Honeywell LTS101-750C-1

Service difficulty reports · 68

Newest first. General aviation reporting is voluntary.

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 engine_model_key = 'LTS101750C1'
  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 CA190426021Engine · power loss(CAN) REPORTED TO HAVE A POWER LOSS SHORTLY AFTER TAKEOFF AND CRASHED INTO RESIDENTIAL BUILDINGS AIRCRAFT CAME TO REST ON THE LEFT SIDE. EXTENT OF INJURIES NOT REPORTED BUT NO FATALITIES INVOLVED. (TC# 20190426021)Apr 26, 2019 · Bell 222U · Engine (Turbine/Turboprop)SDR QMLA2014090514107Engine · leakingRETURNING TO BASE AT THE COMPLETION OF A SCENE FLIGHT, THE ECS UNIT WAS TURNED ON. AFTER A FEW MINUTES THE MEDIC, IN THE CABIN, STATED THAT THERE WAS A FOG IN THE CABIN & A STRONG SMELL OF JET FUEL. THE PILOT BACKED UP BY THE NURSE HOLDING THE RFM RAN THE SMSep 5, 2014 · N222MN · Bell 222U · Engine (Turbine/Turboprop)SDR CA130314004Case · cracked(CAN) TOP CASE RT INBD COLLECTIVE IDLER LUG FOUND CRACKED. BUSHING WORN BEYOND LIMIT. CASE REPLACED.Mar 13, 2013 · Bell 222B · Main Rotor GearboxSDR QMLA2012092512159Longeron · crackedDURING INSPECTION OF TAIL ROTOR ACTUATOR AND SURROUNDING AREA FOUND CRACK ON LONGERON ABOVE AND TO THE LT OF THE ACTUATOR.Sep 25, 2012 · N419MA · Bell 222UT · Rotorcraft Tail BoomSDR QMLA2012032912038Actuator · inoperativeON A ROUTINE ENGINE OVERSPEED SYS CHECK, WANTED TO INCREASE THE ENGINE RPM SLIGHTLY WITH THE TRIM SWITCH. FOUND UNABLE TO GET THE SWITCH TO DO ANYTHING. ON INSPECTION, MECHANIC FOUND THAT THE LINEAR ACTUATOR WAS INOPERATIVE AND SUBSEQUENTLY REPLACED THAT PARMar 29, 2012 · N222AM · Bell 222U · Power LeverSDR QMLA2012032512036Unknown · smokeDURING RUN-UP, BOTH ENGINES STARTED & GENERATORS PLACED IN "ON" POSITION FOLLOWING NORMAL START. WHILE PILOT WAS PLACING SYS & SWITCHES TO THE CHECKLIST, PARAMEDIC IN LT SEAT ALERTED HIM TO SMOKE. LOOKED FOR SIGNS OF SMOKE, VERIFIED NO FIRE WARNING LIGHTS, & Mar 25, 2012 · N117MK · Bolkms BK117B2 · Engine (Turbine/Turboprop)SDR CA111130011Arm · damaged(CAN) UPON INSPECTION OF THE ARM ASSY, IT WAS FOUND THAT THE INNER SURFACE AT THE AREA SURROUNDING THE FLOATING BUSHING HAD SEVERE MECHANICAL DAMAGE. DAMAGE WAS FOUND TO 50 PERCENT OF THE CIRCUMFERENCE OF THE AFFECTED AREA.Nov 30, 2011 · Bell 222U · Main Rotor HeadSDR QMLA2011092111094Engine · making metalNR 2 ENG CHIP LIGHT ILLUMINATED, FOUND MINOR DEBRIS ON GEARBOX CHIP DETECTOR AT 13137 ACFT TT. CLEANED DETECTOR IAW LTS 101 2.2MM CHAP 72-00-00, RETURNED ACFT TO SERVICE. NR 2 ENG CHIP LIGHT ILLUMINATED 2ND TIME INTERMITTENTLY WITH TURBINE CHIP LIGHT ALSO ILLSep 21, 2011 · N419MA · Bell 222UT · Engine (Turbine/Turboprop)SDR QMLA2011061511065Gearbox · making metalAFTER ZONE