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 AALA202510216734Rib · wornAIRCRAFT IN BASE MAINTENANCE: WEAR LOWER SKIN IB FIXED LEADING EDGE AT LEVEL RIB 2 ON RH WING L=0.313 INCH W=0.145 INCH, D=0.034 INCH. MAINTENANCE PERFORMED TIME LIMIT REPAIR LOC. ON LOWER SKIN IB FIXED LEADING EDGE AT LEVEL RIB 2 ON RH WING IAW EA 368892.SDR AALA202510218026Rib · wornAIRCRAFT IN BASE MAINTENANCE: WEAR LOWER SKIN IB FIXED LEADING EDGE AT LEVEL RIB 2 ON RH WING. L=0.727 INCH, W=0.442 INCH AND D=0.001 INCH. MAINTENANCE PERFORMED TIME LIMIT REPAIR LOC. ON LOWER SKIN IB FIXED LEADING EDGE AT LEVEL RIB 2 ON RH WING IAW EA 36889SDR AALA202510211013Rib · wornAIRCRAFT IN BASE MAINTENANCE: WEAR LOWER SKIN IB FIXED LEADING EDGE AT LEVEL RIB 2 ON RH WING L=1.514 INCH W=1.173 INCH, D=0.055 INCH. MAINTENANCE PERFORMED TIME LIMIT REPAIR LOC. ON LOWER SKIN IB FIXED LEADING EDGE AT LEVEL RIB 2 ON RH WING IAW EA 368892.SDR UIEA2025071000892Rib · crackedLHW L/E #581HB PANEL RIB FOUND CRACKED.(<P>LHW L/E #581HB PANEL RIB REPLACED AS PER RI-57-51-17762 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2025071000894Rib · crackedLHW L/E #581JB PANEL RIB FOUND CRACKED.(<P>LHW L/E #581JB PANEL RIB REPLACED AS PER RI-57-51-17769 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR DALA2025071105244Rib · corrodedSHIP 3147 FOUND CORROSION AT RIB 9 ASSY. AT FLAP TRACK #2 LEVEL OF THE INBOARD FLAP AT LT WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 622658-14. (1075169).SDR N6WA2025071206Rib · damagedRH RIB AT SLAT STATION 58.41 IS DAMAGED. ACCOMPLISHED REPAIR AND INSTALLED RIB IAW GOJET EO-C550-57MR-011SDR EE4Y20250706226Rib · crackedDURING THE ACCOMPLISHMENT OF SB 190-57-0056, WAS FOUND AT RH WING, LOWER SKIN ASSY – WING BOX, RIB #8, LOWER FLANGE WITH CRACK. DUE TO IT CONDITION WAS REPOARTED TO EMB ASKING FOR REPAIR INSTRUCTIONS. THE CRACKED WAS REPAIRED BY ETD2025-190-923702 AND DOCUMENTSDR IPXA2025071272165Rib · crackedNUMBER 10 SPOILER ACTUATOR SUPPORT HINGE RIB CRACK WS 640. INSTALL NEW FITTING I.A.W SRM 51-40-02-0G REV.92 AND BOEING DWG 112T1000 SH 14 REV: B, 113T1422 SH 1 REV: D, 112T1001 SH 43 REV: -, 113T1653 SH 1 REV: J. I.A.W AMM 27-61-01-424-019 REV 145 STEP 3A TSDR R61A2025072600316Rib · crackedSUSPECTED CRACK LH WING AT RIB 4A. COMPLIED WITH ETD2025-170-924427SDR IPXA2025072138048Rib · crackedMAJOR REPAIR, RH WING, CENTER FLAP, TOP SKIN RIB FLANGE, 2 CRACK INDICATION NOTED AT RIB 25. CIRCLED IN RED. VERIFIED PERMANENT REPAIR ACCOMPLISHED IAW EO-94347-REQ1 AND VT-MAE EA 300-5750-27-A4024, REV. -.SDR IPXA2025072138064Rib · crackedRH WING, CENTER FLAP, TOP SKIN RIB FLANGE, 1 CRACK INDICATION NOTED AT RIB 19. CIRCLED IN RED. VERIFIED REPAIR WAS ACCOMPLISHED IAW E0-94347-REQ1 AND EA 300-5750-27-A4024.SDR IPXA2025072137992Rib · crackedRH