N438LX, cancelled Mar 14, 2024

Service difficulty reports · 17

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 = 'N438LX' AND deregistration_id = 'N438LX-2024-03-14'
  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 DJFA20130912001Transducer · unsecureDURING LANDING, CREW REPORTED STIFF BRAKES FOLLOWED BY INTERMITTENT ANTI-SKID OPERATION. MX FOUND THE WHEEL SPEED TRANSDUCER NOT ENGAGED WITH THE WHEEL HUB CAP ASSY. MX CORRECTED THE CONDITION.Sep 12, 2013 · N438LX · Beech 400A · Brake Anti-Skid SectionSDR DJFA20130910002Duct · contaminatedPASSENGER REPORTED BURNING ODOR IN THE CABIN DURING FLIGHT. AFTER LANDING, CREW NOTED LOWER FORWARD RT SIDE WALL AND FOLDING TABLE WERE HOT TO THE TOUCH. MX FOUND HEATER DUCT TO BE CONTAMINATED WITH CARBONATED DRINK FROM PASSENGER SPILL. THE DUCT WAS CLEANESep 10, 2013 · N438LX · Beech 400A · Air Distribution SystemSDR DJFA20130908001Transducer · failedDURING LANDING, CREW REPORTED ANTI-SKID OPERATION SLUGGISH RESULTING IN DECREASED BREAKING EFFECTIVENESS. MX INSPECTED THE SYS AND FOUND THE RT WHEEL SPEED TRANSDUCER OUT OF LIMITS. THE TRANSDUCER WAS REPLACED.Sep 8, 2013 · N438LX · Beech 400A · Brake Anti-Skid SectionSDR DJFA20120929001Brake Sys · pressure lossCREW REPORTED LEFT SIDE, RIGHT BRAKE PEDAL INTERMITTENTLY COLLAPSES TO TRAVEL LIMIT WITH LITTLE OR GRABBY BRAKING ACTION. AFTER PUMPING PEDAL NORMAL BRAKE OPS RETURN, THOUGH PEDAL STILL FEELS SOFT AND DOESN’T MATCH LT PEDAL. THE RT SIDE BRAKES OPERATES NORMALSep 29, 2012 · N438LX · Beech 400A · Landing Gear Brake SystemSDR DJFA20120815006Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STAB ASSY, RIB FOUND CRACKED ON THE LOWER FLANGE AT RT HORIZTONAL CANTED STATION 46.06, BETWEEN THE FWD AND AFT SPARS. CRACK EMANATE FROM THE FASTENER HOLE. RIBS REPLACED.Aug 15, 2012 · N438LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA20120815005Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STAB ASSY, RIB FOUND CRACKED ON THE LOWER FLANGE AT RT HORIZTONAL CANTED STA 46.06, BETWEEN THE FWD AND AFT SPARS. CRACKS EMANATE FROM THE FASTENER HOLES. RIB REPLACED.Aug 15, 2012 · N438LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA20120815004Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STAB, RIB FOUND CRACKED ON THE LOWER FLANGE AT RT HORIZONTAL CANTED STATION 29.92, BETWEEN THE FWD AND AFT SPARS. CRACK EMANATES FROM THE FASTENER HOLES. RIB REPLACED.Aug 15, 2012 · N438LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA20120815003Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STAB, RIB FOUND CRACKED ON THE LOWER FLANGE AT RT HORIZONTAL CANTED STATION 13.78, BETWEEN THE FWD AND AFT SPARS. CRACK EMANATES FROM THE FASTENER HOLES. RIB REPLACED.Aug 15, 2012 · N438LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA20120815002Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STAB, RIB WAS FOUND CRACKED ON THE LOWER FLANGE AT LT HORIZONTAL CANTED STATION 46.06, BETWEEN THE FWD AND AFT SPARS. CRACK EMANATE FROM THE FASTENER HOLES. RIB REPLACED.Aug 15, 2012 · N438LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA20120815001Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER, THE RIB DESCRIBED BELOW WAS FOUND CRACKED (ALONG WITH 5 OTHER RIBS; EACH RIB FAILURE IS DOCUMENTED ON SEPARATE SDR FORMS) ON THE LOWER FLANGE AT LT HORIZTONAL CANTED STATION 13.78, BAug 15, 2012 · N438LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA20120130008Unknown · odorON APPROACH FOR LANDING, CREW REPORTED AN ELECTRICAL BURNING ODOR COMING FROM THE PILOT'S SIDE GLARESHIELD. ACFT LANDED SAFELY. NO SMOKE WAS NOTED. MAINTENANCE PERFORMED VISUAL INSPECTION BUT COULD NOT FIND THE SOURCE OF SMOKE OR FUMES; ENGINE RUNS AND OTJan 30, 2012 · N438LX · Beech 400A · Air Distribution SystemSDR DJFA2011016Torque Tube · twistedDURING A C-CHECK INSPECTION, MAINTENANCE TECHNICIANS FOUND THE LT AND RT ELEVATORS WOULD NOT LINE UP IN THE NEUTRAL POSITION. UPON FURTHER INVESTIGATION, IT WAS DETERMINED THAT BOTH THE LEFT AND RIGHT TORQUE TUBES WERE TWISTED SUCH THAT ALIGNMENT OF THE ELEVAApr 20, 2011 · N438LX · Beech 400A · Elevator StructureSDR DJFA201002Duct · failedDURING FLIGHT, CREW NOTED BLEED AIR DUCT FAILURE WARNING. ACFT PERFORMED AN UNSCHEDULED LANDING. DETERMINED A BLEED AIR DUCT FAILED. ACFT SCHEDULED TO FERRY TO A MX STATION. AFTER TAKE-OFF FOR FERRY FLT, CREW DETECTED AN OIL ODOR WHEN THROTTLES ADVANCED & Jan 3, 2010 · N438LX · Beech 400A · Engine Bleed Air SystemSDR DJFA2008028Inlet · crackedDURING A SCHEDULED INSPECTION, MAINT DISCOVERED THE NR 2 ENGINE HEATED INLET CRACKED. MAINTENANCE REPLACED THE INLET.Mar 18, 2008 · N438LX · Beech 400A · Air Intake Anti/De-Ice SystemSDR DJFA2007086Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, BOTH THE RT AND LT IB ROLLER BRACKETS WERE FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREAAug 2, 2007 · N438LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA2006235Switch · out of adjustTRIP ID NR 1010703, FOLLOWING SELECTION OF FLAPS FROM (0) DEGREES TO (10) DEGREES WHILE ON APPROACH, THE CREW RECEIVED A FLAP ASYMMETRY LIGHT AND FLAPS REMAINED AT (0) DEGREES. CREW AGREED TO HAVE CFR TRUCKS ROLLED WHEN THE AC LANDED. BEFORE FLAP HANDLE WAS Apr 25, 2006 · N438LX · Beech 400A · Trailing Flap Position Indicating SystemSDR E812005F00000Computer · malfunctionedTROUBLESHOT PILOT REPORT OF TAWS SYSTEM AND RADAR INOPERATIVE. FOUND TAWS8000 SYSTEM LOCKED UP. NO RESPONSE WHEN COMPUTER CONNECTED FOR TROUBLESHOOTING. REPLACED TAWS8000 UNIT WITH REPAIRED UNIT, SYSTEM OPERATIONS NORMAL. FOUND RADAR INOPERATIVE DUE TO REMApr 26, 2005 · N438LX · Beech 400A · Ground Proximity System
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