# Honeywell LTS101-650B-1

- Type: Engine model (FAA registry)
- Registry code: 33820
- Manufacturer (registry): HONEYWELL
- Model: LTS101-650B-1
- Engine type: Turbo-shaft
- Power: 550 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-lts101-650b-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

None registered with this engine model now.

## 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 (590, newest 50)

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

- [SDR QR9R20220617001](https://openairdocs.org/sdr/QR9R20220617001), Jun 17, 2022: ENGINE. SEPARATION. A PREFLIGHT INSPECTION DETECTED METAL AND A DATA PLATE ON THE ENGINE DECK. FURTHER INVESTIGATION NOTED SEPARATION OF EXHAUST FROM HOT END OF ENGINE #2 AND OTHER
- [SDR QR9R20220509002](https://openairdocs.org/sdr/QR9R20220509002), May 9, 2022: SENSOR. ILLUMINATED. DURING RUN-UP, OVSP FAIL LIGHT ILLUMINATED AND COULD NOT BE RESET. REMOVED AND REPLACED MAGNETIC SENSOR IAW 77-14-00-900-802-A01. T/F MOC COMPLETED IAW AMM 05-6
- [SDR QR9R20220428003](https://openairdocs.org/sdr/QR9R20220428003), Apr 28, 2022: INDICATOR. ILLUMINATED. #2 ENGINE FUEL FILTER CAUTION DISPLAYED WHILE TAXIING BACK TO PARKING PAD AFTER .8 HOURS OF HOVER WORK. AFTER PLACING THE BATTERY SWITCH ON, # 2 FUEL FILTER CAU
- [SDR QR9R20220422002](https://openairdocs.org/sdr/QR9R20220422002), Apr 22, 2022: SENSOR. INTERMITTENT. DURING FLIGHT, THE N2 RPM NEEDLE FOR THE #2 ENGINE ON THE TRIPLE TACH MOVED TO ZERO INTERMITTENTLY. AT AIRSPEEDS SLOWER THAN 40 KNOTS THE N2 RPM NEEDLE SYNCHRON
- [SDR QMLA2017050517047](https://openairdocs.org/sdr/QMLA2017050517047), May 5, 2017: LANDING LIGHT. ODOR. ON APPROACH, THE FLIGHT CREW SMELLED A LIGHT ODOR OF BURNING PLASTIC. ONCE ON THE GROUND, THE MECHANIC FOUND THE RETRACTABLE LANDING LIGHT TO BE THE SOURCE. THE
- [SDR HEER20170105759](https://openairdocs.org/sdr/HEER20170105759), Jan 5, 2017: GOVERNOR. MALFUNCTIONED. DURING CRUISE FLIGHT, SUDDEN LOSS OF RIGHT ENGINE POWER ACCOMPANIED WITH HELICOPTER YAW MOVEMENT AND NR 2 ENGINE LOW LIGHT. SIGNIFICANT SPLIT IN TORQUE, N2 AND 
- [SDR QMLA2015071715059](https://openairdocs.org/sdr/QMLA2015071715059), Jul 17, 2015: FIRE WARNING. FALSE ACTIVATION. THE NR 2 FIRE WARNING LIGHT WAS GLOWING VERY DIMLY. DID NOT NOTICE THE FIRE LIGHT WAS ON UNTIL THE OTHER COCKPIT LIGHTS WERE DIMMED FOR SHUTDOWN. THERE WAS NO E
- [SDR QMLA2015062615053](https://openairdocs.org/sdr/QMLA2015062615053), Jun 26, 2015: MOUNT FITTING. WORN. NUMBER 2 INBD FWD ENG MOUNT FITTING BUSHING WORN & ELONGATED, REQUIRING REPAIR SCHEME. REPAIR COMPLETED WITH FORM 337 DATED 07 07 2015.
