# Honeywell LTS101-600A-3

- Type: Engine model (FAA registry)
- Registry code: 33818
- Manufacturer (registry): HONEYWELL
- Model: LTS101-600A-3
- Engine type: Turbo-shaft
- Power: 615 hp
- Data sheet: [TCDS E5NE](https://openairdocs.org/tcds/E5NE) (OpenAirDocs)
- Holder: Intermountain Turbine Services Inc.
- Installed in: 0 registered aircraft
- Page: https://openairdocs.org/engine/honeywell-lts101-600a-3

Model codes come from the FAA registry's reference file.

## ADs that may apply (OpenAirDocs)

Matched to this engine model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2011-23-13](https://openairdocs.org/ad/2011-23-13): Power turbine governors (PTG) · Honeywell International LTS101-600A-2, LTS101-600A-3, LTS101-600A-3A and 1 more. Effective Nov 29, 2011
- [AD 2011-08-06](https://openairdocs.org/ad/2011-08-06): Power turbine rotors · Honeywell International LTP 101-600A-1A, LTP 101-700A-1A, LTS101-600A-2 and 10 more. Effective May 17, 2011
- [AD 2009-24-12](https://openairdocs.org/ad/2009-24-12): Gas generator · Honeywell International LTP 101-600A-1A, LTP 101-700A-1A, LTS101-600A-2 and 12 more. Effective Jan 4, 2010
- [AD 2002-03-09 R1](https://openairdocs.org/ad/2002-03-09-R1): Impellers · Honeywell International LTP 101-600, LTP 101-600A, LTP 101-600A-1A and 14 more. Effective Mar 27, 2002
- [AD 2001-25-04](https://openairdocs.org/ad/2001-25-04): Fuel Controls · Honeywell International LTP 101-600A-1A, LTP 101-700A-1A, LTS101-600A-2 and 1 more. Effective Jan 23, 2002
- [AD 2001-22-07](https://openairdocs.org/ad/2001-22-07): Rigid Tube Fuel Manifold Assemblies · Honeywell International LTP 101-600, LTP 101-600A, LTP 101-600A-1A and 14 more. Effective Nov 30, 2001
- [AD 2001-17-15](https://openairdocs.org/ad/2001-17-15): Engine Fuel Pumps · Honeywell International LTP 101-600A-1A, LTP 101-700A-1A, LTS101-600A-2 and 2 more. Effective Oct 1, 2001
- [AD 96-12-27](https://openairdocs.org/ad/96-12-27): Gas Generator Turbine Disk · Honeywell International LTP 101-600, LTP 101-600A, LTP 101-600A-1A and 21 more. Effective Aug 19, 1996
- [AD 96-12-05](https://openairdocs.org/ad/96-12-05): Turbine rotors · Honeywell International LTP 101-600, LTP 101-600A, LTP 101-600A-1A and 14 more. Effective Aug 12, 1996
- [AD 96-10-04](https://openairdocs.org/ad/96-10-04): Fuel control · Honeywell International LTS101-600A-2 and LTS101-600A-3. Effective Jun 13, 1996
- [AD 96-06-10](https://openairdocs.org/ad/96-06-10): Power turbine (PT) disk · Honeywell International LTS101-600A-2, LTS101-600A-3 and LTS101-750B-2. Effective May 28, 1996
- [AD 95-16-04](https://openairdocs.org/ad/95-16-04): Axial Compressor Rotors · Honeywell International LTP 101-600, LTP 101-600A, LTP 101-600A-1A and 21 more. Effective Oct 2, 1995
- [AD 94-18-06](https://openairdocs.org/ad/94-18-06): Bearings · Honeywell International LTP 101-600, LTP 101-600A, LTP 101-600A-1A and 21 more. Effective Sep 26, 1994
- [AD 93-13-11](https://openairdocs.org/ad/93-13-11): Gas Generator Turbine Rotor Disk · Honeywell International LTP 101-600, LTP 101-600A, LTP 101-600A-1A and 22 more. Effective Nov 8, 1993
- [AD 92-15-07](https://openairdocs.org/ad/92-15-07): Integrally Cast Power Turbine (PT) Rotor Blade · Honeywell International LTP 101-600, LTP 101-600A, LTP 101-600A-1A and 21 more. Effective Sep 2, 1992
- [AD 88-14-01](https://openairdocs.org/ad/88-14-01): Power Turbine Disk · Honeywell International LTS101-600A, LTS101-600A-1, LTS101-600A-2 and 17 more. Effective Jul 6, 1988
- [AD 86-10-04](https://openairdocs.org/ad/86-10-04): Gas Producer (G.P.) Blade · Honeywell International LTP 101-600A-1A, LTP 101-700A-1A, LTS101-600A-2 and 11 more. Effective May 16, 1986

