# Service difficulty reports: Honeywell LTS101-750C-1

A list on [Honeywell LTS101-750C-1](https://openairdocs.org/engine/honeywell-lts101-750c-1.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 68 reports

- [SDR CA190426021](https://openairdocs.org/sdr/CA190426021.md): Engine · power loss · Apr 26, 2019 · Bell 222U · Engine (Turbine/Turboprop)
  > (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)
- [SDR QMLA2014090514107](https://openairdocs.org/sdr/QMLA2014090514107.md): Engine · leaking · Sep 5, 2014 · N222MN · Bell 222U · Engine (Turbine/Turboprop)
  > RETURNING 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 SM
- [SDR CA130314004](https://openairdocs.org/sdr/CA130314004.md): Case · cracked · Mar 13, 2013 · Bell 222B · Main Rotor Gearbox
  > (CAN) TOP CASE RT INBD COLLECTIVE IDLER LUG FOUND CRACKED. BUSHING WORN BEYOND LIMIT. CASE REPLACED.
- [SDR QMLA2012092512159](https://openairdocs.org/sdr/QMLA2012092512159.md): Longeron · cracked · Sep 25, 2012 · N419MA · Bell 222UT · Rotorcraft Tail Boom
  > DURING INSPECTION OF TAIL ROTOR ACTUATOR AND SURROUNDING AREA FOUND CRACK ON LONGERON ABOVE AND TO THE LT OF THE ACTUATOR.
- [SDR QMLA2012032912038](https://openairdocs.org/sdr/QMLA2012032912038.md): Actuator · inoperative · Mar 29, 2012 · N222AM · Bell 222U · Power Lever
  > ON 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 PAR
- [SDR QMLA2012032512036](https://openairdocs.org/sdr/QMLA2012032512036.md): Unknown · smoke · Mar 25, 2012 · N117MK · Bolkms BK117B2 · Engine (Turbine/Turboprop)
  > DURING 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, &
- [SDR CA111130011](https://openairdocs.org/sdr/CA111130011.md): Arm · damaged · Nov 30, 2011 · Bell 222U · Main Rotor Head
  > (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.
- [SDR QMLA2011092111094](https://openairdocs.org/sdr/QMLA2011092111094.md): Engine · making metal · Sep 21, 2011 · N419MA · Bell 222UT · Engine (Turbine/Turboprop)
  > NR 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 ILL
- [SDR QMLA2011061511065](https://openairdocs.org/sdr/QMLA2011061511065.md): Gearbox · making metal · Jun 15, 2011 · N220LN · Bell 222U · Turbine Engine Reduction Gear
  > AFTER 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
- [SDR QMLA2010102510071](https://openairdocs.org/sdr/QMLA2010102510071.md): Disc · unserviceable · Oct 25, 2010 · N220LN · Bell 222UT · Main Rotor Brake
  > DURING 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 DIS
- [SDR 2010F00057](https://openairdocs.org/sdr/2010F00057.md): Gear · failed · Mar 10, 2010 · N222AM · Bell 222UT · Main Rotor Gearbox
  > SPIRAL BEVEL COLLECTOR GEAR FAIL APART, (DRIVE TOOTH/GEAR BOKE AWAY/SEPARATED FROM THE BEVEL GEAR BODY) WITH IN THE MAIN ROTOR GEARBOX/TRANSMISSION.
- [SDR CA081222008](https://openairdocs.org/sdr/CA081222008.md): Servo · unknown · Dec 8, 2008 · Bell 222U · Rotorcraft Servo System
  > (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 OCC
- [SDR CA090127010](https://openairdocs.org/sdr/CA090127010.md): Bracket · cracked · Nov 26, 2008 · Snias AS350B2 · Engine Fuel Distribution
  > HIGH PRESSURE ENGINE FUEL FILTER BRACKET CRACKING AT TOP BOLT HOLE DUE TO HARMONIC VIBRATION, KNOWN PROBLEM.
- [SDR 200709152121](https://openairdocs.org/sdr/200709152121.md): Feeder Cable · shorted · Sep 15, 2007 · N911MK · Bell 222UT · Fire Protection System Wiring
  > CABLE SHORTED, CAUSING FALSE FIRE WARNING INDICATION.
- [SDR BAQA200700022](https://openairdocs.org/sdr/BAQA200700022.md): Blade · loose · Jun 27, 2007 · N587MG · Bell 222U · Tail Rotor Blades
  > WHILE 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.
- [SDR BAQA200700020](https://openairdocs.org/sdr/BAQA200700020.md): Blade · loose · Jun 25, 2007 · N222LF · Bell 222UT · Tail Rotor Blades
  > WHILE 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.
