# Service difficulty reports: Honeywell LTS101-600A-3

A list on [Honeywell LTS101-600A-3](https://openairdocs.org/engine/honeywell-lts101-600a-3.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 75 reports

- [SDR 2025FA0000754](https://openairdocs.org/sdr/2025FA0000754.md): Capacitor · broken · Oct 28, 2025 · N61HL · Snias AS350BA · Powerplant System
  > DURING ROUTINE FLIGHT OPERATION THERE WAS A SUDDEN DECREASE IN ENGINE POWER AND A RISE IN VIBRATION WAS FELT, SO THE AIRCRAFT MADE A PRECAUTIONARY UNSCHEDULED LANDING AND SHUT DOWN WITHOUT INCIDENT. UPON INSPECTION OF THE AIRCRAFT IT WAS FOUND THAT ONE OF TWO
- [SDR CA190430031](https://openairdocs.org/sdr/CA190430031.md): Friction Cup · worn · Apr 24, 2019 · Snias AS350D · Main Rotor Control
  > (CAN) HAD COMPLAINT OF FRICTION STICKING, THEN NO FRICTION, FOUND THE FRICTION BALL TO HAVE WEAR ON IT. ALSO HAD THE FRICTION CUP OR FOLLOWER ON IT (SUPPOSED TO BE A 1 PIECE ASSEMBLY, BREAK AND TURN INTO 3 PIECES. (P/N 350A27159100) THIS LOWER CUP WAS THEN AL
- [SDR CA150721003](https://openairdocs.org/sdr/CA150721003.md): Bolt · loose · Jul 19, 2015 · Snias AS350BA · Main Rotor Mast/Swashplate
  > (CAN) THE MAST CHIP PLUG, REQUIRED MORE FORCE THEN ORDINARY TO BE PULLED OUT. THE TIP OF THE CHIP PLUG WAS FOUND CHOPPED OFF AND THE INTERNAL MAGNET OF THE CHIP DETECTOR WAS APPARENT. THE AICFT WAS THEN GROUNDED. THE TRANSMISSION WAS OPENED ON SITE. RIGHT AF
- [SDR CA150604021](https://openairdocs.org/sdr/CA150604021.md): Bolt · galled · Jun 2, 2015 · Snias AS350D · Main Rotor Head
  > (CAN) WENT TO INSTALL NEW BOLTS IN STARFLEX. INSTALLED 11 OUT OF THE 12 BOLTS. INSTALLED LAST ONE.7500 PERCENT WAY IN GOT TIGHT, REMOVED BOLT AND FOUND IT GALLED UP SHANK AND WAS VERY DIFFICULT TO REMOVE. WAS PROPERLY LUBED AND INSTALLED IAW LATEST MANUAL.
- [SDR 2014FA0000542](https://openairdocs.org/sdr/2014FA0000542.md): Capacitor · broken · Sep 22, 2014 · N61HL · Snias AS350BA · Powerplant System
  > PILOT NOTICED N1 DROOPING AFTER TAKEOFF, LANDED BACK ON THE PAD, VISUAL INSPECTION OF THE ENGINE WAS PERFORMED, NOTICED THE SMALL CAPACITOR LOOKED SLIGHTLY OFF CENTER, SHOULD LOOK PERPENDICULAR TO THE ENGINE, AS A SLIGHT HAND PRESSURE WAS APPLIED THE UNIT BRO
- [SDR CA140505012](https://openairdocs.org/sdr/CA140505012.md): Fuel Control · malfunctioned · May 4, 2014 · Snias AS350BA · Fuel Control/Turbine Engines
  > (CAN) FCU INSTALLED AND ADJUSTED IAW MFG RECOMMENDATIONS DURING GROUND RUNS. LEAK TESTS CARRIED OUT SATISFACTORILY. FLIGHT TESTING CARRIED OUT FOR POST-MAINTENANCE CHECKS. DURING THIS TESTING PERIOD, THE ACFT WAS SHUTDOWN AT ONE POINT AND FAILED TO RESTART.
- [SDR CA131107007](https://openairdocs.org/sdr/CA131107007.md): Rod · cracked · Nov 7, 2013 · Snias AS350BA · Tail Rotor Head
  > (CAN) DURING A VISUAL INSPECTION, A CRACK WAS FOUND AT THE AFT END OF THE TAIL ROTOR ACTUATING ROD, WHERE THE BEARING IS SWAGED.