Historical (superseded or no longer in force):

- [AD 95-09-02](https://openairdocs.org/ad/95-09-02) (historical): Fuel Pumps · Honeywell International LTP 101-600, LTP 101-600A, LTP 101-600A-1A and 12 more. Effective May 10, 1995

## Registered aircraft

None registered with this engine model now.

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB SEA08MA136](https://openairdocs.org/ntsb/SEA08MA136), May 24, 2008: Aerospatiale AS-350-D (N67GE), Avalon, CA, destroyed, 3 fatal. Probable cause: Loss of engine power during approach for landing due to a fatigue fracture of a power turbine blade.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Accident 20080524837089A](https://openairdocs.org/incident/20080524837089A), May 24, 2008: Snias AS350D (N67GE), Catalina Islan, CA, Destroyed, 3 fatal. (-23) On may 24, 2008, at 0920 pacific daylight time, an aerospatiale AS-350-D helicopter, N67GE, operated by island express helicopters, inc. impacted terrain…

## Service difficulty reports (75, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR 2025FA0000754](https://openairdocs.org/sdr/2025FA0000754), Oct 28, 2025: CAPACITOR. BROKEN. 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 L
- [SDR CA190430031](https://openairdocs.org/sdr/CA190430031), Apr 24, 2019: FRICTION CUP. WORN. (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
- [SDR CA150721003](https://openairdocs.org/sdr/CA150721003), Jul 19, 2015: BOLT. LOOSE. (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
- [SDR CA150604021](https://openairdocs.org/sdr/CA150604021), Jun 2, 2015: BOLT. GALLED. (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 GALL
- [SDR 2014FA0000542](https://openairdocs.org/sdr/2014FA0000542), Sep 22, 2014: CAPACITOR. BROKEN. 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 
- [SDR CA140505012](https://openairdocs.org/sdr/CA140505012), May 4, 2014: FUEL CONTROL. MALFUNCTIONED. (CAN) FCU INSTALLED AND ADJUSTED IAW MFG RECOMMENDATIONS DURING GROUND RUNS. LEAK TESTS CARRIED OUT SATISFACTORILY. FLIGHT TESTING CARRIED OUT FOR POST-MAINTENA
- [SDR CA131107007](https://openairdocs.org/sdr/CA131107007), Nov 7, 2013: ROD. CRACKED. (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), Nov 4, 2013: RESERVOIR. CONTAMINATED. (CAN) WATER AND ICE CONTAMINATION WAS FOUND IN THE HYDRAULIC RESERVOIR TAPERED FILTER.
- [SDR CA131107005](https://openairdocs.org/sdr/CA131107005), Nov 4, 2013: RESERVOIR. CONTAMINATED. (CAN) WATER AND ICE CONTAMINATION WAS FOUND IN THE HYDRAULIC RESERVOIR TAPERED FILTER.
- [SDR CA130621004](https://openairdocs.org/sdr/CA130621004), Jun 20, 2013: WIRE HARNESS. CHAFED. (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
- [SDR CA130318022](https://openairdocs.org/sdr/CA130318022), Mar 15, 2013: SERVO. MALFUNCTIONED. (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 T
- [SDR CA130318024](https://openairdocs.org/sdr/CA130318024), Mar 15, 2013: SERVO. CONTAMINATED. (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 FO
- [SDR CA130131004](https://openairdocs.org/sdr/CA130131004), Jan 25, 2013: IDLER GEAR. UNSECURE. (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 INSP
- [SDR CA120223007](https://openairdocs.org/sdr/CA120223007), Feb 23, 2012: PLUG. LEAKING. (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. REPLA
- [SDR CA120223008](https://openairdocs.org/sdr/CA120223008), Feb 17, 2012: BATTERY. FAILED. (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
- [SDR CA111209009](https://openairdocs.org/sdr/CA111209009), Dec 7, 2011: LONGERON. CRACKED. (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 
- [SDR CA120122001](https://openairdocs.org/sdr/CA120122001), Nov 22, 2011: ACCUMULATOR. LEAKING. (CAN) ON RUN UP PILOT PERFORMED USSUAL, GROUND CHECKS, FOUND LATTERAL MOVEMENT NOT WITHIN SPECIFICATIONS, NORMAL SHUTDOWN OCCURED. MAINTENANCE FOUND LEAKING ACC
- [SDR CA111031002](https://openairdocs.org/sdr/CA111031002), Oct 31, 2011: SKIN. CRACKED. (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 DISASSEMB
- [SDR 2011FA0000651](https://openairdocs.org/sdr/2011FA0000651), Sep 26, 2011: DAMPER. CRACKED. 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), Sep 23, 2011: MODULATOR. UNSERVICEABLE. (CAN) PILOT REPORTED INCREASE IN COMPRESSOR SPEED AND DROP IN ROTOR RPM ON APPROACH. PILOT MANAGED TO LAND WITHOUT INCIDENT. MAINTENANCE PERSONNEL FOUND THE AIR
