# Honeywell LTS101-750C-1

- Type: Engine model (FAA registry)
- Registry code: 33828
- Manufacturer (registry): HONEYWELL
- Model: LTS101-750C-1
- Engine type: Turbo-shaft
- Power: 684 hp
- Data sheet: [TCDS E5NE](https://openairdocs.org/tcds/E5NE) (OpenAirDocs)
- Holder: Intermountain Turbine Services Inc.
- Installed in: 1 registered aircraft
- Page: https://openairdocs.org/engine/honeywell-lts101-750c-1

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 2011-08-06](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 2001-22-07](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 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 95-26-01](https://openairdocs.org/ad/95-26-01): Power Turbine · Honeywell International LTS101-650B-1, LTS101-650C, LTS101-750B-1 and 1 more. Effective Apr 22, 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 95-08-14](https://openairdocs.org/ad/95-08-14): Electronic Overspeed Protection System · Honeywell International LTS101-650B-1, LTS101-650C-3, LTS101-650C-3A and 2 more. Effective May 9, 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 (1)

- [N4VE](https://openairdocs.org/aircraft/N4VE): [Greenway Avia Inc](https://openairdocs.org/faa-owner/GREENWAY%20AVIA%20INC), [Leesburg, FL](https://openairdocs.org/faa-place/FL/Leesburg), S/N 47142

## NTSB investigations

None matched to aircraft with this engine model.

## FAA accident and incident reports

None matched to aircraft with this engine model.

