N343AL

Service difficulty reports · 18

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 n_number = 'N343AL' AND registry_match = 'registration'
  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.

SDR ALG2006F00019Line · leakingDURING HOT REFUEL, OIL WAS OBSERVED LEAKING FROM THE AIRCRAFT. REMOVED AND REPLACED ENGINE OIL PRESSSURE LINE WITH SERVICEABLE LINE. (K)Jan 3, 2006 · N343AL · Bell 206L3 · Turbine Engine Oil SystemSDR ALG2005F00049Pump · intermittentIN CRUISE FLIGHT, PILOT NOTICED THAT LT BOOST PUMP IS INTERMITTENT. UPON LANDING THE MECHANIC REMOVED AND REPLACED THE LT FUEL BOOST PUMP AND AC WAS RETURNED TO SERVICE AFTER COMPLETION OF OPERATIONAL CHECKS IAW MM. (K)Jul 17, 2005 · N343AL · Bell 206L3 · Fuel Boost PumpSDR ALGA096731Blade · corrodedTRAILING EDGE EXTRUSION EXFOLIATED, LOWER O/B GRIP FINGER DOUBLER SEPARATED AND CORRODED, ALSO CORROSION BETWEEN SKIN AND SPAR. SCRAPPED BLADE, AND INSTALLED A NEW BLADE.Aug 4, 2004 · N343AL · Bell 206L3 · Main Rotor BladesSDR ALG2003F00064Tube · disconnectedDURING CONTROL FUNCTION CHECK ON RUN-UP TAIL ROTOR PEDALS FELT WEAK, PILOT SHUT THE AIRCRAFT DOWN AND NOTIFIED MAINTENANCE. THE MECHANIC FOUND TAIL ROTOR CONTROL TUBE IN THE BOX BEAM TO THE BELLCRANK IN HAT RACK AREA NOT CONNECTED, THE MECHANIC RECONNECTED THMar 6, 2003 · N343AL · Bell 206L3 · Tail Rotor Control SystemSDR ALG2002F00050Gear · contaminatedUPON DISASSEMBLY AND INSPECTION OF PARTS DUE TO METAL CONTAMINATION. PINION GEAR HAS EXCESSIVE GALLING ON GEAR TEETH DUE TO IMPROPER MACHINING AND MESHING WITH T/M GEAR. BOTH PARTS WERE SCRAPPED AND SENT FOR WARRANTY CREDIT. ASSURE PROPER MACHINING AND MESHFeb 3, 2002 · N343AL · Bell 206L3 · Main Rotor GearboxSDR 2001F00602Turbine Blades · corrodedDURING DISASSEMBLY TO REPAIR FOR LOW POWER. SULPHADATION ON FRONT SIDES OF BLADES. HAVE WHEELS TESTED FOR PROPER COATING. (M)Aug 15, 2001 · N343AL · Bell 206L3 · Turbine SectionSDR 2001F00577Blade · corrodedDURING DISASSEMBLY TO REPAIR FOR LOW POWER, SULPHIDATION ON FRONT SIDES OF BLADES. (M)Aug 15, 2001 · N343AL · Bell 206L3 · Turbine SectionSDR 99ZZZX3027Blade · corrodedDURING DAILY INSPECTION, CORROSION AND DEBOND OF SKIN AND SPAR BENEATH GRIP FINGER DOUBLER ON LOWER SURFACE. DAMAGE BEYOND MANUFACTURER'S LIMITS, BLADE SCRAPPED.Jun 29, 1999 · N343AL · Bell 206L3 · Main Rotor BladesSDR 99ZZZX1230Bearing · looseDURING INSPECTION, FOUND BEARING WITH EXCESSIVE PLAY.Mar 8, 1999 · N343AL · Bell 206L3 · Engine Mount SectionSDR 99ZZZX1229Line · leakingDURING FLIGHT, THE HYDRAULIC SYSTEM LOST PRESSURE. PRESSURE LINE FROM PUMP WAS FOUND LEAKING.Mar 6, 1999 · N343AL · Bell 206L3 · Hydraulic System, MainSDR 97ZZZX245Blade · corrodedDURING DAILY INSPECTION FOUND BLADE SKIN CORRODED AND SEPARATED FROM SPAR AT BLADE TIP.Aug 28, 1996 · N343AL · Bell 206L3 · Main Rotor BladesSDR 96ZZZX3460Nut · lost torqueWHEN REMOVING SWASHPLATE, MECHANIC FOUND NUT TO HAVE LOST TORQUE. (HAND TIGHT.) HAVE FOUND SEVERAL MAST NUTS ON 206L-3'S AND 206L-4'S MAST ASSEMBLIES THAT HAVE LOST TORQUE. BELIEVE THE CONTACT AREA BETWEEN THE MAST NUT AND THE BEARING INNER RACE IS TOO SMALMay 7, 1996 · N343AL · Bell 206L3 · Main Rotor Mast/SwashplateSDR 96ZZZX295Link Idler · wornDURING DAILY INSPECTION, FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2 EACH 206-010-338-003 BUSHINGS, 2 EACH NAS6605D64 BOLTS, 1 EACH 206-010-470-101 BEARING. Dec 13, 1995 · N343AL · Bell 206L3 · Main Rotor Mast/SwashplateSDR 96ZZZX294Lever Assy · wornDURING DAILY INSPECTION, FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2 EACH 206-010-338-003 BUSHINGS, 2 EACH NAS6605D64 BOLTS, 1 EACH 206-010-470-101 BEARING. Dec 13, 1995 · N343AL · Bell 206L3 · Main Rotor Mast/SwashplateSDR 95ZZZX3355Link Idler · wornDAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2 EACH 206-010-338-003 BUSHINGS, 2 EACH NAS 6605D64 BOLTS, AND 1 EACH 206-010-470-101 BEARING. NORJun 15, 1995 · N343AL · Bell 206L3 · Main Rotor Mast/SwashplateSDR 95ZZZX3354Lever Assy · wornDAILY INSPECTION FOUND BUSHINGS AND BEARINGS WORN BEYOND LIMITS. PARTS REQUIRING REPLACEMENT: 4 EACH 206-010-338-001 SPACERS, 4 EACH 206-010-337-001 BEARINGS, 2 EACH 206-010-338-003 BUSHINGS, 2 EACH NAS 6605D64 BOLTS, AND 1 EACH 206-010-470-101 BEARING. NORJun 15, 1995 · N343AL · Bell 206L3 · Main Rotor Mast/SwashplateSDR 95ZZZX2784Compressor · contaminatedDURING A COMPRESSOR CHANGE FOUND WHILE POSITIONING THE COMPRESSOR ON A WORK BENCH, A SMALL WHITE HARD BEAD ROLLED OUT OF THE SCROLL DISCHARGE TUBE. THE COMPRESSOR SCROLL WAS BORESCOPED TO CHECK FOR ANY MORE BEADS WHICH MAY HAVE BEEN LODGED IN THE SCROLL. NO May 22, 1995 · N343AL · Bell 206L3 · Turbine Engine Compressor SectionSDR 95ZZZX2785Gearshaft · pittedUPON DISASSEMBLY AND INSPECTION, FOUND AIR OIL GEARSHAFT PITTED.May 2, 1995 · N343AL · Bell 206L3 · Turbine Engine Accessory Drive
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