD JACK RIB I.A.W FEDEX EA NO: T6-5740-T0380719 P1, SEQ NO:790, TITLE: WINGS- ATTACH FITTINGS- LH WING #5 SPOILER JACK RIB AT STA ASDR SWAA2024092336839Rib · crackedLH WING TRAILING EDGE CLIP BETWEEN THE MIDFLAP DEFLECTION RIB AND WEB IS CRACKED. (MPN 115A6260-1)<[01] LOCATED AND DRILLED FASTENER HOLES IN NEW CLIP PER SRM 51-40-05.;[02] LOCATED AND DRILLED FASTENER HOLES IN NEW CLIP PER SRM 51-40-05. INSPECTION C/W.;[03] SDR SWAA2024091336665Rib · crackedUPPER TAB ON LEFT WING DEFLECTION CONTROL RIB CRACKED/SEPARATED<[01] REMOVED DAMAGE; FLAP PEENED AREA AND TREATED AND PRIMED REF 57-51-02-2R-3.;[02] ACCOMPLISHED REPAIR 3 - LEFT WING INBOARD FIXED TRAILING EDGE DEFLECTION CONTROL RIB UPPER TAB CRACK DAMAGE REPSDR SWAA2024091336664Rib · crackedLEFT WING DEFLECTION CONTROL RIB ATTACHMENT CLIP UNDER FIXED UPPER PANEL CRACKED<[01] REPLACED LEFT WING DEFLECTION CONTROL RIB ATTACHMENT CLIP UNDER FIXED UPPER PANEL PER SRM 51-40-02SDR UIEA2024091000894Rib · corrodedCORROSION DAMAGES ON THE RIB OF LH WING FIXED T/E PANEL SUPPORT AT BS 1294.(<P>1. PERFORM EI NO: T2024A57M-1993 REV =1. 2. CONDITION CHECK NORMAL AND JOB COMPLETED.</P>)SDR HNAA2024101700988Rib · cracked57-2062 LH WING AT RIB 9 LWR SPLICE XIV CRACKED AT 3 HI-LOK HOLES. REPAIRED IAW EO1-57-24-0600SDR HNAA2024101700987Rib · cracked57-2061 RH WING AT RIB 9 SLICE XIV CRACKED AT 1 HY-LOK HOLE. REPAIRED IAW EO1-57-24-0600SDR LR7A2024090303504Bulkhead · leakingDURING SCHEDULED C-15 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH OUTER WING REAR BEAM LEAKING AT FS597, OWS18-59R. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. DRC# 0770.SDR IPXA2024092734608Rib · crackedCRACKED CHORD, L/H WING INBD T/E CAVITY RIB UPPER CHORD, WS 737. (REPAIR). ACCOMPLISH REPAIR PER EO-91290-REQ1 AND EGAT EI F2024A57M-2243, REV. 0 AND 1.SDR R61A2024083100380Rib · damagedDURING HEAVY CHECK FOUND RH WING AFT FACE SPAR 2 RIB 10 ELONGATED HOLE. REMOVED AND REPLACED RIB 10 RH WING AFT FACE SPAR 2. REF EMB SRM 51-40-08. ACFT REMAINS IN HEAVY CHECK UNTIL COMPLETIONSDR IPXA2024092595314Rib · crackedCRACKED UPPER CHORD, RH WING TE WBL 448.70 RIB (REPAIR). ACCOMPLISH REPAIR PER EO-91263-REQ1 AND EGAT EI F2024A57M-2242, REV. 0 AND 1.SDR IPXA2024093055314Rib · crackedCRACKED UPPER RIB CHORD, RT WING TE WBL 448.70. ACCOMPLISHED REPAIR PER EO-91263-REQ1 AND EGAT EI F2024A57M-2242, REV. 0 AND 1. OPENSDR UIEA2024083000861Support Rib · brokenRHW #16 K/FLAP AREA FWD L/E D-BEAM INNER SUPPORT RIB BROKEN.(<P><SPAN>RH #16 K/FLAP AREA FWD L/E D-BEAM INNER SUPPORT RIB BROKEN FABRICATED IAW RI-57-00-17048 REV.A AND REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02 REV.43. NO FURTHER DEFECTS NOTED.