## Service difficulty reports (68, newest 50)

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

- [SDR CA190426021](https://openairdocs.org/sdr/CA190426021), Apr 26, 2019: ENGINE. 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 
- [SDR QMLA2014090514107](https://openairdocs.org/sdr/QMLA2014090514107), Sep 5, 2014: ENGINE. LEAKING. 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 T
- [SDR CA130314004](https://openairdocs.org/sdr/CA130314004), Mar 13, 2013: CASE. CRACKED. (CAN) TOP CASE RT INBD COLLECTIVE IDLER LUG FOUND CRACKED. BUSHING WORN BEYOND LIMIT. CASE REPLACED.
- [SDR QMLA2012092512159](https://openairdocs.org/sdr/QMLA2012092512159), Sep 25, 2012: LONGERON. CRACKED. 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), Mar 29, 2012: ACTUATOR. INOPERATIVE. 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 INSP
- [SDR QMLA2012032512036](https://openairdocs.org/sdr/QMLA2012032512036), Mar 25, 2012: UNKNOWN. SMOKE. DURING RUN-UP, BOTH ENGINES STARTED & GENERATORS PLACED IN "ON" POSITION FOLLOWING NORMAL START. WHILE PILOT WAS PLACING SYS & SWITCHES TO THE CHECKLIST, PARAME
- [SDR CA111130011](https://openairdocs.org/sdr/CA111130011), Nov 30, 2011: ARM. 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
- [SDR QMLA2011092111094](https://openairdocs.org/sdr/QMLA2011092111094), Sep 21, 2011: ENGINE. MAKING METAL. 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 T
- [SDR QMLA2011061511065](https://openairdocs.org/sdr/QMLA2011061511065), Jun 15, 2011: GEARBOX. MAKING METAL. 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 STRAI
- [SDR QMLA2010102510071](https://openairdocs.org/sdr/QMLA2010102510071), Oct 25, 2010: DISC. UNSERVICEABLE. DURING LIFT OFF, ROTORBRAKE WARNING LIGHTS ILLUMINATED, FOLLOWED BY TRANSMISSION CHIP LIGHTS AND TRANSMISSION OIL PRESSURE. CREW REPORTED SMELLING SOMETHING BUR
- [SDR 2010F00057](https://openairdocs.org/sdr/2010F00057), Mar 10, 2010: GEAR. FAILED. 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), Dec 8, 2008: SERVO. UNKNOWN. (CAN) SOLID RESISTANCE FELT WITH AFT CYCLIC MOVEMENT DURING OPERATIONS WITH FORCE TRIM ON & UTILIZING CYCLIC TRIM RELEASE SWITCH. ON FIRST OCCURRENCE RESISTANCE
- [SDR CA090127010](https://openairdocs.org/sdr/CA090127010), Nov 26, 2008: BRACKET. CRACKED. HIGH PRESSURE ENGINE FUEL FILTER BRACKET CRACKING AT TOP BOLT HOLE DUE TO HARMONIC VIBRATION, KNOWN PROBLEM.
- [SDR 200709152121](https://openairdocs.org/sdr/200709152121), Sep 15, 2007: FEEDER CABLE. SHORTED. CABLE SHORTED, CAUSING FALSE FIRE WARNING INDICATION.
- [SDR BAQA200700022](https://openairdocs.org/sdr/BAQA200700022), Jun 27, 2007: BLADE. LOOSE. 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
- [SDR BAQA200700020](https://openairdocs.org/sdr/BAQA200700020), Jun 25, 2007: BLADE. LOOSE. 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
- [SDR BAQA200700021](https://openairdocs.org/sdr/BAQA200700021), Jun 25, 2007: BLADE. LOOSE. 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
- [SDR 47540060306](https://openairdocs.org/sdr/47540060306), Jun 3, 2006: TUBE. CRACKED. 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), Dec 17, 2005: TRANSMITTER. FAILED. 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), Feb 22, 2005: FLEXURE. DELAMINATED. 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. LO
- [SDR 47518011705](https://openairdocs.org/sdr/47518011705), Jan 17, 2005: LINE. RUPTURED. 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 
- [SDR 047504123104](https://openairdocs.org/sdr/047504123104), Dec 31, 2004: SERVO. MALFUNCTIONED. 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 
- [SDR 47504123104](https://openairdocs.org/sdr/47504123104), Dec 31, 2004: SERVO. FAILED. 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 L
- [SDR 47567122504](https://openairdocs.org/sdr/47567122504), Dec 25, 2004: LINK. FAILED. 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
- [SDR CA041007009](https://openairdocs.org/sdr/CA041007009), Sep 29, 2004: SKIN. 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 S
- [SDR N406MA0204](https://openairdocs.org/sdr/N406MA0204), Feb 27, 2004: WIRE. CHAFED. 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 W
- [SDR N406MA](https://openairdocs.org/sdr/N406MA), Feb 18, 2004: DETECTOR. BROKEN. 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 T
- [SDR N431MA](https://openairdocs.org/sdr/N431MA), Feb 10, 2004: MOUNT. DEBONDED. ENROUTE TO THE HOSPITAL FOR PATIENT PICKUP. STRONG 2 PER REV VIBRATION EXPERIENCED. LANDED AT PSP AIRPORT. CONTACTED MAINTENANCE FOR REPAIRS. AFTER TROUBLESHOOT
- [SDR BAQA087531](https://openairdocs.org/sdr/BAQA087531), Jun 8, 2003: PUMP. FAILED. FUEL PUMP DOESN'T TURN FREELY. REPLACED WITH SERVICEABLE UNIT.
- [SDR BAQA087055](https://openairdocs.org/sdr/BAQA087055), Jun 8, 2003: PUMP. FAILED. FUEL PUMP WOULD NOT TURN. REPLACED WITH SERVICEABLE UNIT.
- [SDR BAQA085865](https://openairdocs.org/sdr/BAQA085865), Mar 31, 2003: MANIFOLD. CRACKED. CRACKED AND LEAKING FUEL AT 10 DEGREE CLOCK NOZZLE. HARD CARD ENCLOSED. REPLACED WITH SERVICEABLE UNIT.
- [SDR CA030228004](https://openairdocs.org/sdr/CA030228004), Feb 21, 2003: FITTING. 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.
- [SDR HEEA083048](https://openairdocs.org/sdr/HEEA083048), Jan 7, 2003: VALVE. STUCK. FUEL CONTROL VALVE IS STUCK IN THE NORMAL MODE.
- [SDR CA021001001](https://openairdocs.org/sdr/CA021001001), Jul 11, 2002: BRACKET. 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 
- [SDR CA020521004](https://openairdocs.org/sdr/CA020521004), Apr 11, 2002: FITTING. 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
- [SDR CA020228013](https://openairdocs.org/sdr/CA020228013), Feb 1, 2002: SLEEVE. 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 F
- [SDR CA020131002](https://openairdocs.org/sdr/CA020131002), Jan 18, 2002: FITTING. BROKEN. (CAN) VERTICAL LOWER FIN FITTING FOUND ATTACHMENT LUG BROKEN OFF ON A PRE FLIGHT.
- [SDR CA011116007](https://openairdocs.org/sdr/CA011116007), Sep 8, 2001: REGULATOR. 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 REM
- [SDR AU000375](https://openairdocs.org/sdr/AU000375), Feb 13, 2000: SPACER. 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 OUT
- [SDR 2000ZZZX752](https://openairdocs.org/sdr/2000ZZZX752), Oct 18, 1999: BEARING. CORRODED. BEARING HAD EXCESSIVE PITTING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
- [SDR 99ZZZX3021](https://openairdocs.org/sdr/99ZZZX3021), Jul 27, 1999: PY LINE. CRACKED. THIS PY AIR LINE CRACKED AND CAUSED SUDDEN DECELERATION. PILOT MADE NORMAL SINGLE ENGINE LANDING WITHIN PUBLISHED OEI LIMITATIONS. VIBRATIONS WERE RECORDED ON M
- [SDR 99ZZZX2879](https://openairdocs.org/sdr/99ZZZX2879), May 25, 1999: SHROUD. FLAKING. COATING FLAKING OFF OF IMPELLER SHROUD PREMATURELY. REF: MCN 69. REMOVED AND REPLACED.
- [SDR 99ZZZX1798](https://openairdocs.org/sdr/99ZZZX1798), Feb 25, 1999: BEARING. WORN. BEARING WORN BEYOND SERVICEABLE LIMITS. INSTALLED AT ASE GREER FACILITY. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
- [SDR 99ZZZX1259](https://openairdocs.org/sdr/99ZZZX1259), Nov 12, 1998: PUMP. LEAKING. FUEL PUMP LEAKING FUEL FROM OVERBOARD DRAIN. REMOVED AND REPLACED.
- [SDR 99ZZZX1280](https://openairdocs.org/sdr/99ZZZX1280), Sep 22, 1998: ROTOR ASSY. DAMAGED. SEALING PLATE IS SEPARATING FROM BLADES. REMOVED AND REPLACED.
- [SDR 99ZZZX902](https://openairdocs.org/sdr/99ZZZX902), Sep 22, 1998: HOUSING. CRACKED. HOUSING CRACKED AT 6 O'CLOCK STRUT. REMOVED AND REPLACED.
- [SDR 97ZZZX5218](https://openairdocs.org/sdr/97ZZZX5218), Dec 13, 1997: MANIFOLD. CRACKED. 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 I
- [SDR 97ZZZX4835](https://openairdocs.org/sdr/97ZZZX4835), Oct 11, 1997: TUBE. CRACKED. REPLACED CRACKED PY LINE AT FUEL CONTROL UNIT.
- [SDR 97ZZZX4093](https://openairdocs.org/sdr/97ZZZX4093), Aug 22, 1997: FUEL MANIFOLD. LEAKING. 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
- [SDR CA970722004](https://openairdocs.org/sdr/CA970722004), Jul 10, 1997: FUEL 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.

