N390AL

Service difficulty reports · 20

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 = 'N390AL' 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 9EKA20161029017Stud · brokenDURING SCHEDULED INSPECTION, FOUND BROKEN STUD FROM FORWARD RIGHT HAND OUTBOARD COMBINING GEARBOX MOUNT.Oct 29, 2016 · N390AL · Bell 214* · Main Rotor GearboxSDR 2017FA0000421Panel · crackedFUSELAGE LOWER PANEL BELOW LEFT FUEL BLADDER HAS A 30 INCHES LONGITUDINAL CRACK.Jul 2, 2016 · N390AL · Bell 214ST · Fuselage Main, Plate/SkinSDR 9EKA20160702009Skin Panel · crackedDURING A POST FLIGHT INSPECTION, FUSELAGE LOWER PANEL, BELOW LT FUEL BLADDER FOUND TO HAVE A 30" LONGITUDINAL CRACK.Jul 2, 2016 · N390AL · Bell 214ST · Fuselage Main, Plate/SkinSDR 9EKA20160512006Ecu · faultyENGINE 1 INDICATED EXCESSIVE TORQUE SPLIT WITH YAW MOTION OF THE ACFT. ENG 1 THROTTLE WAS MANUALLY BROUGHT DOWN TO 10% BELOW NR 2 & SAFELY RETURNED TO BASE.May 12, 2016 · N390AL · Bell 214ST · Fuel Control/Turbine EnginesSDR 9EKA2014122314Elbow · wornOIL COOLER CAUTION PANEL LIGHT CAME ON DURING FLIGHT. ENGAGED SECONDARY OIL COOLER SYS & RETURNED TO BASE IAW EMER PROCEDURES IN ROTOR FLIGHT CRAFT MANUAL.Dec 23, 2014 · N390AL · Bell 214* · Hydraulic System, MainSDR 9EKA20140516004Skin · crackedFOUND CRACK IN SKIN OF RT ELEVATOR. CRACK IS LOCATED AT THE AFT INBD BOTTOM SIDE OF THE ELEVATOR, JUST FWD OF THE RIVETS ATTACHING THE TAB.May 16, 2014 · N390AL · Bell 214ST · Elevator, Plate/SkinSDR 9EKA2013082200002Fitting · crackedCRACK ON THE VERTICAL SPAR OF THE TAIL IT IS LOCATED IN THE COLD WORK AREA JUST ABOVE THE OUTPUT QUILL OF THE 42 DEG GEARBOX. LOCATED ON THE LEFT SIDE AT BS 569.689, WL 95 ON FIN STATION 32. CRACK IS .040 DEEP AND 1.1 INCHES LONG.Aug 21, 2013 · N390AL · Bell 214ST · Rotorcraft Tail BoomSDR ALG2005F00056Line · leakingENROUTE, A HOWLING NOISE STARTED AND BECAME LOUDER, THE PILOT NOTICED NR 1 HYD PRESSURE FLUCTUATED BETWEEN 200-300 PSI. THE PILOT TURNED OFF NR 1 HYD NOISE WENT AWAY. UPON LANDING THE MECHANIC FOUND NR 1 PRESSURE LINE TO THE COLLECTIVE SERVO IS LEAKING. HE Jul 30, 2005 · N390AL · Bell 214ST · Hydraulic System, MainSDR ALGA087947Starter · brokenREPAIR DUE TO THE STARTER WOULD NOT ENGAGE.Jul 4, 2003 · N390AL · Bell 214ST · Engine StarterSDR ALGA087940Amplifier · will not testNR 2 ELEVATOR WILL NOT TEST AND ALSO KICKS OFF.Jun 29, 2003 · N390AL · Bell 214ST · Autopilot SystemSDR ALGA084142Gearbox · wornTAIL ROTOR GEARBOX MOUNT HOLE ELONGATED AND WORN AT CONTACT POINT.Feb 20, 2003 · N390AL · Bell 214ST · Tail Rotor GearboxSDR ALGA084141Gearbox · wornMOUNT HOLE ON GEARBOX ELONGATED AND WORN AT CONTACT POINT.Feb 20, 2003 · N390AL · Bell 214ST · Tail Rotor GearboxSDR ALG2003F00026Sensing Element · inoperativeDURING RUN-UP CHECKS. NR 1 ENGINE FIRE DETECTION SYSTEM WOULD NOT TEST.Feb 13, 2003 · N390AL · Bell 214ST · Fire DetectionSDR ALGA084066Bearing · wornTAIL ROTOR BEARING WORN.Jan 30, 2003 · N390AL · Bell 214ST · Tail Rotor Drive ShaftSDR 98ZZZX3100Blower · failedNR 1 ENGINE PARTICLE SEPARATOR FAILED ON TAKEOFF. FOUND PARTICLE SEPARATOR BLOWER SHAFT SHEARED.Jun 23, 1998 · N390AL · Bell 214ST · Engine Air Intake SystemSDR 96ZZZX2215Longeron · crackedDAILY INSPECTION FOUND CRACK AT UPPER LEFT TAIL BOOM ATTACH POINT, AIRFRAME SIDE. THIS LONGERON BASE IS ONE OF ONLY FOUR ATTACH POINTS. THE UPPER LEFT CARRIES HIGHEST LOADS.Mar 15, 1996 · N390AL · Bell 214ST · Fuselage Main, Longeron/StringerSDR 96ZZZX1833Longeron · crackedUPPER TAILBOOM ATTACHMENT LONGERON CRACKED THROUGH ATTACHMENT FITTING. CRACK WAS DISCOVERED DURING THE DAILY VISUAL INSPECTION. PART WAS TAGGED AND SHIPPED TO BELL HELICOPTER IN FORT WORTH, TEXAS.Mar 15, 1996 · N390AL · Bell 214ST · Rotorcraft Tail BoomSDR 96ZZZX2214Support Angle · crackedPHASE INSPECTION FOUND ANGLE CRACKED ON FORWARD END APPROXIMATELY 2 INCHES FROM END OF ANGLE. THE SUSPECT CAUSE WAS VIBRATION.Mar 13, 1996 · N390AL · Bell 214ST · Rotorcraft Tail BoomSDR 95ZZZX6206Erosion Shield · separatedIN CRUISE FLIGHT OVER THE GULF OF MEXICO, THE AIRCRAFT DEVELOPED A SEVERE VIBRATION. THE PILOT MADE AN IMMEDIATE PRECAUTIONARY LANDING TO AN OFFSHORE DRILLING PLATFORM. EXAMINATION OF THE AIRCRAFT REVEALED THE LOWER EROSION SHIELD ON A MAIN ROTOR BLADE HAD SOct 30, 1995 · N390AL · Bell 214ST · Main Rotor BladesSDR 95ZZZX2091Bearing · fracturedWHILE HANGER ASSY WAS REMOVED TO LUBRICATE FLEX-COUPLINGS. HANGER BEARING FELT ROUGH WHEN ROTATED BY HAND WITH HANGER ASSY REMOVED. OUTER RACE OF BEARING WAS FOUND FRACTURED WHEN REMOVED FROM THE HOUSING. CAUSE UNKNOWN.Mar 29, 1995 · N390AL · Bell 214ST · Tail Rotor Drive Shaft
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