- [SDR CA131107004](https://openairdocs.org/sdr/CA131107004.md): Reservoir · contaminated · Nov 4, 2013 · Snias AS350BA · Hydraulic Reservoir, Main
  > (CAN) WATER AND ICE CONTAMINATION WAS FOUND IN THE HYDRAULIC RESERVOIR TAPERED FILTER.
- [SDR CA131107005](https://openairdocs.org/sdr/CA131107005.md): Reservoir · contaminated · Nov 4, 2013 · Snias AS350BA · Hydraulic Reservoir, Main
  > (CAN) WATER AND ICE CONTAMINATION WAS FOUND IN THE HYDRAULIC RESERVOIR TAPERED FILTER.
- [SDR CA130621004](https://openairdocs.org/sdr/CA130621004.md): Wire Harness · chafed · Jun 20, 2013 · Snias AS350BA · Engine Indicating System Wiring
  > (CAN) ENGINE POWER TURBINE MODULE INDICATING HARNESS WAS FOUND WORN BEYOND REPAIR DUE TO CHAFING AGAINST THE FDC/AEROFILTER INLET HOUSING. THERE WERE NO REPORTS OF INACCURATE OR LOST OF T4 INDICATION BY THE PILOT.
- [SDR CA130318022](https://openairdocs.org/sdr/CA130318022.md): Servo · malfunctioned · Mar 15, 2013 · Snias AS350BA · Rotorcraft Servo System
  > (CAN) THE OPERATION HAD TO CONDUCT PILOT TRAINING, WHICH WAS PARKED OUTDOOR FOR THE LAST 4 DAYS. AFTER THE START WAS COMPLETED THE PILOT IN COMMAND FOUND THAT THE FORE AND AFT MOVEMENT OF THE CYCLIC SERVO WAS RESTRICTED IN THE FORWARD MOVEMENT. THE ACFT WAS
- [SDR CA130318024](https://openairdocs.org/sdr/CA130318024.md): Servo · contaminated · Mar 15, 2013 · Snias AS350BA · Rotorcraft Servo System
  > (CAN) THE OPERATION HAD TO CONDUCT PILOT TRAINING WITH ACFT WHICH WAS PARKED OUTDOORS FOR THE LAST 4 DAYS. AFTER THE START WAS COMPLETED THE PILOT IN COMMAND FOUND THAT THE FORE AND AFT MOVEMENT OF THE CYCLIC SERVO WAS RESTRICTED IN THE FORWARD MOVEMENT. TH
- [SDR CA130131004](https://openairdocs.org/sdr/CA130131004.md): Idler Gear · unsecure · Jan 25, 2013 · Snias AS350BA · Turbine Engine Reduction Gear
  > (CAN) DURING THE SCHEDULED 1800 HRS INSPECTION, THE 8 BOLTS ON THE TORQUE IDLER GEAR WERE FOUND LOOSE. THE GEAR ASSY AS TO BE REMOVED AND SENT FOR DETAILED INSPECTION. A PREVIOUS SDR WAS SUBMITTED DUE TO SIMILAR PROBLEM CAUSING AN EMERGENCY LANDING, WERE THE
- [SDR CA120223007](https://openairdocs.org/sdr/CA120223007.md): Plug · leaking · Feb 23, 2012 · Snias AS350D · Fuel Storage
  > (CAN) FUEL FOUND LEAKING ON HANGER FLOOR. FOUND TO BE PLUG ON FUEL TANK, THIS ITEM IS MADE OUT OF RUBBER. RUBBER WAS CRACKED AROUND INTERAL CIRCUMFERENCE. REPLACED PART, NO FURTHER PROBLEM.
- [SDR CA120223008](https://openairdocs.org/sdr/CA120223008.md): Battery · failed · Feb 17, 2012 · Snias AS350D · Battery/Charger System
  > (CAN) ROUTINE MAINTENANCE FOUND JELL LIKE SUBSTANCE HAD LEAKED OUT OF BATTERY ON TO BATTERY MOUNT. REMOVED BATTERY, CLEANED UP AREA, REPLACED BATTERY NO FURTHER PROBLEM. CONTACTED DISTRIBUTOR FOR BATTERY, INDICATED NEVER HAD THIS PROBLEM BEFORE. WE HAD NO I
- [SDR CA111209009](https://openairdocs.org/sdr/CA111209009.md): Longeron · cracked · Dec 7, 2011 · Snias AS350BA · Fuselage Main, Longeron/Stringer
  > (CAN) NOISE WAS HEARD BY ENGINEER DURING MX WHILE MOVING CYCLIC FROM SIDE TO SIDE. AFTER THE BELLY SKIN WAS REMOVED A 5 INCH CRACK WAS FOUND IN ONE OF THE MAIN LONGERONS OF THE CABIN FLOOR. JUST BELOW WHERE THE CYCLIC MIXING UNIT ATTACHES. CRACK SEEMS TO HA
- [SDR CA120122001](https://openairdocs.org/sdr/CA120122001.md): Accumulator · leaking · Nov 22, 2011 · Snias AS350D · Hydraulic System, Main
  > (CAN) ON RUN UP PILOT PERFORMED USSUAL, GROUND CHECKS, FOUND LATTERAL MOVEMENT NOT WITHIN SPECIFICATIONS, NORMAL SHUTDOWN OCCURED. MAINTENANCE FOUND LEAKING ACCUMULATOR, ACCUMULATOR REPLACED, GROUND RUN UP CONFIRMED, NO FURTHER PROBLEM.