All 68: https://openairdocs.org/engine/honeywell-lts101-750c-1/reports.md

## STCs that may be installed (OpenAirDocs) (1)

Approved for this engine model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [STC SE934GL](https://openairdocs.org/stc/SE934GL): Installation of a fuel flow tranducer. Shadin Avionics

## PMA parts (OpenAirDocs) (185, 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
- [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
- [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
- [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
- [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
- [343698HT](https://drs.faa.gov/browse/excelExternalWindow/E8F990AC4967641486257F0F00814655.0001): Pin. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 343698 · Nov 22, 2015
- [2543226HT](https://drs.faa.gov/browse/excelExternalWindow/E7F8F0039537116E86257F0F00814368.0001): Cover Assembly. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2543226 · Nov 22, 2015
- [2529153HT](https://drs.faa.gov/browse/excelExternalWindow/DBC2BA2A75CF3A9F86257F0F00814464.0001): Spring, Helical, Extension. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2529153 · Nov 22, 2015
- [2539179HT](https://drs.faa.gov/browse/excelExternalWindow/DABF8276679DB56486257F0F00814311.0001): Bearing, Sintered. HYE-Tech Manufacturing LLC · PMA PQ2317NM · Replaces 2539179 · Nov 22, 2015

All of them: https://openairdocs.org/engine/honeywell-lts101-750c-1/pma.md

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