<SDR FDEA202408271178Support Rib · corrodedRH FWD LUG RIB 5 CORROSION FOUND IN BORE . REMOVED CORROSION FROM R/H MLG RIB 5 FWD LUG PER, E.A.6-5710-T0380346 PT 1SDR VNAA20251005003Rib · crackedCRACK ON RIB LEADING EDGE UPPER FACE SS=57.16 AT RH WING WAS REPAIRED PER REO 690-57-41-240 REV. - . CRACK ON RIB LEADING EDGE UPPER FACE SS=57.16 AT RH WING WAS REPAIRED PER REO 690-57-41-240 REV. - - .SDR VNAA20251005002Rib · crackedCRACK WAS FOUND ON RIB LEADING EDGE SS57.16 UPPER FACE T LH WING. CRACK WAS FOUND ON RIB LEADING EDGE SS57.16 UPPER FACE LH WING WAS REPAIRED PER REO 690-57-41-240 REV - -.SDR VNAA20251004005Rib · crackedCRACK ON RIB LEADING EDGE UPPER FACE SS=57.16 AT RH WING. CRACK ON RIB LEADING EDGE UPPER FACE SS=57.16 AT RH WING WAS REPAIRED PER REO 690-57-41-240 REV. - - .SDR VNAA20251004004Rib · crackedCRACK WAS FOUND ON RIB LEADING EDGE SS57.16 UPPER FACE T LH WING. CRACK WAS FOUND ON RIB LEADING EDGE SS57.16 UPPER FACE T LH WING WAS REPAIRED PER REO 690-57-41-240 REV - -.SDR VNAA20251004001Rib · crackedCRACK WAS FOUND AFFECTING AFT DRAG ANGLES AT LT VERTICAL STABILIZER BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM. PERMANENT REPAIR PERFORMED IN ACCORDANCE WITH CRJ-900 SRM 55-31-00-201-001-A01.SDR SWAA2024092030923Rib · crackedRT WING TE DEFLECTION CONTROL RIB CRACKED AT PANEL/SERRATED PLATE ATTACHED AREA.<[01] ACCOMPLISHED REPAIR OF R/W T/E DEFLECTION CONTROL RIB UPPER TAB PER SRM 57-51-02-2R-3.;[02] VERIFIED REPAIR OF R/W T/E DEFLECTION CONTROL RIB UPPER TAB;[03] REJECT....T/C TTGSDR IXXA20241002009Rib · gougedRH WING FIXED LEADING EDGE RIB IS GOUGED, JUST OUTBD OF #2 PYLON AT APPROX OFSS 450. STREAMER ATTACHED. HAECO WO 320008 NON ROUTINE 40324SDR SWAA2024091129620Rib · crackedLT WING T/E ANGLE RIB CRACK AT ORSS 261+13.<[01] REMOVED AND REPLACED LT WING T/E ANGLE RIB AT ORSS 261+13 IAW SRM 51-40-02.;[02] REMOVED AND REPLACED LT WING T/E ANGLE RIB AT ORSS 261+13 IAW SRM 51-40-02 AND IPC 57-50-00-25A.;[03] VERIFIED ACTION 2.<BR>JOB COSDR DALA2024081508188Rib · wornAIRCRAFT 3732, INITIAL INSPECTION: WEAR ON HOLES OF DEFLECTION CONTROL RIB OF INBOARD FIXED TRAILING EDGE WS 278.5 AT LH WING. CORRECTIVE ACTION: DEFLECTION CONTROL RIB OF INBOARD FIXED TRAILING EDGE WS 278.5 AT LH WING.WAS REPAIRED PER B737-800 SRM 57-51-02-2SDR FDEA202408141216Rib · wornTHE BOLT BORE LOCATION #4 DAMAGE ON R5 SPOILER JACK RIB. ACCOMPLISHED THE REINFORCEMENT REPAIR AT RH WING #5 SPOILER JACK RIB ABX175.875 I.A.W FEDEX EA NO:T6-5740-T0380389 P1, SEQ NO:977, TITLE:WINGS-ATTACH FITTINGS-RH WING #5 SPOILER JACK RIB AT STA175.87SDR ASAA2024081452154Rib · crackedRIGHT WING DEFLECTION RIB CRACKED. GROUNDED - YES. REPAIRED R/W DEFLECTION RIB IAW B737-700 SRM 57-51-02-2R-3.SDR SCNA20240820304Rib · crackedWORK ORDER FS240105 NR001: LH WING OUTER RIB P/N 737-5274-1 #18 HOLE AS A CRACK INDICATION. - - RESOLUTION: LH WING OUT RIB P/N 737-5274-1 #18 CRAKCED HOLE WAS REPAIRED IAW EA 24007 REV IRSDR WX0A2024081432155Rib · damaged(AIRCRAFT NOT GROUNDED) (DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 