- [SDR CA110929011](https://openairdocs.org/sdr/CA110929011), Aug 15, 2011: RETAINING RING. DETERIORATED. (CAN) - ENGINE PREVIOUSLY REMOVED FOR OIL VENTING . (PREVIOUS SDR) - ENGINE ACCESSORY GEAR BOX DISSASEMBLED FOR INTERNAL INSPECTION. ALTERNATOR GEAR FWD BEARING
- [SDR CA110708005](https://openairdocs.org/sdr/CA110708005), Jul 6, 2011: DAMPER. BROKEN. 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
- [SDR CA110704013](https://openairdocs.org/sdr/CA110704013), Jun 29, 2011: OIL SYSTEM. LEAKING. (CAN) ENGINE VENTING LARGE AMOUNTS OF OIL OUT OF VENT TUBE.
- [SDR CA110407007](https://openairdocs.org/sdr/CA110407007), Mar 28, 2011: ENGINE. MAKING METAL. (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), Jan 16, 2011: CARGO HOOK. FAILED. UN-COMMANDED BELLY CARGO HOOK RELEASE.
- [SDR CA110128003](https://openairdocs.org/sdr/CA110128003), Jan 11, 2011: SEAL. LEAKING. (CAN) OIL LEAKAGE FROM FORWARD OUTPUT SEAL.
- [SDR CA110209011](https://openairdocs.org/sdr/CA110209011), Dec 1, 2010: TRANSMITTER. DIRTY. 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), Nov 27, 2010: BUSHING. STIFF. 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), Nov 1, 2010: INDICATOR. STUCK. FUEL QUANTITY INDICATION STICKING.
- [SDR CA100701005](https://openairdocs.org/sdr/CA100701005), Jun 28, 2010: FILTER. DAMAGED. 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 SHOWE
- [SDR CA110209010](https://openairdocs.org/sdr/CA110209010), Apr 11, 2010: FUEL CONTROL. MALFUNCTIONED. (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 SU
- [SDR CA090413003](https://openairdocs.org/sdr/CA090413003), Mar 21, 2009: PUMP. UNSERVICEABLE. (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 BEE
- [SDR CA080115009](https://openairdocs.org/sdr/CA080115009), Jan 10, 2008: GROUND WIRE. FAILED. (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 SIMULA
- [SDR SSH2006F00000](https://openairdocs.org/sdr/SSH2006F00000), Nov 27, 2006: FUEL CONTROL. MALFUNCTIONED. 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 CONTI
- [SDR CA060920002](https://openairdocs.org/sdr/CA060920002), Sep 20, 2006: LINE. CRACKED. (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 W
- [SDR CA060920003](https://openairdocs.org/sdr/CA060920003), Sep 20, 2006: STARTER GEN. BROKEN. (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), May 3, 2006: FCU. FAILED. 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 W
- [SDR CA060313005](https://openairdocs.org/sdr/CA060313005), Mar 9, 2006: STARTER GEN. NOISY. VIBRATION ON START TO 60 PERCENT, AND STRANGE NOISE FROM THE ENGINE, FOUND BROKEN STARTER.
- [SDR CA051220006](https://openairdocs.org/sdr/CA051220006), Dec 6, 2005: SERVO. INOPERATIVE. (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. T
- [SDR CA051208007](https://openairdocs.org/sdr/CA051208007), Nov 11, 2005: B-NUT. CRACKED. (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 COMPLE
- [SDR CA050609003](https://openairdocs.org/sdr/CA050609003), Mar 18, 2005: LIMIT SWITCH. FAILED. (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), Mar 15, 2005: PUMP. LEAKING. (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 
- [SDR CA050312003](https://openairdocs.org/sdr/CA050312003), Feb 23, 2005: MAGNETIC SEAL. DISLODGED. (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. U
- [SDR CA050216009](https://openairdocs.org/sdr/CA050216009), Feb 16, 2005: SKIN. CRACKED. (CAN) CRACK FOUND ON VERTICAL UPPER FIN.
- [SDR CA040304003](https://openairdocs.org/sdr/CA040304003), Feb 25, 2004: O-RING. FAILED. (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 TEMPE
- [SDR CA040304004](https://openairdocs.org/sdr/CA040304004), Feb 25, 2004: BELT. UNBONDED. (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 HY
- [SDR CA040131001](https://openairdocs.org/sdr/CA040131001), Jan 30, 2004: DRIVE BELT. BROKEN. (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 T
- [SDR CA031015020](https://openairdocs.org/sdr/CA031015020), Oct 13, 2003: SPACER. BROKEN. (CAN) SENDER REMOVED FOR CLEANING TANK, AND NOTICED SEVERAL BRIDGE SPACERS HAD EITHER BROKEN OR LOOSE RIVETS.
- [SDR 2003FA0000772](https://openairdocs.org/sdr/2003FA0000772), Jul 24, 2003: DIFFUSER. MISOVERHAULED. 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 ENG
- [SDR CA030530010](https://openairdocs.org/sdr/CA030530010), May 19, 2003: FUEL CONTROL. FAILED. (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 