WING, CENTER FLAP, TOP SKIN RIB FLANGE, 2 CRACK INDICATION NOTED AT RIB 26. CIRCLED IN RED. VERIFIED REPAIR HAS BEEN ACCOMPLISHED IAW VT-MAE EA 300-5720-27-A4024 REV- AND EO-94347-REQ1.SDR IPXA2025080838089Rib · crackedRIGHT WING, CENTER FLAP, TOP SKIN RIB FLANGE, 1 CRACK INDICATION NOTED AT RIB 13. CIRCLED IN RED. ACCOMPLISH PERMANENT REPAIR IN ACCORDANCE WITH EO-94347-REQ1 AND VT-MAE EA 300-5750-27-A4024, REV. -. REVIEWED.SDR IPXA2025071043323Rib · crackedMAJOR REPAIR, CRACK - RIB, R/H WING T/E CAVITY, UPPER SIDE, WBL 445 (REPAIR) 1. ACCOMPLISHED REPAIR I.A.W EO-93910-REQ1 REV.1 AND EI F2025A57M-1387 REV.1 2.SDR HYIA20250627002Rib · crackedDURING SCHEDULED INSPECTION, A CRACK WAS VISUALLY IDENTIFIED ON THE RIGHT HAND CLOSEOUT RIB LOCATED AT RWS 106.79. THIS CRACK IS LOCATED IN THE FORWARD VERTICAL ROW OF FASTENERS COMMON TO THE AFT TRUNNION SUPPORT. IT TRAVELS IN AN UP AND DOWN DIRECTION BETWEENSDR SWAA2025063082147Rib · crackedRIGHT WING DEFLECTION RIB TO WEB; OB CLIP IS CRACKED<[01] REMOVED AND REPLACED RIGHT WING DEFLECTION RIB TO WEB; OB CLIP IAW SRM 51-40-02<BR>DESC: CLIP<BR>P/N: 115A6260-2;[02] VERIFIED CORRECTIVE ACTION 1SDR FDEA202506150955Rib · damagedLH WING FLE RIB AT OSS 571.049 WAS DAMAGED (P/N 114T2104-19). THE FORWARD FLANGE OF THE RIB WAS CRACKED AND DEFORMED IN MULTIPLE LOCATIONS. THE CRACKED AREAS WERE TRIMMED AWAY. THE WEB WAS FOUND DEFORMED AND COLD WORKED TO REMOVE MOST OF THE DENT DAMAGE. SDR SWIA2025009090611Rib · mechanic errorUPON REMOVAL OF THE RT WING OTBD FLAP, INBD LATERAL SEAL & SHIM FOUND INBD RIB FOUND 2 MISDRILLED HOLES. REPLACED RT OUTBOARD FLAP INBOARD CLOSING RIB IAW SRM 51-42-13-001-001-A01, REO 690-57-53-173 REV-A AND DWG. 601R14501, REV.K. COMPLIED WITH SKYWEST TASSDR CALA2025061605573Rib · crackedLEFT WING T/E FITTING ATTACHMENT OF AILERON OUTERMOST HINGE, UPPER FLANGE IS CRACKED. CRACKED FITTING (SUPPORT RIB) WAS REMOVED AND REPLACED BY NEW SUPPORT RIB P/N: UA-113N1511-19-1, TRAVELER #T25/1812775 IAW SRM 51-40-02 AND DWG: 113N1511 REV B.SDR KCSA202506101093Rib · crackedLEFT WING LEADING EDGE MACHINED RIB CRACKED AT LOWER FORWARD FASTENER HOLE AT APPROX ILES 964.55SDR FDEA202506100874Rib · crackedLEFT WING - FIXED LEADING EDGE RIB DOUBLER AT STATION XOS 789 FOUND CRACK ABOUT 2 INCH. LT WING FIXED LEADING EDGE CRACKED RIB DOUBLER AT STATION XOS 789 REMOVED IAW SRM 51-33-01-0G AND FABRICATED RIB DOUBLER IAW DRAWING ARB3954 REV K. INSTALLED FABRICATEDSDR KCSA202506101092Rib · crackedLEFT WING LEADING EDGE MACHINED RIB CRACKED AT LOWER FORWARD FASTENER HOLE AT APPROX ILES 1014.95SDR VNAA20250714006Rib · crackedCRACK ON MACHINED RIB LEADING EDGE SS58.41 AT LEFT WING. CRACK ON MACHINED RIB LEADING EDGE SS58.41 AT LEFT WING WAS REPAIRED REO 690-57-41-240 REV --SDR CALA2025061705609Rib · corrodedR/W FRONT SPAR FIXED L/E LOWER SUPPORT RIB HAS EXFOLIATED CORROSION AT OFSS 308 LOWER CHORD I/B SLAT # 5 ACTUATOR MKD DOT 032 REF AAR N/R 9976229 ESFR REPORTED AND SENT REMOVED AND INSTALLED NEW SUPPORT RIB AT RT WING FRONT SPAR FIXED L/E I/B OF SS 308 REF B73SDR AALA202506173241Rib · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON INBOARD BOTTOM SIDE OF LEFT HAND WINGLET RIB 0. REPLACED WINGLET PER JOB CARD 08C52057001 AND JOB CARD 08C52057004.SDR IPXA2025060844671Rib · damagedLEFT WING LOWER CHORD ON O/B SIDE OF ANTI ICE DUCT DAMAGED AT FWD L/E AND 4" FWD OF AFT END. VERIFIED THE INSTALLATION OF SLAT CAP IAW MD11 SRM 51-35-01 AND SRM 51-33-01. C/W FIT AND FARE ADJUSTMENT PER AMM 30-11-01-400-802SDR SWIA202509020008Rib · crackedRIGHT INBD GROUND SPOILER INBD FITTING ASSY AT SPS0.00 FOUND TO BE CRACKED AT AFT LOWER FASTENER HOLE LOCATION. FABRICATED NEW RIB. REMOVED OLD AND INSTALLED NEW GROUND SPOILER RIB ASSEMBLY. COMPLIED WITH TASK CARD 51-900-1002-SKY. REF DWG# CC670-16150 REV: SDR SWAA2025060276505Rib · crackedLH WING FIXED LEADING EDGE #4 RIB AT KRAS 166.32 APPROXIMATELY 10' UP FROM LOWER SKIN EDGE; HAS A FASTENER HOLE WITH AN NDT CRACK INDICATION. -MARKED- <[01]. REAMED HOLE TO 0.216 DIAMETER PER SRM 51-40-05.; [02] ACCOMPLISHED A HIGH-FREQUENCY EDDY CURRENT (HFESDR VNAA202508020011Rib · crackedCRACK ON RIB LEADING EDGE SS57.16 AT LH WING. RIB LEADING EDGE SS57.16 AT LH WING WAS REPAIRED PER REO 690-57-41-240 REV -SDR HYIA20250522002Rib · crackedDURING SCHEDULED MAINTENANCE A CRACK WAS VISUALLY IDENTIFIED ON THE RIGHT UPPER OUTBOARD RIB CAP COMMON TO THE CLOSEOUT RIB LOCATED AT RWS 106.79 (OEM: 5122115-12). THIS CRACK WAS IDENTIFIED IN THE RADIUS OF THE CAP TRAVELING FORWARD AND AFT, AND MEASURES APPRSDR SWIA202506290517Rib · crackedRIGHT WING LEADING EDGE RIB AT SS58.41 CRACKED. PERFORMED REPAIR LEADING EDGE RIB SS58.41 AT RT WING IAW REO 670-57-41-624 REV -, 670-57-41-624 REV-P1, SRM 57-21-12, AMM 20-70-00, 30-11-08, NDT PERFORMED IAW SRM 51-21-01, AMM 30-12-00, & 30-11-00.SDR IPXA2025060884755Rib · crackedRH FIXED LE HAS A CRACK AT #3 RIB O/B OF #12 SLAT TRACK. INSTALLED 1EA RIB AT O/B OF #12 SLAT TRACK IN RH WING FIXED L/E COMPARTMENT AT STA XOS=794 REF. MD-11 SRM 51-33-01-0G-0 AND SRM 51-35-01-0G-0.SDR 2025FA0000354Rib · corrodedRH FLAP CLOSE-OUT PANEL RIB AND STRAP CORROSION.SDR DALA2025051203668Rib · misrepaired(LOG 0957915) TRIM OUT PERFORMED INCORRECTLY ON RIB 22 OF RH WING. COMPLIED WITH ER/A 625366-14 REV ORIGINAL.SDR HNAA2025061600439Rib · crackedF044753 POSSIBLE RH WING RIB 21 IS CRACKED UNDER ACCESS PANEL 651CB. PERFORMED CUTOUT OF DAMAGED AREA IAW EMB 145 SRM 57-20-07 RE, ITEM 4. ACCOMPLISHED RH WING RIB 21 REPAIR IAW EMB 145 SRM 57-20-07RE, ITEM 4, FIG 203 AND EO1-57-25-0196.SDR