- [SDR QMLA2015031915019](https://openairdocs.org/sdr/QMLA2015031915019), Mar 19, 2015: FIRE WARNING. FALSE ACTIVATION. NUMBER 2 ENG FIRE LIGHT ILLUMINATED IN FLIGHT WITH NO FIRE. ACFT LANDED WITHOUT INCIDENT. NR 2 ENG FIRE DETECTOR SYS INSPECTED & TESTED, NO FAULTS FOUND, COULD 
- [SDR QMLA2014072214088](https://openairdocs.org/sdr/QMLA2014072214088), Jul 25, 2014: SEAL. WORN. DURING DAILY AIRWORTHINESS CHECK, NOTICED EXCESSIVE NOISE & HORIZONTAL PLAY IN M/R MAST AT TRANSMISSION UPPER BEARING AREA WHEN SHAKING M/R BLADES. DURING INVES
- [SDR QMLA2013080113110](https://openairdocs.org/sdr/QMLA2013080113110), Aug 1, 2013: SWITCH. WORN. DURING LANDING , NOTICED NR 1 ENGINE FIRE LIGHT ILLUMINATED. AFTER LANDING AND SHUTDOWN NOTICED THE TEST SWITCH WAS NOT IN THE SPRING LOADED NEUTRAL POSITION. D
- [SDR QMLA2012052712088](https://openairdocs.org/sdr/QMLA2012052712088), May 27, 2012: ENGINE. MAKING METAL. DURING LANDING, THE NR 1 ENGINE CHIP LIGHT ILLUMINATED AS THE COLLECTIVE WAS PLACED FULL DOWN AFTER LANDING. EXCESS CHIPS WERE FOUND ON CHIP DETECTOR AND MX DET
- [SDR QMLA2012042112062](https://openairdocs.org/sdr/QMLA2012042112062), Apr 21, 2012: ENGINE. POWER LOSS. ON APPROACH, MASTER CAUTION LIGHT ILLUMINATED WITH A NR 1 ENGINE LOW LIGHT FOLLOWED BY A LARGE TORQUE SPLIT ( NR 1 LOW AT 20 PERCENT AND NR 2 HIGH AT 80 PERCENT
- [SDR CA111103006](https://openairdocs.org/sdr/CA111103006), Nov 1, 2011: SPLINE. BROKEN. (CAN) THE GOVERNOR WAS REMOVED FOR SPOOL BEARING CHANGE IAW SB LTS101-73-20-0262 & THE REPAIR SHOP DISCOVERED THE BROKEN DRIVE SPLINE. THIS WOULD NOT HAVE BEEN 
- [SDR QMLA2011093011097](https://openairdocs.org/sdr/QMLA2011093011097), Sep 30, 2011: ENGINE. POWER LOSS. THE PILOT REPORTED, AFTER PREFLIGHT AND CONFIRMATION CHECKS WERE CONDUCTED, LIFTED TO HOVER. USED THE ENGINE BEEP SWITCH TO SLIGHTLY INCREASE THE NR/N2 RPM TO 1
- [SDR RMXADMR334393](https://openairdocs.org/sdr/RMXADMR334393), Apr 14, 2011: SKIN. SCRATCHED. A .012" DEEP .3750" LONG SCRATCH WAS FOUND ON THE RT SIDE OF THE TAIL BOOM UNDER THE OMEGA STRINGER, 12 INCHES AFT OF THE CONNECTING FLANGE.
