JASC 5410
Service difficulty reports · 4,119
Reports filed under 5410 · Nacelle/Pylon, Main Frame, 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 = '5410' 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 = '5410' 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 98ZZZX2868Keel · damagedAT SCHEDULED INSPECTION, DETERMINED THE LEFT NACELLE INBOARD KEEL ASSEMBLY TO FAIL CONDUCTIVITY TEST PER RAYTHEON SERVICE BULLETIN 54-3071 PART II. VISUAL INSPECTIONS PROVED SATISFACTORY PER PART I OF SAME BULLETIN. SCHEDULED REPETITIVE VISUAL INSPECTIONS UNSDR 99ZZZX1134Frame · crackedDURING ROUTINE MAINTENANCE CHECKS, CRACKS WERE FOUND ON BOTH ENGINE NACELLE NR 1 FRAMES. ON THE LT FRAME, THE CRACK IS LOCATED ON THE LOWER SIDE OF THE STIFFENING WEB, BETWEEN THE TOP OUTBOARD MOUNTING BOLT HOLE AND THE OUTBOARD EDGE OF THE FRAME. ON THE RT SDR 99ZZZX1133Frame · crackedRECOMMEND REPLACING BOTH FRAMES, AND CONTINUE MOINITORING IAW EXISTING MAINTENANCE CHECKS.SDR CA980330018Intake · cracked(CAN) DURING DAILY INSPECTION, IT WAS FOUND THAT THE RAM AIR RECOVERY VANE P/N 81-3103-109 WAS LOOSE AND THE NACELLE AREA WHICH SUPPORTS THE VANE WAS CRACKED. NACELLE CRACKS WERE REPAIRED PER STANDARD REPAIR PRACTICES AND NEW VANE INSTALLED.SDR CA971210018Collar · loose(CAN) ON INSP A NO OF FAILED COMPONENTS WERE FOUND IN BOTH WHEEL WELL AREAS.COLLAR P/N27-35012-001 WAS FOUND LOOSE & MOVED WITH FORE & AFT PRESSURE ON LOWER GEAR LEG.P/N27-35011-007(DOUBLER).DUE TO MOVEMENT OF- ABOVE FITTING,FASTENERS THAT ATTACH FITTING TO BASDR AU971450Web · cracked(AUS) NACELLE LH AND RH WEBS CRACKED. FOUND DURING INSPECTION IAW SB200.SDR AU971449Angle · cracked(AUS) LH NACELLE BOX ANGLE LOCATED FORWARD OF PNO NB-20-C-5677 CRACKED.SDR CA971128004Collar · loose(CAN) ON INSP A NO OF FAILED COMPONENTS WERE FOUND IN BOTH WHEEL WELL AREAS.COLLAR P/N27-35012-001 WAS FOUND LOOSE & MOVED WITH FORE & AFT PRESSURE ON LOWER GEAR LEG.P/N27-35011-007(DOUBLER).DUE TO MOVEMENT OF- ABOVE FITTING,FASTENERS THAT ATTACH FITTING TO BASDR AU970474Angle · loose(AUS) RH ENGINE NACELLE LOWER ANGLE SHEAR PLATE LOCATED AT WS65.69 ANDWS89.31 HAD LOOSE AND WORKING RIVETS ALLOWING FORE AND AFT MOVEMENT OF THE LOWER ENGINE MOUNT ATTACHMENT BRACKETSSDR AWXA9700043Structure · crackedNR 2 ENGINE CANTILEVER STRUCTURE FROM RIB 01-07 OUTBOARD SPAR CRACKED. COMPLIED WITH AWA E.R. NR 32-54-20-15. TRANSFERRED TO AWM 106 NR 970009 FOR WEEKLY INSPECTION UNTIL PERMANENT REPAIR. S.IA. NR 54-002-97 ISSUED BY ENGINEERING ON 1-10-97. REQUIRES INSPESDR CA961231004Beam Assembly · cracked(CAN) NR1 FORWARD ENGINE BEAM CRACKS FOUND ON BOTH THE LEFT AND RIGHT ENGINE BEAM INBOARD AND OUTBOARD. CRACKS LOCATED DIRECTLY UNDER THE MOUNT AND/OR ORIGINATING FROM END OF THE BEAM AND IN A CIRCULAR SHAPEOF ANCHOR NUT FORWARD END. CRACKS EXTENDING THROUGH TSDR 96ZZZX5861Firewall · crackedFIREWALL CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR 96ZZZX4295Frame · corrodedWHILE COMPLETING 100-HOUR FACTORY INSPECTION, NOTED CORROSION BUILD-UP AFT OF EXHAUST ON TOP OF RT NACELLE. REMOVED CORROSION AND FOUND 1 INCH HOLE. BOTH SKIN AND FRAME HAD BEEN EATEN THROUGH. REPLACED FRAME WITH NEW AND C/W RIVETED PATCH REPAIR ON NACELLE SDR AU960210Pin · cracked(AUS) LH ENGINE PYLON MID SPAR FITTING FUSE PIN CRACKED ON INNER BORE APPROXIMATELY 23MM (0.90IN) IN FROM THE HEAD OF THE PIN - CRACK LENGTH APPROXIMATELY 12MM (0.47IN) - FOUND DURING EDDY CURRENT INSPECTION IAW B76-54-40-4D - CRACK CONFIRMED BY MAGNETICPARTISDR F6LM9594Firewall · crackedCRACKED AT THE UPPER SUPPORT CORNERS. THIS FIREWALL WAS INSTALLED FOR 93 HOURS REPLACED THE FIRE WALL. ON INSTALLATION WE HAD TO SHIM THE LEGS TO GET A STRESS FREE INSTALLATION, USED MGB UPPER COWLS TO POSITION FIREWALL PRIOR TO FINAL TIGHTENING AJUSTED ENGINSDR UPS402747Rib · crackedWHILE IN AMSTERDAM FOR 'C' CHECK MAINTENANCE FOUND NR 4 PYLON RIB CRACKED AT NAC STA 163 O/B SIDE. REPLACED RIB PER SRM 51-30-2.SDR C2XA95IA035Mount · chafedIAH - DURING C-CHECK INSPECTION, THE LEFT NACELLE INBOARD TRUSS MOUNT MIDDLE TUBE WAS FOUND TO BE CHAFED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE AFFECTED MOUNT, AND THE AIRCRAFT WAS RETURNED TO SERVICE. REF ATR MM 54-21-61-DVI. (Z)SDR 95ZZZX606Doubler · corrodedDURING INSPECTION, UPPER SKIN DOUBLER FOR THE RIGHT ENGINE PYLON WAS FOUND HEAVILY CORRODED. THIS PART IS MADE OF 4130 STEEL AND IS SUSCEPTIBLE TO RUST. REMOVED TOP SKIN AND REPLACED DOUBLER.SDR DL72L950096Angle · wornDURING HMV, NR 2 PYLON COWLING SUPPORT ANGLE WORN AT 6 O'CLOCK POSITION. REPAIRED PER M/M 53-11-0.
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