- [SDR BAQA200700021](https://openairdocs.org/sdr/BAQA200700021.md): Blade · loose · Jun 25, 2007 · N222LF · Bell 222UT · Tail Rotor Blades
  > WHILE 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.
- [SDR 47540060306](https://openairdocs.org/sdr/47540060306.md): Tube · cracked · Jun 3, 2006 · N402MA · Bell 222U · Fuel Controlling System
  > ONE OF THE AIR LINES THAT RUNS FROM THE FUEL CONTROL TO THE OVERSPEED SOLENOID CRACKED AT A FLARE, CAUSING ENGINE TO DECEL.
- [SDR HEEA107416](https://openairdocs.org/sdr/HEEA107416.md): Transmitter · failed · Dec 17, 2005 · N6992 · Bell 222U · Engine Oil Pressure
  > NR 1 ENGINE OIL PRESSURE GAUGE PEGGED OUT ON THE HIGH SIDE. MAINTENANCE REPLACED THE ENGINE OIL PRESSURE TRANSMITTER.
- [SDR 47518022205](https://openairdocs.org/sdr/47518022205.md): Flexure · delaminated · Feb 22, 2005 · N419MA · Bell 222UT · Main Rotor Transmission Mount
  > SHORTLY 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 COLLECTIVE
- [SDR 47518011705](https://openairdocs.org/sdr/47518011705.md): Line · ruptured · Jan 17, 2005 · N419MA · Bell 222UT · Hydraulic System, Main
  > THE 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 PROBL
- [SDR 047504123104](https://openairdocs.org/sdr/047504123104.md): Servo · malfunctioned · Dec 31, 2004 · N431MA · Bell 222U · Hydraulic System, Main
  > NR 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.
- [SDR 47504123104](https://openairdocs.org/sdr/47504123104.md): Servo · failed · Dec 31, 2004 · N431MA · Bell 222U · Hydraulic Power System
  > SCENE 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. PATIEN
- [SDR 47567122504](https://openairdocs.org/sdr/47567122504.md): Link · failed · Dec 25, 2004 · N220LN · Bell 222U · Main Rotor Transmission Mount
  > WHILE 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
- [SDR CA041007009](https://openairdocs.org/sdr/CA041007009.md): Skin · cracked · Sep 29, 2004 · Bell 222U · Rotorcraft Tail Boom
  > (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.
- [SDR N406MA0204](https://openairdocs.org/sdr/N406MA0204.md): Wire · chafed · Feb 27, 2004 · N406MA · Bell 222B · Turbine Engine System Wiring
  > DURING 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.
- [SDR N406MA](https://openairdocs.org/sdr/N406MA.md): Detector · broken · Feb 18, 2004 · N406MA · Bell 222B · Engine Oil Temperature
  > WHILE 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 ABSENCE
- [SDR N431MA](https://openairdocs.org/sdr/N431MA.md): Mount · debonded · Feb 10, 2004 · N431MA · Bell 222U · Main Rotor Transmission Mount
  > ENROUTE 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.
- [SDR BAQA087531](https://openairdocs.org/sdr/BAQA087531.md): Pump · failed · Jun 8, 2003 · N219HM · Bell 222U · Engine Fuel Pump
  > FUEL PUMP DOESN'T TURN FREELY. REPLACED WITH SERVICEABLE UNIT.
- [SDR BAQA087055](https://openairdocs.org/sdr/BAQA087055.md): Pump · failed · Jun 8, 2003 · N219HM · Bell 222U · Engine Fuel Pump
  > FUEL PUMP WOULD NOT TURN. REPLACED WITH SERVICEABLE UNIT.
- [SDR BAQA085865](https://openairdocs.org/sdr/BAQA085865.md): Manifold · cracked · Mar 31, 2003 · N911WJ · Bolkms BK117A4 · Engine Fuel Distribution
  > CRACKED AND LEAKING FUEL AT 10 DEGREE CLOCK NOZZLE. HARD CARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT.
- [SDR CA030228004](https://openairdocs.org/sdr/CA030228004.md): Fitting · cracked · Feb 21, 2003 · Bell 222U · Fuselage Main, Bulkhead
  > (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.
- [SDR HEEA083048](https://openairdocs.org/sdr/HEEA083048.md): Valve · stuck · Jan 7, 2003 · N6992 · Bell 222U · Fuel Control/Turbine Engines
  > FUEL CONTROL VALVE IS STUCK IN THE NORMAL MODE.