- [SDR QMLA2011012911017](https://openairdocs.org/sdr/QMLA2011012911017), Jan 29, 2011: CHIP DETECTOR. CONTAMINATED. NR 2 ENGINE CHIP LIGHT ILLUMINATED ALONG WITH THE MASTER CAUTION LIGHT. PILOT NOTED THAT THERE WERE NO N2 FLUCTUATIONS. AIR RETURNED AND ATTEMPTED A CHIP BURN W
- [SDR QMLA2011012411012](https://openairdocs.org/sdr/QMLA2011012411012), Jan 24, 2011: ACCESS DOOR. CHAFED. THE LT TRANSMISSION ACCESS COWLING CHAFED INTO THE MAIN TRANSMISSION DECK STRUCTURE AT AF STA 4239, WL 2753 AND BL 452.00L BEYOND MFG ACCEPTABLE LIMITS. THE APP
- [SDR QMLA2010102510072](https://openairdocs.org/sdr/QMLA2010102510072), Oct 25, 2010: FUEL SYS. CONTAMINATED. ACFT HAD UNDERGONE FUEL QTY INDICATOR CALIBRATION 2 DAYS PREVIOUSLY. PILOT ATTEMPTED TO START ENGINES, NEITHER ENGINE WOULD START. MX DETERMINED FUEL SYS HAD NO
- [SDR RMXA0305107013](https://openairdocs.org/sdr/RMXA0305107013), Mar 5, 2010: COMPENSATOR. UNSERVICEABLE. ENGINE WAS RETURNED TO IDLE POSITION & NOT SHUTDOWN IN FLIGHT. ON RETURN LEG OF FLIGHT, PILOT NOTICED TORQUE SPLITS BETWEEN ENGINES. ADJUSTED & NOTICED TORQUE S
- [SDR HEEA127331](https://openairdocs.org/sdr/HEEA127331), Feb 8, 2010: GOVERNOR. SPLIT. IN CRUISE FLIGHT, NR 2 ENG LOW MASTER CAUTION ILLUMINATED. VERFIED ENG LOW BY WIDE TORQUE SPLIT. LOWERED POWER AND COMPLIED WITH ENG LOW CHECKLIST. PERFORMED OE
- [SDR RMXA2009071401085](https://openairdocs.org/sdr/RMXA2009071401085), Jul 14, 2009: ICS BOX. DEFECTIVE. AT 3000FT AND CRUISE, PILOT AND CTR CONSOLE LIGHTS WENT OUT. WEATHER WAS CAVU WITH A HALF MOON. USED MAP LIGHT FOR ILLUMINATION AND RETURNED TO HOME BASE. ON SH
- [SDR RMXA2008121600575](https://openairdocs.org/sdr/RMXA2008121600575), Dec 15, 2008: CHIP DETECTOR. ACTIVATED. NR 1 ENGINE CHIP LIGHT ILLUMINATED AND COULD NOT BE EXTINGUISHED WITH ZAPPER. PILOT SECURED NR 1 ENGINE AND PERFORMED NIGHT SINGLE ENGINE RUN-ON LANDING TO JZI 
- [SDR RMXA2008121518093](https://openairdocs.org/sdr/RMXA2008121518093), Dec 15, 2008: CONNECTOR. DIRTY. THE NR 2 ENGINE FIRE WARNING LIGHT ILLUMINATED. ENGINES WERE OPERATING NORMALLY. FLIGHT NURSE AND PILOT NOTICED A SLIGHT BURNING SMELL. DISCHARGED THE NR 2 ENGI
- [SDR 705805272008](https://openairdocs.org/sdr/705805272008), May 27, 2008: ACTUATOR. FAILED. AFTER DROPPING A PATIENT OFF AT THE HOSPITAL, ON THE RETURN LEG TO THE AIRCRAFT HOME BASE, IN CRUISE FLT, THE NR 1 ENGINE FAILED TO FOLLOW COLLECTIVE MOVEMENTS 
- [SDR 04222008](https://openairdocs.org/sdr/04222008), Apr 22, 2008: SUPPORT BRACKET. LOOSE. DURING SCHEDULED INSPECTION, A TAIL ROTOR CONTROL TUBE SUPPORT MOUNT WAS FOUND LOOSE INSIDE THE TAILCONE DUE TO WORKING RIVETS.
- [SDR BAQA20080003](https://openairdocs.org/sdr/BAQA20080003), Apr 19, 2008: O-RING. DAMAGED. CRUISE FLIGHT, CLOSE TO FLIGHT DESTINATION, CREW SMELLED "STRANGE ODOR" IN CABIN/COCKPIT. PILOT TURNED OFF THE ENVIRONMENTAL CONTROL UNIT AND SMELL CEASED. INSP
- [SDR BAQA20080004](https://openairdocs.org/sdr/BAQA20080004), Apr 19, 2008: O-RING. DAMAGED. CRUISE FLIGHT, CLOSE TO FLIGHT DESTINATION, CREW SMELLED "STRANGE ODOR" IN CABIN/COCKPIT. PILOT TURNED OFF THE ENVIRONMENTAL CONTROL UNIT AND SMELL CEASED. INSP
- [SDR BAQA20080005](https://openairdocs.org/sdr/BAQA20080005), Apr 19, 2008: O-RING. DAMAGED. CRUISE FLIGHT, CLOSE TO FLIGHT DESTINATION, CREW SMELT "STRANGE ODOR" IN CABIN/COCKPIT. PILOT TURNED OFF THE ENVIRONMENTAL CONTROL UNIT (ECU) AND SMELL CEASED. 