All 75: https://openairdocs.org/engine/honeywell-lts101-600a-3/reports.md

## PMA parts (OpenAirDocs) (194, first 50)

Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this engine model on its data sheet, so check the FAA record before relying on it. Newest first.

- [4-131-010-30](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID192455809320241018160209.0001): Liner Assy, Combustion Chamber. Honeywell International Inc. · PMA PQ1222NM · Replaces 4-131-010-30 · Jul 2, 2024
- [4-111-015-19](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168494359020241018160209.0001): Disk – First Turbine Rotor. Honeywell International Inc. · PMA PQ1222NM · Replaces 4-111-015-19 · Jul 2, 2024
- [4-111-058-06](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID150699376320241018160209.0001): Blade, Turbine Rotor – Stage 1 – Low Flow. Honeywell International Inc. · PMA PQ1222NM · Replaces 4-111-058-06 · Jul 2, 2024
- [4-141-290-30](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID135990764120241018160210.0001): Turbine Rotor. Honeywell International Inc. · PMA PQ1222NM · Replaces 4-141-290-30 · Jul 2, 2024
- [4-111-062-06](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132122400520241018160209.0001): Disk, Rotor – HP Turbine. Honeywell International Inc. · PMA PQ1222NM · Replaces 4-111-062-06 · Jul 2, 2024
- [4-131-070-04](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID130507704220241018160210.0001): Curl, Comb Chamber Assy. Honeywell International Inc. · PMA PQ1222NM · Replaces 4-131-070-04 · Jul 2, 2024
- [4-111-014-65](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID118223391920241018160208.0001): Blade, Turbine Rotor, Turbine Engine. Honeywell International Inc. · PMA PQ1222NM · Replaces 4-111-014-65 · Jul 2, 2024
- [82010546-001HT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165966587020230717173049.0001): Bearing, Ball (Drive). HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 82010546-001 · May 22, 2023
- [82010580-001HT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID159338547920230717173051.0001): Grease, Aircraft Bearing. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 82010580-001 · May 22, 2023
- [2539533HT](https://drs.faa.gov/browse/excelExternalWindow/FDF710A0D9BAAADD8625855000632B9C.0001): Bearing, Sintered. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2539533 · Apr 30, 2019
- [951190HT](https://drs.faa.gov/browse/excelExternalWindow/FC8B8869AAFBA24A8625855000632D54.0001): Pin, Sraight, Headless. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 951190 · Apr 30, 2019
- [197498HT](https://drs.faa.gov/browse/excelExternalWindow/F58363F6C29A0E2C8625855000636674.0001): Nut, Self-Locking. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 197498 · Apr 30, 2019
- [2543791HT](https://drs.faa.gov/browse/excelExternalWindow/F497876A15FC19DE8625855000638525.0001): Nut, Plain. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2543791 · Apr 30, 2019
- [2543598HT](https://drs.faa.gov/browse/excelExternalWindow/ECA18564BCB7E7E0862585500063865B.0001): Bellows Assembly (Governor). HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2543598 · Apr 30, 2019
- [336132HT](https://drs.faa.gov/browse/excelExternalWindow/E07190E2A02F10498625855000636717.0001): Tapered Pin, Split. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 336132 · Apr 30, 2019