5000-0013: 33284-23 LH WING TRAILING EDGE, RIBLET E AT RIB 13 CORRODED / AT LH WING TRAILING EDGE , RIBLET E AT RIB 13 REPLACED AS PER AIRBUS DOSSIER 81427484 AND REPAIR DRAWINSDR FDEA202408051248Rib · chafedRH WING LEADING EDGE RIB GOUGE WAS FOUND ON THE UPPER FLANGE OF THE ANTI-ICE DUCT CUT-OUT AT STA WOFX-259.4 TRIMMED OUT AND INSTALLED THE REPAIR ANGLE AT RH WING LEADING EDGE RIB WOFX-259.4 I.A.W FEDEX EA NO:T6-5710-T0380442 P1, SEQ NO:984, TITLE:WING-BASISDR IPXA2024090677035Rib · crackedLH WING FIXED L/E STRUCTURE HAS CRACKED RIB JUST O/B OF KRUGER FLAP NEAR STA. 142. DOT 142-010. INSTALLED RIB P/N: A572419920200 BATCH: 4282208 WITH RIVET P/N: MS20470AD5-6 BATCH: 4139271, RIVET P/N: MS20470AD4-4 BATCH: 3997710, CHERRY RIVET P/N: CR3213-5-04 BSDR SWAA2024082922205Rib · crackedON THE LEFT WING OTBD FIXED TRAILING EDGE PANEL; THE OTBD ATTACH BRACKET AT THE DEFLECTION RIB IS CRACKED ALL THE WAY THROUGH.<[01] TRIMMED OUT DAMAGED UPPER TAB COMPLETELY FROM THE DEFLECTION CONTROL RIB IAW SRM 57-51-02-2R-3;[02] C/W HFEC INSP OF TRIMMED OUTSDR UIEA2024072300736Shim · migratedFUEL TANK LEFT WING, INTERNAL SURFACE, ON RIB 3 UPPER AND LOWER CHORDS WITH SEVERAL MIGRATED SHIMS FROM L6 TO FRONT SPAR.(<P>FUEL TANK LEFT WING, INTERNAL SURFACE, ON RIB 3 UPPER AND LOWER CHORDS WITH SEVERAL MIGRATED SHIMS FROM L6 TO FRONT SPAR. AREA ON LH WISDR ASAA2024072652146Rib · corrodedL/H WING I/B FLAP, #1 RIB HAS CORROSION ON LOWER AFT LEG INNER SURFACE. GROUNDED - YES. EVALUATED CORROSION, FOUND TO BE 100% MATERIAL LOSS. TRIMMED OUT CORRODED AREA 48.26MM X 19.05MM IAW A320 SRM 51-74-00/001 REV149-01MAY2024. L/H WING I/B FLAP REMOVED AND RSDR IXXA20240726004Rib · crackedLEFT WING L/E AIR LOAD RIB LOWER CORD CRACKED AT FWD END AT LES 540 LOCATED JUST AFT OF #4 SLAT.SDR YENA2024072501045Rib · crackedDURING HEAVY MAINTENANCE: CRACK ON RIB 17 AT FIXED LEADING EDGE LH WING; REF: TOMX W/O 2563 N/R-00106 RIB 17 WAS REPLACED PER EMB190 SRM 51-43-03, SRM 51-43-04 AND SRM 51-41-02.SDR 2024FA0000510Flange · crackedWHILE COMPLYING WITH PIPER SB1161D, CRACKING WAS DISCOVERED ON THE FLANGES IDENTIFIED BY THE SERVICE BULLETIN, ON BOTH WINGS. THE FLANGES WERE PART OF A PREVIOUSLY INSTALLED REPAIR KIT AND WERE NOT THE WING RIB'S ORIGINAL FLANGE. THE REPAIR KIT IS NOT AN ADEQUSDR DALA2024072207375Rib · crackedSHIP 3138 CRACK RIB ANGLE TELESCOPIC DUCT OB FIXED LEADING EDGE ON RH WING. CORRECTIVE ACTION: REPLACED RIB ANGLE LOCATED ON OUTBOARD SIDE OF TELESCOPIC DUCT FIXED LEADING EDGE ON RH WING AS PER A319 SRM 51-42-11-801 AND SRM 51-72-11. (0457617)SDR VNAA20250820003Rib · crackedCRACK ON RIB LEADING EDGE SS57.16 AT LH WING FRONT SPAR. THE LH WING FRONT SPAR, RIB LEADING EDGE SS57.16 WAS REPAIRED PER REO 690-57-41-240 REV -.SDR HNAA2024081300696Rib · crackedE045630 LH WING RIB 21 IS CRACKED. PERFORMED