- [SDR BAQA20080006](https://openairdocs.org/sdr/BAQA20080006), Apr 19, 2008: O-RING. DAMAGED. CRUISE FLIGHT, CLOSE TO FLIGHT DESTINATION, CREW SMELLED "STRANGE ODOR" IN CABIN/COCKPIT. PILOT TURNED OFF THE ENVIRONMENTAL CONTROL UNIT AND SMELL CEASED. INSP
- [SDR BAQA20080009](https://openairdocs.org/sdr/BAQA20080009), Apr 19, 2008: O-RING. BLOWN. CRUISE FLIGHT, CLOSE TO FLIGHT DESTINATION, CREW SMELLED "STRANGE ODOR" IN CABIN/COCKPIT. PILOT TURNED OFF THE ENVIRONMENTAL CONTROL UNIT AND SMELL CEASED. INSP
- [SDR BAQA200800003](https://openairdocs.org/sdr/BAQA200800003), Apr 19, 2008: O-RING. DAMAGED. CRUISE FLIGHT, CLOSE TO FLIGHT DESTINATION CREW SMELLED "STRANGE ODOR" IN CABIN/COCKPIT. PILOT TURNED OFF THE ENVIRONMENTAL CONTROL UNIT AND SMELL CEASED. INSPE
- [SDR BAQA20080021](https://openairdocs.org/sdr/BAQA20080021), Apr 19, 2008: O-RING. BLOWN. CRUISE FLIGHT, CLOSE TO FLIGHT DESTINATION, CREW SMELLED "STRANGE ODOR" IN CABIN/COCKPIT. PILOT TURNED OFF THE ENVIRONMENTAL CONTROL UNIT AND SMELL CEASED. INSP
- [SDR 712902242008](https://openairdocs.org/sdr/712902242008), Feb 24, 2008: WIRE. CHAFED. IMMEDIATELY AFTER TAKEOFF, AN ELECTRICAL BURNING ODOR WAS NOTED IN THE COCKPIT. SPAS (STICK POSITION AUGMENTATION SYSTEM) LIGHT ILLUMINATED AND SPAS CIRCUIT BRE
- [SDR 01282008](https://openairdocs.org/sdr/01282008), Jan 25, 2008: DOUBLER. CRACKED. DURING DAILY INSPECTION, A 3 INCH LONG CRACK WAS FOUND ON THE LT SIDE TAILBOOM DOUBLER.
- [SDR 717311162007](https://openairdocs.org/sdr/717311162007), Nov 16, 2007: COMPUTER. FAILED. DURING FLIGHT, YAW CSAS CAUTION LIGHT ILLUMINATED. DIVERTED LANDING FROM HELIPAD TO AIRPORT 4 MILES AWAY. COMPLETED APPROPRIATE EMERGENCY PROCEDURE IAW AFM.
- [SDR 711510292007](https://openairdocs.org/sdr/711510292007), Oct 29, 2007: POWER LEVER. DISLODGED. HELICOPTER STUCK SEVERAL GEESE. 1 PENETRATED THE WINDOW ON RT SIDE BEHIND THE SLIDING DOOR NEXT TO PARAMEDIC & LODGED ITSELF BETWEEN THE WALL & AIRFRAME. ANOTHE
- [SDR 10252007](https://openairdocs.org/sdr/10252007), Oct 24, 2007: SKIN. CRACKED. DURING DAILY INSPECTION, A 1 INCH LONG CRACK WAS DISCOVERED ON A TAIL BOOM SHEET METAL DOUBLER, LT SIDE, JUST AFT OF THE HORIZONTAL STABILIZER.
