# Continental LTSIO-360-RB

- Type: Engine model (FAA registry)
- Registry code: 17304
- Manufacturer (registry): CONT MOTOR
- Model: LTSIO-360-RB
- Engine type: Reciprocating
- Power: 220 hp
- Data sheet: [TCDS E9CE](https://openairdocs.org/tcds/E9CE) (OpenAirDocs)
- Holder: Continental Aerospace Technologies, Inc.
- Installed in: 0 registered aircraft
- Page: https://openairdocs.org/engine/continental-ltsio-360-rb

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 2023-09-09](https://openairdocs.org/ad/2023-09-09): Exhaust Turbine System (Recip) · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 292 more. Effective Jul 17, 2023
- [AD 2023-05-16](https://openairdocs.org/ad/2023-05-16): Reciprocating Engine Power Section · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-H and 147 more. Effective Mar 15, 2023
- [AD 2013-21-02](https://openairdocs.org/ad/2013-21-02): Turbochargers · Continental Motors LTSIO-360-RB, TSIO-360-MB, TSIO-360-RB and 2 more. Effective Nov 13, 2013
- [AD 2012-03-06](https://openairdocs.org/ad/2012-03-06): Fuel servo diaphragm · Continental Motors 6-260-A, 6-285-A, 6-285-B and 482 more. Effective Feb 24, 2012
- [AD 2011-13-03](https://openairdocs.org/ad/2011-13-03): Turbocharger Turbine · Lycoming Engines LTO-360-E1A6D, O-540-L3C5D, TIGO-541-E1A and 20 more. Effective Jul 13, 2011
- [AD 2010-11-04](https://openairdocs.org/ad/2010-11-04): Hydraulic lifters · Continental Motors FSO-470-A, GIO-470-A, GTSIO-520-C and 190 more. Effective Jun 16, 2010
- [AD 2009-02-03](https://openairdocs.org/ad/2009-02-03): Fuel injection servos · Lycoming Engines AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 261 more. Effective Feb 9, 2009
- [AD 2000-23-21](https://openairdocs.org/ad/2000-23-21): Crankshaft · Continental Motors IO-360-A, IO-360-AB, IO-360-B and 164 more. Effective Dec 12, 2000
- [AD 97-26-17](https://openairdocs.org/ad/97-26-17): Crankshaft · Continental Motors IO-360-A, IO-360-AB, IO-360-B and 90 more. Effective Jan 23, 1998
- [AD 93-10-02](https://openairdocs.org/ad/93-10-02): Missing Cylinder Valve Retainer Key · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 180 more. Effective Aug 12, 1993
- [AD 92-04-09](https://openairdocs.org/ad/92-04-09): Rocker Shaft Hold Down Stud · Continental Motors IO-360-A, IO-360-AB, IO-360-B and 41 more. Effective Jun 22, 1993
- [AD 91-19-03](https://openairdocs.org/ad/91-19-03): Oil Filter · Continental Motors 6-285-A, 6-285-B, 6-285-BA and 169 more. Effective Sep 29, 1991

Historical (superseded or no longer in force):

- [AD 2023-04-08](https://openairdocs.org/ad/2023-04-08) (historical): Reciprocating Engine Power Section · Continental Aerospace Technologies GTSIO-520-C, GTSIO-520-D, GTSIO-520-H and 141 more. Effective Feb 23, 2023
- [AD 2009-24-52](https://openairdocs.org/ad/2009-24-52) (historical): Hydraulic lifters · Continental Motors FSO-470-A, GIO-470-A, GTSIO-520-C and 192 more
- [AD 2009-24-51](https://openairdocs.org/ad/2009-24-51) (historical): Hydraulic lifters · Teledyne Continental Motors FSO-470-A, GIO-470-A, GTSIO-520-C and 156 more
- [AD 2000-08-51](https://openairdocs.org/ad/2000-08-51) (historical): Crankshaft · Teledyne Continental Motors IO-360-A, IO-360-AB, IO-360-B and 158 more