- [SDR CA111031002](https://openairdocs.org/sdr/CA111031002.md): Skin · cracked · Oct 31, 2011 · Snias AS350BA · Vertical Stabilizer, Plate/Skin
  > (CAN) DURING SCHEDULED 12 YEARS INSPECTION, A CRACK WAS FOUND ON VERTICAL STABILIZER T/E SKIN. A SMALL PORTION STARTED TO EMERGE (.50" LONG) BUT AFTER DISASSEMBLY FOUND (6.0" LONG). THE CRACK STARTING AREA BETWEEN 2 PARTS (FIN SPAR & SPLICING PLATE) AND WAS N
- [SDR 2011FA0000651](https://openairdocs.org/sdr/2011FA0000651.md): Damper · cracked · Sep 26, 2011 · N61HL · Snias AS350BA · Turbine Governor
  > PART FOUND CRACKED AT INSPECTION. CRACK RUNS ALONG WITH METAL GRAIN ALONG THE INBD SECTION NEXT TO WELDED NIPPLE. FAILURE OF THIS PART WILL CAUSE ENGINE FAILURE.
- [SDR CA110926004](https://openairdocs.org/sdr/CA110926004.md): Modulator · unserviceable · Sep 23, 2011 · Snias AS350BA · Turbine Engine Compressor Section
  > (CAN) PILOT REPORTED INCREASE IN COMPRESSOR SPEED AND DROP IN ROTOR RPM ON APPROACH. PILOT MANAGED TO LAND WITHOUT INCIDENT. MAINTENANCE PERSONNEL FOUND THE AIRFLOW MODULATOR DEFECTIVE DUE TO A BROKEN BLEED AIR TRANSFERT TUBE.
- [SDR CA110929011](https://openairdocs.org/sdr/CA110929011.md): Retaining Ring · deteriorated · Aug 15, 2011 · Snias AS350BA · Accessory Gearboxes
  > (CAN) - ENGINE PREVIOUSLY REMOVED FOR OIL VENTING. (PREVIOUS SDR) - ENGINE ACCESSORY GEAR BOX DISSASEMBLED FOR INTERNAL INSPECTION. ALTERNATOR GEAR FWD BEARING RETAINING RING FOUND DETERORATED. RETAINING RING REPLACED. FORWARD AND AFT ALTERNATOR GEAR SEALS
- [SDR CA110708005](https://openairdocs.org/sdr/CA110708005.md): Damper · broken · Jul 6, 2011 · Snias AS350BA · Turbine Governor
  > THE PILOT WHILE IN FLIGHT FELT A YAW MOVEMENT FROM THE ACFT FOLLOWED BY A INCREASE OF ENGINE TORQUE AND MAIN ROTOR SPEED. THE PILOT THEN REDUCED THE FUEL TO THE ENGINE WITH THE ENGINE FUEL CONTROL LEVER AND CONDUCTED A PRECAUTIONARY LANDING IN A LOGGING ROAD.
- [SDR CA110704013](https://openairdocs.org/sdr/CA110704013.md): Oil System · leaking · Jun 29, 2011 · Snias AS350D · Turbine Engine Oil System
  > (CAN) ENGINE VENTING LARGE AMOUNTS OF OIL OUT OF VENT TUBE.
- [SDR CA110407007](https://openairdocs.org/sdr/CA110407007.md): Engine · making metal · Mar 28, 2011 · Snias AS350D · Engine (Turbine/Turboprop)
  > (CAN) ENGINE CHIP LIGHT DETECTED. ACFT LANDED. CHIP PLUG INSPECTION REVEALED METAL PARTCLES AND CHUNKS ON 2 OF 3 PLUGS INCLUDING ACCESSORY GEARBOX CHIP PLUG.