- [SDR CA021001001](https://openairdocs.org/sdr/CA021001001.md): Bracket · cracked · Jul 11, 2002 · Bell 222U · Passenger/Crew Doors
  > (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 ULTIMATE
- [SDR CA020521004](https://openairdocs.org/sdr/CA020521004.md): Fitting · worn · Apr 11, 2002 · Bell 222U · Engine Fuel Distribution
  > (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 FITT
- [SDR CA020228013](https://openairdocs.org/sdr/CA020228013.md): Sleeve · worn · Feb 1, 2002 · Bell 222B · Main Rotor Head
  > (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 BEARINGS
- [SDR CA020131002](https://openairdocs.org/sdr/CA020131002.md): Fitting · broken · Jan 18, 2002 · Bell 222U · Rotorcraft Tail Boom
  > (CAN) VERTICAL LOWER FIN FITTING FOUND ATTACHMENT LUG BROKEN OFF ON A PRE FLIGHT.
- [SDR CA011116007](https://openairdocs.org/sdr/CA011116007.md): Regulator · leaking · Sep 8, 2001 · Bell 222U · Emergency Flotation Section
  > (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.
- [SDR AU000375](https://openairdocs.org/sdr/AU000375.md): Spacer · corroded · Feb 13, 2000 · Bell 222U · Tail Rotor Control System
  > (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.
- [SDR 2000ZZZX752](https://openairdocs.org/sdr/2000ZZZX752.md): Bearing · corroded · Oct 18, 1999 · N404EM · Bell 222U · Turbine Engine Reduction Gear
  > BEARING HAD EXCESSIVE PITTING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
- [SDR 99ZZZX3021](https://openairdocs.org/sdr/99ZZZX3021.md): Py Line · cracked · Jul 27, 1999 · N143CF · Bell 222U · Fuel Controlling System
  > THIS 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.
- [SDR 99ZZZX2879](https://openairdocs.org/sdr/99ZZZX2879.md): Shroud · flaking · May 25, 1999 · N219HM · Bell 222U · Turbine Engine Compressor Section
  > COATING FLAKING OFF OF IMPELLER SHROUD PREMATURELY. REF: MCN 69. REMOVED AND REPLACED.
- [SDR 99ZZZX1798](https://openairdocs.org/sdr/99ZZZX1798.md): Bearing · worn · Feb 25, 1999 · N404EM · Bell 222U · Turbine Engine Reduction Gear
  > BEARING WORN BEYOND SERVICEABLE LIMITS. INSTALLED AT ASE GREER FACILITY. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
- [SDR 99ZZZX1259](https://openairdocs.org/sdr/99ZZZX1259.md): Pump · leaking · Nov 12, 1998 · N222HX · Bell 222U · Engine Fuel Pump
  > FUEL PUMP LEAKING FUEL FROM OVERBOARD DRAIN. REMOVED AND REPLACED.
- [SDR 99ZZZX1280](https://openairdocs.org/sdr/99ZZZX1280.md): Rotor Assy · damaged · Sep 22, 1998 · N911LW · Bell 222 · Turbine Section
  > SEALING PLATE IS SEPARATING FROM BLADES. REMOVED AND REPLACED.
- [SDR 99ZZZX902](https://openairdocs.org/sdr/99ZZZX902.md): Housing · cracked · Sep 22, 1998 · N911LW · Bell 222 · Turbine Engine Combustion Section
  > HOUSING CRACKED AT 6 O'CLOCK STRUT. REMOVED AND REPLACED.
- [SDR 97ZZZX5218](https://openairdocs.org/sdr/97ZZZX5218.md): Manifold · cracked · Dec 13, 1997 · N781SA · Bell 222U · Engine Fuel Distribution
  > FUEL 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
- [SDR 97ZZZX4835](https://openairdocs.org/sdr/97ZZZX4835.md): Tube · cracked · Oct 11, 1997 · N142CF · Bell 222U · Fuel Controlling System
  > REPLACED CRACKED PY LINE AT FUEL CONTROL UNIT.
- [SDR 97ZZZX4093](https://openairdocs.org/sdr/97ZZZX4093.md): Fuel Manifold · leaking · Aug 22, 1997 · N143CF · Bell 222U · Engine Fuel Distribution
  > TUBE 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.
- [SDR CA970722004](https://openairdocs.org/sdr/CA970722004.md): Fuel Manifold · leaking · Jul 10, 1997 · Bell 222U · Engine Fuel Distribution
  > (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.

Next page: https://openairdocs.org/engine/honeywell-lts101-750c-1/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/engine/honeywell-lts101-750c-1/reports

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