INSPECTION ON NR1 ENGINE, ACFT WAS BEING GROUND RUN FOR LEAK CHECKS. ON START UP, THE ENGINE G/B CHIP LIGHT IMMEDIATELY CAME ON, PILOT SHUTDOWN STRAIGHT AWAY. MECHANIC PULLED THE CHIP PLUG AND FOUND NUMEROUS CHIPS ON THE PLUG. THIS WAS THE SECOND Jun 15, 2011 · N220LN · Bell 222U · Turbine Engine Reduction GearSDR QMLA2010102510071Disc · unserviceableDURING LIFT OFF, ROTORBRAKE WARNING LIGHTS ILLUMINATED, FOLLOWED BY TRANSMISSION CHIP LIGHTS AND TRANSMISSION OIL PRESSURE. CREW REPORTED SMELLING SOMETHING BURNING. PILOT IMMEDIATELY LANDED ACFT AND SHUTDOWN. INSPECTED ROTORBRAKE AREA AND FOUND ROTORBRAKE DISOct 25, 2010 · N220LN · Bell 222UT · Main Rotor BrakeSDR 2010F00057Gear · failedSPIRAL BEVEL COLLECTOR GEAR FAIL APART, (DRIVE TOOTH/GEAR BOKE AWAY/SEPARATED FROM THE BEVEL GEAR BODY) WITH IN THE MAIN ROTOR GEARBOX/TRANSMISSION.Mar 10, 2010 · N222AM · Bell 222UT · Main Rotor GearboxSDR CA081222008Servo · unknown(CAN) SOLID RESISTANCE FELT WITH AFT CYCLIC MOVEMENT DURING OPERATIONS WITH FORCE TRIM ON & UTILIZING CYCLIC TRIM RELEASE SWITCH. ON FIRST OCCURRENCE RESISTANCE RELEASED WITH A FIRM BUMP & FAULTY LT CYCLIC TRIM RELEASE SWITCH SUSPECTED HOWEVER WITH SECOND OCCDec 8, 2008 · Bell 222U · Rotorcraft Servo SystemSDR CA090127010Bracket · crackedHIGH PRESSURE ENGINE FUEL FILTER BRACKET CRACKING AT TOP BOLT HOLE DUE TO HARMONIC VIBRATION, KNOWN PROBLEM.Nov 26, 2008 · Snias AS350B2 · Engine Fuel DistributionSDR 200709152121Feeder Cable · shortedCABLE SHORTED, CAUSING FALSE FIRE WARNING INDICATION.Sep 15, 2007 · N911MK · Bell 222UT · Fire Protection System WiringSDR BAQA200700022Blade · looseWHILE COMPLETING A GROUND RUN FOR MAINTENANCE, A VIBRATION WAS FELT, AIRCRAFT WAS SHUTDOWN, AND FOUND THE IB FEATHERING BEARING ON THE TAIL ROTOR BLADE LOOSE IN THE BORE. NEW STYLE BEARINGS 222-312-761-101 INSTALLED IAW TB 222U-06-99 AT TIME SINCE REPAIRED.Jun 27, 2007 · N587MG · Bell 222U · Tail Rotor BladesSDR BAQA200700020Blade · looseWHILE COMPLETING A DAILY INSPECTION, FOUND THE IB FEATHERING BEARING ON THE TAIL ROTOR BLADE LOOSE IN THE BORE. NEW STYLE BEARINGS 222-312-761-101 INSTALLED IAW TB 222U-06-99 AT TIME SINCE REPAIRED.Jun 25, 2007 · N222LF · Bell 222UT · Tail Rotor BladesSDR BAQA200700021Blade · looseWHILE COMPLETING A DAILY INSPECTION, FOUND THE OB FEATHERING BEARING ON THE TAIL ROTOR BLADE LOOSE IN THE BORE. NEW STYLE BEARINGS 222-312-761-101 INSTALLED IAW TB 222U-06-99 AT TIME SINCE REPAIR.Jun 25, 2007 · N222LF · Bell 222UT · Tail Rotor BladesSDR 47540060306Tube · crackedONE OF THE AIR LINES THAT RUNS FROM THE FUEL CONTROL TO THE OVERSPEED SOLENOID CRACKED AT A FLARE, CAUSING ENGINE TO DECEL.Jun 3, 2006 · N402MA · Bell 222U · Fuel Controlling SystemSDR HEEA107416Transmitter · failedNR 