- [SDR 2758071607](https://openairdocs.org/sdr/2758071607), Jul 16, 2007: SKIN. CRACKED. 1 INCH LONG SKIN CRACK FOUND ON IB SIDE OF VERTICAL STABILIZER SKIN.
- [SDR 200706092204](https://openairdocs.org/sdr/200706092204), Jun 9, 2007: BEARING. BINDING. PILOT EXPERIENCED BINDING IN THE T/R CONTROLS. DIRT WAS FOUND IN T/R GRIP BEARINGS CAUSING BINDING IN CONTROL.
- [SDR 2007FA0000336](https://openairdocs.org/sdr/2007FA0000336), Apr 16, 2007: RADIO. SHORTED. WHILE SHUTTING DOWN AIRCRAFT THE CREW NOTED A WHIFF OF SMOKE AND ELECTRICAL SMELL IN THE COCKPIT. FOUND THE NR (2) COMM RADIO INTERNALLY SHORTED.
- [SDR BAQA20060007](https://openairdocs.org/sdr/BAQA20060007), Nov 15, 2006: FRAME. CRACKED. CRACK FOUND IN OVER HEAD FRAME. DETERMINED TO BE MINOR REPAIR. REPAIRED BY INSTALLING DOUBLERS IAW AC 43.13-1B MM.
- [SDR BAQA20060006](https://openairdocs.org/sdr/BAQA20060006), Nov 13, 2006: RETAINING NUT. LOOSE. POWER TURBINE WHEEL RETENTION NUT LOST TORQUE. DISCOVERED BY N2 FLUCTUATION ACCOMPANIED BY A CHIP LIGHT.
- [SDR 7110650](https://openairdocs.org/sdr/7110650), Jun 5, 2006: MANIFOLD. LEAKING. ON POST FLIGHT AFTER MISSION WAS COMPLETED, PILOT FOUND FUEL LEAKING FROM THE NR 2 ENGINE FUEL MANIFOLD.
- [SDR BAQA093911](https://openairdocs.org/sdr/BAQA093911), Mar 10, 2004: MODULATOR. INOPERATIVE. UNIT REMOVED FOR OVERHAUL. PART WAS INSTALLED ON ENG S/N LE45239, BUT ENGINE WAS ORIGINALLY INSTALLED ON A/C S/N 7068. INSTALLED ON 5/4/99 AT ENG TT 3407.8 AND 
- [SDR BAQA091292](https://openairdocs.org/sdr/BAQA091292), Dec 1, 2003: MANIFOLD. MALFUNCTIONED. ENGINE HARD TO LIGHT OFF. REMOVED FUEL MANIFOLD FROM ENGINE. REPLACED WITH SERVICEABLE UNIT. 12/10/03
- [SDR BAQA090586](https://openairdocs.org/sdr/BAQA090586), Oct 22, 2003: FUEL CONTROL. MALFUNCTIONED. ENGINE FLAME-OUT DURING OVERSPEED CHECKS. REPLACED WITH SERVICEABLE UNIT. 11/3/03
- [SDR BAQA089814](https://openairdocs.org/sdr/BAQA089814), Oct 7, 2003: TRANSDUCER. FLUCTUATES. ENGINE NR 2 TORQUE FLUCTUATIONS. REPLACED WITH SERVICEABLE UNIT.
- [SDR BAQA088826](https://openairdocs.org/sdr/BAQA088826), Sep 2, 2003: INDICATOR. ERRATIC. N1 INDICATOR GIVING ERRATIC INDICATIONS. REPLACED WITH SERVICEABLE UNIT.
- [SDR BAQA088340](https://openairdocs.org/sdr/BAQA088340), Aug 6, 2003: PUMP. LEAKING. OIL PUMP LEAKS FROM TOP AREA OF HOUSING. REPLACED WITH SERVICEABLE UNIT.

All 590: https://openairdocs.org/engine/honeywell-lts101-650b-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) (196, 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
- [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
- [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

All of them: https://openairdocs.org/engine/honeywell-lts101-650b-1/pma.md

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