- [2537184HT](https://drs.faa.gov/browse/excelExternalWindow/CF0C0BE63149DF618625855000638483.0001): Split Head Ring. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2537184 · Apr 30, 2019
- [2520561HT](https://drs.faa.gov/browse/excelExternalWindow/C93D07A85055A49E86258550006358AA.0001): Roller. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2520561 · Apr 30, 2019
- [2522105HT](https://drs.faa.gov/browse/excelExternalWindow/C831F72FFA3592EE8625855000633FF3.0001): Spacer. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2522105 · Apr 30, 2019
- [2543133HT](https://drs.faa.gov/browse/excelExternalWindow/C1075D8C43C8BBEE8625855000632CB1.0001): Cover Assembly. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2543133 · Apr 30, 2019
- [2523475HT](https://drs.faa.gov/browse/excelExternalWindow/C0E2E0F3CEAF58978625855000632DF6.0001): Gasket. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2523475 · Apr 30, 2019
- [2522102HT](https://drs.faa.gov/browse/excelExternalWindow/BE78A04D762789BA8625855000635942.0001): Pin, Straight, Headless. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2522102 · Apr 30, 2019
- [2523280HT](https://drs.faa.gov/browse/excelExternalWindow/BD2D6F5C8ACE954186258550006329A7.0001): Seat, Valve. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2523280 · Apr 30, 2019
- [2537508HT](https://drs.faa.gov/browse/excelExternalWindow/AB6226D24673A7D586258550006330BA.0001): Washer, Spring Tension. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2537508 · Apr 30, 2019
- [2523237HT](https://drs.faa.gov/browse/excelExternalWindow/A3761C3D79364D138625855000631D0C.0001): Bearing, Ball. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2523237 · Apr 30, 2019
- [2529242HT](https://drs.faa.gov/browse/excelExternalWindow/A0D34607F558EA0D862585500063302A.0001): Spring, Helical, Extension. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2529242 · Apr 30, 2019
- [2520488HT](https://drs.faa.gov/browse/excelExternalWindow/9CC32778DD3467368625855000635816.0001): Gasket. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2520488 · Apr 30, 2019
- [2538982HT](https://drs.faa.gov/browse/excelExternalWindow/9C95C51F6250D76586258550006343F2.0001): Nut. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2538982 · Apr 30, 2019
- [2525104HT](https://drs.faa.gov/browse/excelExternalWindow/984FA7DADBC0CFED8625855000632EF8.0001): Gasket. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2525104 · Apr 30, 2019
- [2520569HT](https://drs.faa.gov/browse/excelExternalWindow/9432CA88F2F1B9128625855000633EBF.0001): Bushing. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2520569 · Apr 30, 2019
- [2543734HT](https://drs.faa.gov/browse/excelExternalWindow/8B394A535BB0AE8E862585500062E3A5.0001): Bearing, Ball. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2543734 · Apr 30, 2019
- [2523282HT](https://drs.faa.gov/browse/excelExternalWindow/889B68627F1BF6D78625855000632A53.0001): Seat, Valve. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2523282 · Apr 30, 2019
- [2523242HT](https://drs.faa.gov/browse/excelExternalWindow/7299489DDD08CEDB8625855000634089.0001): Spacer. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2523242 · Apr 30, 2019
- [2520503HT](https://drs.faa.gov/browse/excelExternalWindow/6FF55BB83A1236CA8625855000631AD3.0001): Bearing, Ball. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2520503 · Apr 30, 2019