1 ENGINE OIL PRESSURE GAUGE PEGGED OUT ON THE HIGH SIDE. MAINTENANCE REPLACED THE ENGINE OIL PRESSURE TRANSMITTER.Dec 17, 2005 · N6992 · Bell 222U · Engine Oil PressureSDR 47518022205Flexure · delaminatedSHORTLY AFTER TAKEOFF WHILE ACCELERATING THROUGH 40-50 KTS A MODERATE 1/1 WAS NOTED. IT CONTINUED TO WORSEN WITH AIR SPEED. I TURNED AROUND AT ABOUT 100 KTS. LOWERED COLLECTIVE, AND RETURNED TO BASE. THE SEVERITY OF THE VIBRATION LESSENED WITH LOWER COLLECTIVEFeb 22, 2005 · N419MA · Bell 222UT · Main Rotor Transmission MountSDR 47518011705Line · rupturedTHE NR 1 HYD SYSTEM CAUTION LIGHT CAME ON. PRESSURE CHECKED AND WAS CONFIRMED TO BE AT ZERO. CYCLED SWITCH, MOVED PEDALS AND VERIFIED ACTUAL FAILURE, SO TURNED HYD SYSTEM #1 OFF, PROCEEDED TO FULLERTON AIRPORT AND MADE LANDING FROM A HOVER TO HELIPAD, NO PROBLJan 17, 2005 · N419MA · Bell 222UT · Hydraulic System, MainSDR 047504123104Servo · malfunctionedNR 1 HYDRAULIC SYSTEM LOST PRESSURE. THE AIRCRAFT WAS LANDED IN A OPEN FIELD AT VALLEY HOSPITAL WITH OUT INCIDENT. PATIENT WAS TRANSPORTED VIA AMBULANCE ACROSS THE STREET TO UMC. RT DUAL ACTUATOR SERVO LEAKING AT PISTON. REMOVED AND REPLACED SERVO.Dec 31, 2004 · N431MA · Bell 222U · Hydraulic System, MainSDR 47504123104Servo · failedSCENE FLIGHT FROM BASE 7 LAS VEGAS, NV TO JEAN, NV TO UNIVERSITY MEDICAL CENTER (UMC), LAS VEGAS, NV. APPROXIMATELY 1 MILE SOUTH OF UMC, NR 1 HYDRAULIC SYSTEM LOST PRESSURE. THE AIRCRAFT WAS LANDED IN A OPEN FIELD AT VALLEY HOSPITAL WITH OUT INCIDENT. PATIENDec 31, 2004 · N431MA · Bell 222U · Hydraulic Power SystemSDR 47567122504Link · failedWHILE IN CRUISE FLIGHT WITH PATIENT ABOARD. TWO LOAD BANGS WERE HEARD. A PRECAUTIONARY LANDING WAS MADE AT DCU. LANDED AIRCRAFT AND INSPECTED DOORS. NOTHING WAS FOUND. RESUMED THE FLIGHT AND APPROXIMATELY 2 MIN LATER A LOUD BANG BEGAN ACCOMPANIED BY VIBRATION Dec 25, 2004 · N220LN · Bell 222U · Main Rotor Transmission MountSDR CA041007009Skin · cracked(CAN) CARRYING OUT A DAILY CHECK IT WAS OBSERVED THAT A VERTICAL LATERAL CRACK HAD DEVELOPED ON THE LOWER SKIN OF TAILBOOM JUST 5 INCHES AFT OF THE HORIZONTAL STABILIZER. THE SKIN IS 2024 T3 .032 IN.Sep 29, 2004 · Bell 222U · Rotorcraft Tail BoomSDR N406MA0204Wire · chafedDURING FLIGHT TAIL ROTOR CAUTION LIGHT ILLUMINATED. RETURNED TO BASE. FOUND POWER WIRE TO CHIP DETECTOR WAS FOUND TO HAVE CHAFED THROUGH AND SHORTED. REPAIRED WIRE.Feb 27, 2004 · N406MA · Bell 222B · Turbine Engine System WiringSDR N406MADetector · brokenWHILE ENROUTE TO A SCENE CALL, CLIMBING THROUGH 3800 FT EAST OF ROMNA, CA. I NOTICED NR 2 ENGINE OIL TEMP PEGGED ABOVE MAX. TEMP HAD BEEN NORMAL ON LAUNCH AND THROUGH THE FIRST 10 MIN. OF FLIGHT. ABORTED MISSION AND RETURNED TO BASE. DUE TO TERRAIN