CUTOUT, FABRICATED AND INSTALLED NEW FABRICATED DOUBLER AND FILLER FOR LH WING RIB 21 IAW EMB 145 SRM 57-20-07 ITEM 4 FIG 203 AND EO1-57-24-0467SDR VNAA20250820013Rib · crackedCRACK ON INBD MACHINED RIB OF WS 163.00 TRAILING EDGE AT LH WING. CRACK ON INBD MACHINED RIB OF WS 163.00 TRAILING EDGE AT LH WING WAS REPAIRED PER REO 690-57-51-452 REV -.SDR VNAA20250820010Rib · crackedCRACK ON OUTB MACHINED RIB OF WS 163.00 TRAILING EDGE AT RH WING. CRACK ON OUTB MACHINED RIB OF WS 163.00 TRAILING EDGE AT RH WING WAS REPAIRED PER REO 690-57-51-450 REV - -SDR VNAA20250820009Rib · crackedCRACK ON OUTB MACHINED RIB OF WS 163.00 TRAILING EDGE AT LH WING. CRACK ON OUTB MACHINED RIB OF WS 163.00 TRAILING EDGE AT LH WING WAS REPAIRED PER REO 690-57-51-451 REV. -.SDR SWAA2024082612406Rib · crackedREF TTG8Q00UK2MT; CRACK FOUND ON THE LEFT WING FUEL VENT BOX AT RIB 6<SDR ASAA2024071152147Rib · corrodedR/W I/B FLAP, INBOARD RIB ASSY HAS CORROSION ON AFT LOWER LEG INNER SURFACE. GROUNDED - YES. EVALUATED CORROSION, FOUND TO BE 100% MATERIAL LOSS. TRIMMED OUT CORRODED AREA .950" X 1.350" IAW A320 SRM 51-74-00/001 REV149-01MAY2024. R/W I/B FLAP REMOVED AND REPLSDR HYIA20240711002Rib · crackedDURING MAINTENANCE A CRACK WAS DISCOVERED ON THE LEFT HAND CLOSEOUT RIB (P/N: 5122115-55) AT L.W.S. 106.79. THIS CRACK ORIGINATES FROM A HOLE IN THE FORWARD ROW OF FASTENERS COMMON TO THE AFT MAIN LANDING GEAR TRUNNION SUPPORT PLATE AND TRAVELS VERTICALLY TO ASDR HYIA20240711001Rib · crackedDURING MAINTENANCE THREE CRACKS WERE VISUALLY IDENTIFIED ON THE RIGHT HAND CLOSEOUT RIB (OEM P/N: 5122115-56). ALL CRACKS ARE LOCATED IN THE AREA OF FASTENERS COMMON TO THE FORWARD TRUNNION SUPPORT. THESE CRACKS ARE CONSISTENT WITH OTHERS THAT HAVE BEEN FOUND SDR DALA2024071006989Rib · crackedSHIP 3309 LEFT HAND WING / RIB 6 FITTING / FWD LUG CRACK. CORRECTIVE ACTION: COMPLIED WITH ERA 614005-14AD REV B. (0438135)SDR DALA2024071006988Rib · crackedSHIP 3309 LEFT HAND WING / RIB 6 FITTING / FWD LUG CRACK. CORRECTIVE ACTION: COMPLIED WITH ERA 614005-14AD REV B. (0438115)SDR IXXA20240816010Rib · crackedRIGHT WINGLET AFT ATTACH FRAME IS CRACKED INTERNAL JUST AFT OF UPPER AFT MOUNT BOLT. REF HAECO WO 320007 NON ROUTINE 38717SDR IPXA2024072753567Rib · cracked[STR] R/H WING. FIXED L/E COMPARTMENT HAS CRACKED RIB ANGLE LOCATED APPROX STA XORS 480. (015-10) ATA57.REMOVED RIB ANGLE DAMAGE AT R/H WING FIXED L/E COMP APPROX STA XORS 480 IN REF MD11 SRM 51-33-01.INSTALLED PROTECCION EWIS ON R/H WING FIXED L/E COMPARTMENTSDR WX0A2024081932159Rib · corroded(AIRCRAFT NOT GROUNDED) (DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 5000-0012: 33284-20 LH WING TRAILING EDGE , RIBLET L BETWEEN RIB 18 AND RIB 19 CORRODED / AT LH WING TRAILING EDGE , RIBLET L BETWEEN RIB 18 AND RIB 19 REPLACED AS PER AIRBUS
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