- [366783HT](https://drs.faa.gov/browse/excelExternalWindow/6BDB9F5E1EB61600862585500063679B.0001): Washer, Crush. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 366783 · Apr 30, 2019
- [2543226HT](https://drs.faa.gov/browse/excelExternalWindow/5A59E752DA8E60A98625855000632C18.0001): Cover Assembly. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2543226 · Apr 30, 2019
- [2523106HT](https://drs.faa.gov/browse/excelExternalWindow/4CC17275E02B523986258550006359D3.0001): Screen. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2523106 · Apr 30, 2019
- [2539179HT](https://drs.faa.gov/browse/excelExternalWindow/4C489B323A9992148625855000632AF7.0001): Bearing, Sintered. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2539179 · Apr 30, 2019
- [2523549HT](https://drs.faa.gov/browse/excelExternalWindow/45FC85266F9461F58625855000632E87.0001): Tube. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2523549 · Apr 30, 2019
- [2543792HT](https://drs.faa.gov/browse/excelExternalWindow/457DF2F181776F0486258550006385AC.0001): Insert Assembly, Carboloy. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2543792 · Apr 30, 2019
- [2537677HT](https://drs.faa.gov/browse/excelExternalWindow/40BC85624A10FBDE8625855000633134.0001): Pin, Straight, Headless. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2537677 · Apr 30, 2019
- [2523333HT](https://drs.faa.gov/browse/excelExternalWindow/3F8DC35D3825035F862585500063411D.0001): Nut. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2523333 · Apr 30, 2019
- [2544028HT](https://drs.faa.gov/browse/excelExternalWindow/3B1E3F42228359F88625855000636835.0001): Ring, Damper, Bellows. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2544028 · Apr 30, 2019
- [2523240HT](https://drs.faa.gov/browse/excelExternalWindow/3999BB6F4232A600862585500063206A.0001): Packing, Preformed O Ring. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2523240 · Apr 30, 2019
- [2537747HT](https://drs.faa.gov/browse/excelExternalWindow/24F79C028AC52BA486258550006331C3.0001): Diaphragm, By-Pass Valve. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2537747 · Apr 30, 2019
- [2529153HT](https://drs.faa.gov/browse/excelExternalWindow/0D41BC0586E5BAF88625855000632F86.0001): Spring, Helical, Extension. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2529153 · Apr 30, 2019
- [2537678HT](https://drs.faa.gov/browse/excelExternalWindow/0B599622025D67ED86258550006342B5.0001): Screw. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2537678 · Apr 30, 2019
- [343698HT](https://drs.faa.gov/browse/excelExternalWindow/075870B02E230B5B862585500063359B.0001): Pin. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 343698 · Apr 30, 2019
- [116115A6](https://drs.faa.gov/browse/excelExternalWindow/61251AE719378D7786258489004290ED.0001): PUMP ASSEMBLY COMPLETE. Triumph Engine Control Systems, LLC · PMA PQ0108NE · Replaces 4-301-377-10 · Mar 20, 2019
- [116115A7](https://drs.faa.gov/browse/excelExternalWindow/530C058E13EB78008625848900429103.0001): PUMP ASSEMBLY COMPLETE. Triumph Engine Control Systems, LLC · PMA PQ0108NE · Replaces 4-301-377-13 · Mar 20, 2019
- [2522102HT](https://drs.faa.gov/browse/excelExternalWindow/F021B8411976F1BB86257F0F00815030.0001): Pin, Straight, Headless. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2522102 · Nov 22, 2015

All of them: https://openairdocs.org/engine/honeywell-lts101-600a-3/pma.md

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.