AND ABSENCEFeb 18, 2004 · N406MA · Bell 222B · Engine Oil TemperatureSDR N431MAMount · debondedENROUTE TO THE HOSPITAL FOR PATIENT PICKUP. STRONG 2 PER REV VIBRATION EXPERIENCED. LANDED AT PSP AIRPORT. CONTACTED MAINTENANCE FOR REPAIRS. AFTER TROUBLESHOOTING FOUND LATERAL ISOLATION MOUNT DE-BONDED. REMOVED AND INSTALLED SERVICEABLE UNIT.Feb 10, 2004 · N431MA · Bell 222U · Main Rotor Transmission MountSDR BAQA087531Pump · failedFUEL PUMP DOESN'T TURN FREELY. REPLACED WITH SERVICEABLE UNIT.Jun 8, 2003 · N219HM · Bell 222U · Engine Fuel PumpSDR BAQA087055Pump · failedFUEL PUMP WOULD NOT TURN. REPLACED WITH SERVICEABLE UNIT.Jun 8, 2003 · N219HM · Bell 222U · Engine Fuel PumpSDR BAQA085865Manifold · crackedCRACKED AND LEAKING FUEL AT 10 DEGREE CLOCK NOZZLE. HARD CARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT.Mar 31, 2003 · N911WJ · Bolkms BK117A4 · Engine Fuel DistributionSDR CA030228004Fitting · cracked(CAN) UPON A THREE HUNDRED HOUR INSPECTION 270 BULKHEAD FITTING 222-031-506-103A WAS FOUND CRACKED. TO REPAIR INCORPORATION OF TB 222U-94-72.Feb 21, 2003 · Bell 222U · Fuselage Main, BulkheadSDR HEEA083048Valve · stuckFUEL CONTROL VALVE IS STUCK IN THE NORMAL MODE.Jan 7, 2003 · N6992 · Bell 222U · Fuel Control/Turbine EnginesSDR CA021001001Bracket · cracked(CAN) RIGHT, LOWER DOOR SUPPORT HINGE FOUND CRACKED AFTER A FLIGHT. IT WAS DISCOVERED THAT A BELL 206 HAD LANDED AT THE BASE SEVERAL DAYS PRIOR, THIS SAME DOOR HAD FLOWN OPEN. CHECKED AFTER INCIDENT BY THE PILOTS BUT NO DAMAGE NOTED. MAY HAVE BEEN THE ULTIMATEJul 11, 2002 · Bell 222U · Passenger/Crew DoorsSDR CA020521004Fitting · worn(CAN) ENROUTE TO VICTORIA AIRPORT STRONG SMELL OF JET FUEL NOTICED. THEY WERE JUST IN ZONE WITH TOWER. PILOT DECLARED EMERGENCY WITH AIRPORT. A/C LANDED WITH NO INCIDENT AND AIR TAXI BACK TO HANGAR. INVESTIGATION OF ODOUR FUEL CONTROL TO START FUEL LINE FITTApr 11, 2002 · Bell 222U · Engine Fuel DistributionSDR CA020228013Sleeve · worn(CAN) WHEN SWASH PLATE ASSY WAS REMOVED TO FACILITATE 7 YEAR MAST REMOVAL FOR INSPECTION AND RECALIBRATION, THE SLIDER BEARINGS (2OF) P/N 222-310-464-003 WERE FOUND DETACHED AND LOOSE, CREATING AN EXCESSIVE WEAR ON THE SLEEVE JOURNALS THAT HOUSE THESE BEARINGSFeb 1, 2002 · Bell 222B · Main Rotor HeadSDR CA020131002Fitting · broken(CAN) VERTICAL LOWER FIN FITTING FOUND ATTACHMENT LUG BROKEN OFF ON A PRE FLIGHT.Jan 18, 2002 · Bell 222U · Rotorcraft Tail BoomSDR CA011116007Regulator · leaking(CAN) AIRCRAFT BELL 222U POP-OUT FLOAT SYSTEM CHARGED TO 3000 PSI AFTER CHANGING FLOAT BOTTLE. SYSTEM LEAKED APPROXIMATELY 200 PSI OVER A 12 HOUR PERIOD. BY REMOVING THE LINES TO AIR BAG IT WAS CONFIRMED THAT AIR WAS LEAKING THROUGH SHEAR HEAD BY SMALL CRACKS.Sep 8, 2001 · Bell 