HNAA2025061000413Rib · cracked57-2010 RH LE #2 OB END RIB CRACKED. RAR RIB IAW SRM 51-40-02, ETD2025-145-921063, AND EO1-05-25-0202SDR CALA2025050204414Rib · corrodedLH WING T/E LOWER SURFACE PANEL LANDS AT RIB 23-27 HAVE EVIDENCE OF CORROSION. ACCOMPLISHED REPAIR INSTRUCTIONS PER HAECO REO-L25457 REV IR WIT H NO DEVIATIONS IAW A320 ECRA 5751-01560.SDR VNAA20250602015Rib · crackedCRACK ON RIB LEADING EDGE SS57.16 WAS FOUND CRACK ON RIB LEADING EDGE SS57.16 WAS REPAIRED PER REO 690-57-41-240 REVSDR JJBA20250505013Rib · crackedRH AFT WW RIB FOUND CRACKED. RH AFT WW RIB REMOVED AND REPLACEDSDR JJBA20250505009Rib · crackedLH AFT WW RIB FOUND CRACKED. LH AFT WW RIB REMOVED AND REPLACEDSDR VNAA20250529024Rib · 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 690-57-51-362 REV - -SDR FDEA202504160712Rib · wornRH WING #5 SPOILER O/B JACK RIB UPPER BORE GOT ABRASION ACCOMPLISHED THE REPAIR WITH BUSH, REINFORCING PLATE AND PACKING PLATE AT RH WING #5 SPOILER O/B JACK RIB UPPER BORE ABX184.625 I.A.W EA NO:T6-5740-T0383103 P1, SEQ NO:1060, TITLE:WING-ATTACH FITTINGSSDR JGVR202504007005Bulkhead · corrodedMECHANICALLY REMOVED CORROSION LOCATED IN RH MLG WHEEL WELL AT MIDDLE EMERGENCY BRAKE LINE CARRY THRU ON WS 52.00 INBOARD SIDE, PERFORMED NDT, REPORTED FOR REPAIR DISPOSITION, CLEANED, TREATED, AND, PRIMED PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.SDR JGVR202504007004Bulkhead · corrodedMECHANICALLY REMOVED CORROSION LOCATED IN LH MLG WHEEL WELL AT MIDDLE EMERGENCY BRAKE LINE CARRY THRU ON WS 52.00 INBOARD SIDE, PERFORMED NDT, REPORTED FOR REPAIR DISPOSITION, CLEANED, TREATED, AND, PRIMED PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.SDR SWIA20250418006Rib · damagedL/H WING TIP HAS ELONGATED HOLES INBD AND OUTBD SIDES OF 600-15107-3 RIB AND 600-15116-11 RIB (C-CHECK RO 04/17/2025)REPLACED LH WING TIP RIB P/N: 600-15116-11 REF CRJ-200 SRM 51-42-21, SRM 51-42-15 AND DWG 600-15110 REV. -E FOR FASTENER CALL OUT COMPLIED WISDR SWAA2025042219650Rib · cracked(A204 DOT 4) RH WING TRAILING EDGE CAVITY; 24 INCHES FORWARD OF PANEL TRAILING EDGE. ATTACH ANGLE COMMON TO DEFLECTION CONTROL RIB IS CRACKED AT LOWER OUTBOARD HOLE.<[01] 04 - REPAIRED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL SDR IXXA20250424001Rib · gougedFABRICATE RIGHT WING LEADING EDGE RIB USING ALTERNATE FINISH. HAECO W.O. 320011 AND NR 35297SDR NACA2025031500005Rib · crackedCRACKED RIB, AFT FACE OF L/H WING INBD T/E CAVITY AFT LOWER RIB, WBL 127.SDR SWAA2025033114809Rib · crackedLEFT WING I/B FIXED TRAILING EDGE UPPER PANEL TO DEFLECTION RIB INTERCOSTAL IS CRACKED<[01] DRILLED NEW INTERCOSTAL (ANGLE) PER SRM 51-40-05.;[02] C/W INSPECTION DRILLED NEW INTERCOSTAL (ANGLE) PER SRM 51-40-05.;[03] REMOVED AND REPLACED LEFT WING I/B FIXED TR
Back to JASC 5712