- [SDR CA110209016](https://openairdocs.org/sdr/CA110209016.md): Cargo Hook · failed · Jan 16, 2011 · Snias AS350BA · Cargo Compartments
  > UN-COMMANDED BELLY CARGO HOOK RELEASE.
- [SDR CA110128003](https://openairdocs.org/sdr/CA110128003.md): Seal · leaking · Jan 11, 2011 · Snias AS350BA · Turbine Engine Oil System
  > (CAN) OIL LEAKAGE FROM FORWARD OUTPUT SEAL.
- [SDR CA110209011](https://openairdocs.org/sdr/CA110209011.md): Transmitter · dirty · Dec 1, 2010 · Snias AS350D · Fuel Quantity Sensor
  > FUEL QUANTITY LEVEL INDICATION FOUND INCORRECT. DIRT ACCUMULATION FOUND IN BOTTOM OF UNIT WAS CLEANED OUT AND UNIT REINSTALLED AND FUNCTION TESTED OK.
- [SDR CA110209013](https://openairdocs.org/sdr/CA110209013.md): Bushing · stiff · Nov 27, 2010 · Snias AS350BA · Rotorcraft Flight Control
  > PILOT REPORTED STIFF IN LATERAL CYCLIC CONTROL. MIXING UNIT LEVER BUSHING FOUND TOO TIGHT AND BIND WHEN ROTATED.
- [SDR CA110209014](https://openairdocs.org/sdr/CA110209014.md): Indicator · stuck · Nov 1, 2010 · Snias AS350BA · Fuel Quantity Indicator
  > FUEL QUANTITY INDICATION STICKING.
- [SDR CA100701005](https://openairdocs.org/sdr/CA100701005.md): Filter · damaged · Jun 28, 2010 · Snias AS350BA · Engine Fuel Distribution
  > WHEN REMOVING THE P/C FILTER FOR A SCHEDULED 100 HR CLEANING THE THREADS ON THE FITTING WERE VERY TIGHT TO COME OFF. INSP OF THE THREADS ON THE FILTER HSG SHOWED THE THREADS WERE STRIPPED. LOG BOOK SHOWED THE P/C FILTER ASSY WAS INSTALLED NEW JUST 68 HR FOR T
- [SDR CA110209010](https://openairdocs.org/sdr/CA110209010.md): Fuel Control · malfunctioned · Apr 11, 2010 · Snias AS350D · Fuel Control/Turbine Engines
  > (CAN) PILOT REPORTED ENGINE SURGING DURING LOW SETTING BETWEEN 40 PERCENT AND 60 PERCENT TORQUE. FUEL CONTROL UNIT REPLACED AND TEST FLIGHT COMPLETED WITH NO SURGING NOTED. (TC NR 20110209010)
- [SDR CA090413003](https://openairdocs.org/sdr/CA090413003.md): Pump · unserviceable · Mar 21, 2009 · Snias AS350BA · Hydraulic Pump (Electric/Engine), Main
  > (CAN) HYD FEED BACK ON HYD TEST PRIOR TO FLIGHT. CHECK ALL SYS AND FLUID. FOUND METAL INSIDE FILTER. REPLACED HYDR PUMP WITH SERVICEABLE PUMP. HOLD PUMP AS BEEN INSPECTED AND GEAR FOUND TO BE WORN INSIDE THE PUMP. CHIP DETECTOR AS NOT COLLECTED ANY METAL.