222U · Emergency Flotation SectionSDR AU000375Spacer · corroded(AUS) TAIL ROTOR PITCH CHANGE MECHANISM SPACER SEVERELY CORRODED. A PIECE OF THE SPACER HAD FLAKED OFF AND JAMMED THE SPLINE PLATE PN 222-012-725-001 ON THE OUTPUT SHAFT SPLINES.Feb 13, 2000 · Bell 222U · Tail Rotor Control SystemSDR 2000ZZZX752Bearing · corrodedBEARING HAD EXCESSIVE PITTING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.Oct 18, 1999 · N404EM · Bell 222U · Turbine Engine Reduction GearSDR 99ZZZX3021Py Line · crackedTHIS PY AIR LINE CRACKED AND CAUSED SUDDEN DECELERATION. PILOT MADE NORMAL SINGLE ENGINE LANDING WITHIN PUBLISHED OEI LIMITATIONS. VIBRATIONS WERE RECORDED ON MAIN DRIVESHAFT. THE ENGINE ASSY AND MAIN DRIVE SHAFT WERE REPLACED.Jul 27, 1999 · N143CF · Bell 222U · Fuel Controlling SystemSDR 99ZZZX2879Shroud · flakingCOATING FLAKING OFF OF IMPELLER SHROUD PREMATURELY. REF: MCN 69. REMOVED AND REPLACED.May 25, 1999 · N219HM · Bell 222U · Turbine Engine Compressor SectionSDR 99ZZZX1798Bearing · wornBEARING WORN BEYOND SERVICEABLE LIMITS. INSTALLED AT ASE GREER FACILITY. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.Feb 25, 1999 · N404EM · Bell 222U · Turbine Engine Reduction GearSDR 99ZZZX1259Pump · leakingFUEL PUMP LEAKING FUEL FROM OVERBOARD DRAIN. REMOVED AND REPLACED.Nov 12, 1998 · N222HX · Bell 222U · Engine Fuel PumpSDR 99ZZZX1280Rotor Assy · damagedSEALING PLATE IS SEPARATING FROM BLADES. REMOVED AND REPLACED.Sep 22, 1998 · N911LW · Bell 222 · Turbine SectionSDR 99ZZZX902Housing · crackedHOUSING CRACKED AT 6 O'CLOCK STRUT. REMOVED AND REPLACED.Sep 22, 1998 · N911LW · Bell 222 · Turbine Engine Combustion SectionSDR 97ZZZX5218Manifold · crackedFUEL LEAK NOTED ON POST-FLIGHT INSPECTION. FUEL MANIFOLD WAS FOUND TO HAVE A CRACK OR HOLE AT 5 O'CLOCK POSITION. UNABLE TO DETECT WITH NAKED EYE. FUEL POOLED IN ENGINE COMPARTMENT AREA MAKING THIS A VERY DANGEROUS SITUATION. FUEL LEAKING ONTO THE TURBINE Dec 13, 1997 · N781SA · Bell 222U · Engine Fuel DistributionSDR 97ZZZX4835Tube · crackedREPLACED CRACKED PY LINE AT FUEL CONTROL UNIT.Oct 11, 1997 · N142CF · Bell 222U · Fuel Controlling SystemSDR 97ZZZX4093Fuel Manifold · leakingTUBE OR WELD CRACKED WHERE TUBE ENTERS FUEL NOZZLE FITTING. THIS IS THE SIXTH OCCURRENCE SINCE MAY, 1997. THREE WERE P/N 4-401-376-01 MANIFOLDS AND 3 WERE P/N 4-301-236-04 MANIFOLDS. THIS IS BEING ADDRESSED BY ALLIED SIGNAL.Aug 22, 1997 · N143CF · Bell 222U · Engine Fuel DistributionSDR CA970722004Fuel Manifold · leaking(CAN) THE SMELL OF FUEL WAS EVIDENT DURING DESCENT. POST FLIGHT INVESTIGATION FOUND THE FUEL MANIFOLD LEAKING AT A BRAZED WELD. THE FUEL MANIFOLD WAS REPLACED.Jul 10, 1997 · Bell 222U · Engine Fuel Distribution
Back to Honeywell LTS101-750C-1