- [SDR CA080115009](https://openairdocs.org/sdr/CA080115009.md): Ground Wire · failed · Jan 10, 2008 · Snias AS350B · Rotors Flight Control System Wiring
  > (CAN) IN THE PROCESS OF DOING RECURRENT TRAINING FLIGHT. AFTER SEVERAL SIMULATED HYD FAILURES IN AND OUT OF GROUD EFFECT HOVER, PROCEEDED TO PRACTICE THE SIMULATED HYD FAILURE. THE SIMULATED PROCEDURE WAS INITIATED FROM 100 FOOT HOVER WITH A VERBAL WARNING THA
- [SDR SSH2006F00000](https://openairdocs.org/sdr/SSH2006F00000.md): Fuel Control · malfunctioned · Nov 27, 2006 · N9511 · Snias AS350B2 · Fuel Controlling System
  > PILOT REPORTED ON TAKEOFF, HE INCREASED THE COLLECTIVE TO GET THE HELICOPTER LIGHT ON THE SKIDS PAUSING FOR A FEW SECONDS SO THE ROTOR RPM STABILIZED THEN CONTINUED THE TAKEOFF. JUST ABOUT 3 FT OFF THE GROUND, MOVING FORWARD INTO FLIGHT THE LOW RPM AUDIO SOUN
- [SDR CA060920002](https://openairdocs.org/sdr/CA060920002.md): Line · cracked · Sep 20, 2006 · Snias AS350BA · Aircraft Fuel Distribution System
  > (CAN) GOVERNOR FAIL TO RESPONSE ON TAKE OFF, VISUAL CHECK OF ENGINE COMPARTMENT FOUND CRACKED LINE ON GOVERNOR TO FCU LINE NP TO PR TO PG LINE. LINE REPLACED WITH NEW A/C BACK TO SERVICE. (TC NR 20060920002)
- [SDR CA060920003](https://openairdocs.org/sdr/CA060920003.md): Starter Gen · broken · Sep 20, 2006 · Snias AS350BA · Starter-Generator
  > (CAN) GENERATOR LIGHT CAME ON IN FLIGHT, LANDED AND SHOTDOWN, STARTER FOUND BROKEN. STARTER REPLACED AND SENT FOR OVERHAUL. (TC NR 20060920003)
- [SDR CA060510003](https://openairdocs.org/sdr/CA060510003.md): Fcu · failed · May 3, 2006 · Snias AS350BA · Fuel Control/Turbine Engines
  > ON SECOND START OF THE DAY, A FLAME WAS SEEN COMING OUT OF EXHAUST AND A RAPID INCREASE IN TURBINE OUTLET TEMPERATURE. AFTER SEVERAL MINUTES, A SECOND ATTEMPT WAS GIVEN WITH SIMILAR RESULTS.
- [SDR CA060313005](https://openairdocs.org/sdr/CA060313005.md): Starter Gen · noisy · Mar 9, 2006 · Snias AS350BA · Starter-Generator
  > VIBRATION ON START TO 60 PERCENT, AND STRANGE NOISE FROM THE ENGINE, FOUND BROKEN STARTER.
- [SDR CA051220006](https://openairdocs.org/sdr/CA051220006.md): Servo · inoperative · Dec 6, 2005 · Snias AS350BA · Rotorcraft Servo System
  > (CAN) PILOT REPORTED STIFF RAPID LT MOVEMENT AND COLLECTIVE STICK RISING. AIRCRAFT TESTED ON HYDRAULIC BENCH AND WE FOUND THAT LT SERVO WAS SLOWER TO RETRACT. THE AIRCRAFT WAS OPERATING CORRECTLY AFTER AFFECTED SERVO WAS REPLACED. THIS PROBLEM WAS IMPOSSIBLE
- [SDR CA051208007](https://openairdocs.org/sdr/CA051208007.md): B-Nut · cracked · Nov 11, 2005 · Snias AS350BA · Hydraulic Power Accumulator, Main
  > (CAN) DECREASED OF 15 RPM OBSERVED IN FLIGHT. LEAK CHECK COMPLETE AND LEAK FOUND ON ACCUMULATOR P/N: 366A54-1088. ACCUMULATOR B-NUT TIGHT AND LEAK CHECK COMPLETED, LEAK FOUND ACCUMULATOR REMOVED FROM AC AND FOUND CRACK AND FALL IN 2 PIECES REPLACED WITH NEW
- [SDR CA050609003](https://openairdocs.org/sdr/CA050609003.md): Limit Switch · failed · Mar 18, 2005 · Snias AS350D · Turbine Governor
  > (CAN) DURING OVER SPEED LIMITER TEST, ENGINE NG OSCILLATING 10 PERCENT, FOLLOWED BY TOT AND ITT REPLACED OVER SPEED LIMITER - PROBLEM CORRECTED.
- [SDR CA050609002](https://openairdocs.org/sdr/CA050609002.md): Pump · leaking · Mar 15, 2005 · Snias AS350D · Engine Fuel Pump
  > (CAN) DURING GROUND RUNUP, FUEL WAS LEAKING FROM FUEL PUMP, WHERE THE FUEL PUMP ATTACHES TO THE GEARBOX. FUEL PUMP RECEIVED AFTER INTERNAL SPLINE AD INSPECTION WHICH REQUIRES REMOVAL OF FRONT SEAL HOUSING TO ENABLE REMOVAL OF SHAFT. THIS SEEMS TO BE THE AREA
- [SDR CA050312003](https://openairdocs.org/sdr/CA050312003.md): Magnetic Seal · dislodged · Feb 23, 2005 · Snias AS350D · Tail Rotor Gearbox
  > (CAN) AFTER LANDING, OIL WAS FOUND ALL OVER TAIL GEARBOX AREA, MAINTENANCE WAS CALLED AND T/R G/B WAS REPLACED WITH A RENTAL AND NO FURTHER PROBLEM WAS FOUND. UPON INSPECTION AT MAIN BASE THE VENT HOLE ON THE INPUT WAS FOUND PLUGGED UP, THIS WE FEEL WAS THE
- [SDR CA050216009](https://openairdocs.org/sdr/CA050216009.md): Skin · cracked · Feb 16, 2005 · Snias AS350BA · Rotorcraft Tail Boom
  > (CAN) CRACK FOUND ON VERTICAL UPPER FIN.
- [SDR CA040304003](https://openairdocs.org/sdr/CA040304003.md): O-Ring · failed · Feb 25, 2004 · Snias AS350BA · Rotorcraft Servo System
  > (CAN) HAD A HARD OVER CYCLIC PROBLEM WITH AN ENGINE, THE AIRCRAFT WAS EQUIPPED WITH MFG SERVOS. HAD THIS PROBLEM AT 30 DEGREES C TO -15 DEGREES C (OUTSIDE TEMPERATURE), NO DIFFERENCE. BOLT LATERAL SERVOS WAS DUE FOR OVERHAUL, SEND SERVOS FOR OVERHAUL AND REINS
- [SDR CA040304004](https://openairdocs.org/sdr/CA040304004.md): Belt · unbonded · Feb 25, 2004 · Snias AS350BA · Hydraulic Pump (Electric/Engine), Main
  > (CAN) WHILE IN FLIGHT THE PILOT EXPERIENCE A LOST OF HYDRAULIC POWER AND EMERGENCY LANDED ON A NEAR BY LEAKE WITH NO DAMAGE TO AIRCRAFT. AFTER INSPECTION THE HYDRAULIC BELT HAS BEEN FOUND SECTIONED AT THE GLUED JOINT.
- [SDR CA040131001](https://openairdocs.org/sdr/CA040131001.md): Drive Belt · broken · Jan 30, 2004 · Snias AS350BA · Hydraulic Pump (Electric/Engine), Main
  > (CAN) THE BELT BROKE 2 MINUTES AFTER TAKE-OFF. OAT WAS -15C. THE AIRCRAFT MADE A NORMAL HYDRAULIC-OFF LANDING. NO UNCOMMANDED CONTROL MOVEMENT OCCURRED AT THE TIME OF THE INCIDENT.
- [SDR CA031015020](https://openairdocs.org/sdr/CA031015020.md): Spacer · broken · Oct 13, 2003 · Snias AS350D · Fuel Storage
  > (CAN) SENDER REMOVED FOR CLEANING TANK, AND NOTICED SEVERAL BRIDGE SPACERS HAD EITHER BROKEN OR LOOSE RIVETS.
- [SDR 2003FA0000772](https://openairdocs.org/sdr/2003FA0000772.md): Diffuser · misoverhauled · Jul 24, 2003 · Turbine Engine Compressor Section
  > DIFFUSER 4-101-260-04 (SN 0062A / C301849) WAS OVERHAULED, TRACKING NR C301849-1 DATED 02/26/2003. RECEIVED DIFFUSER FROM CUSTOMER FOR INSTALLATION IN THEIR ENGINE. UPON INSPECTION, DISCOVERED THAT PART WAS MISSING P3 AIR BLEED HOLE. ADDITIONAL DIMENSIONAL IN
- [SDR CA030530010](https://openairdocs.org/sdr/CA030530010.md): Fuel Control · failed · May 19, 2003 · Snias AS350D · Fuel Control/Turbine Engines
  > (CAN) NO FUEL COMING OUT THE FUEL CONTROL UNIT. IT HAPPENED ON THE FIRST START ATTEMPT, IN THE MORNING. INTERNAL FAILURE OF FCU SUSPECTED, SINCE ALL FUEL LINES HAVE BEEN BLED FROM AIR. PREVIOUS FLIGHTS HAD NOT REVEALED ANY FLUCTUATIONS OR PARAMETERS PROBLEMS.

Next page: https://openairdocs.org/engine/honeywell-lts101-600a-3/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 = 'LTS101600A3'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/honeywell-lts101-600a-3/reports

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