## Information bulletins (advisory) (6)

- [SAIB NE-20-05](https://openairdocs.org/saib/NE-20-05): POWERPLANT - Engine Camshaft Gear Tooth Fracture. Issued Apr 6, 2020
- [SAIB NE-16-13](https://openairdocs.org/saib/NE-16-13): Powerplant - Prohibited use of sealant. Issued Mar 8, 2016
- [SAIB NE-13-15](https://openairdocs.org/saib/NE-13-15): Engine Controls: Continental Motors, Inc. (CMI) Throttle and Mixture Control Levers. Issued Feb 8, 2013
- [SAIB NE-13-04](https://openairdocs.org/saib/NE-13-04): Continental Motors, Inc. (CMI) Connecting Rod Piston Pin Bushing Inspection. Issued Oct 31, 2012
- [SAIB NE-10-09](https://openairdocs.org/saib/NE-10-09): Reciprocating Engine Power Section: Hydraulic Valve Lifters. Issued Nov 20, 2009
- [SAIB NE-09-04](https://openairdocs.org/saib/NE-09-04): Fuel Control/Reciprocating Engines. Issued Jan 10, 2009

## Registered aircraft

None registered with this engine model now.

## NTSB investigations

None matched to aircraft with this engine model.

## 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.

- [Incident 20120710018659I](https://openairdocs.org/incident/20120710018659I), Jul 10, 2012: Piper Aircraft Inc PA-34-220T (N4442Y), Rome, NY, Minor damage. Pilot departed rochester, NY (roc) for Rome, NY at approximately 0700 LCL time. The part 91 flight was made in VFR conditions. Wx at the destination was VFR…

## Service difficulty reports (30)

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

- [SDR 2016FA0000554](https://openairdocs.org/sdr/2016FA0000554), Nov 4, 2016: BOLT. NOT REPORTED.  DURING 100 HOUR CHECK OF THE AIRPLANE (G.LANDING GEAR GROUP, POINT 36) WE DISCOVERED THAT BOLT, PN 400-672 (SECTION IX, CONTROL SYSTEM GROUP, FIGURE NR 63, IND
- [SDR AU510002135](https://openairdocs.org/sdr/AU510002135), Dec 12, 2005: PUMP. CONTAMINATED. RT ENGINE DRIVEN FUEL PUMP CONTAMINATED AND WORN INTERNALLY. SUSPECT CAUSED BY CONTAMINATION FROM ELECTRIC FUEL PUMP VANES AND/OR BRUSH MATERIAL.
- [SDR AU510002136](https://openairdocs.org/sdr/AU510002136), Dec 12, 2005: PUMP. CONTAMINATED. RT ENGINE DRIVEN FUEL PUMP CONTAMINATED AND WORN INTERNALLY. SUSPECT CAUSED BY CONTAMINATION FROM ELECTRIC FUEL PUMP VANES AND/OR BRUSH MATERIAL.
- [SDR AU510002141](https://openairdocs.org/sdr/AU510002141), Dec 12, 2005: PUMP. CONTAMINATED. RT ENGINE DRIVEN FUEL PUMP CONTAMINATED AND WORN INTERNALLY. SUSPECT CAUSED BY CONTAMINATION FROM ELECTRIC FUEL PUMP VANES AND/OR BRUSH MATERIAL.
- [SDR AUS20040254](https://openairdocs.org/sdr/AUS20040254), Apr 1, 2004: SERVO. CONTAMINATED. (AUS) RT ENGINE FCU REGULATOR AIR SECTION CONTAMINATED WITH OIL.
- [SDR 2002FA0001225](https://openairdocs.org/sdr/2002FA0001225), Oct 12, 2002: MAGNETO. INOPERATIVE. WHILE TRAINING, A/C SIMULATED ZERO THRUST SINGLE ENGINE APPROACH. WHEN POWER WAS REAPPLIED, ENGINE WAS FOUND DEAD AND WOULD NOT RESPOND TO ANY INPUTS FOUND IN E
- [SDR 2002F00934](https://openairdocs.org/sdr/2002F00934), Oct 1, 2002: FLANGE. FAILED. THE ATTACHMENT FLANGE OF THE INDUCTION MANIFOLD (NR2 CYLINDER) FAILED CAUSING ROUGH RUNNING OF THE ENGINE.
- [SDR AUS20020509](https://openairdocs.org/sdr/AUS20020509), May 23, 2002: WASHER. UNLOCKED. (AUS) RT ENGINE SCAVENGE PUMP COVER BOLT TAB WASHERS WERE NOT LOCKED. THE BOLTS WERE TIGHT. AREA HAD NOT BEEN DISTURBED SINCE FACTORY ASSEMBLY.
- [SDR 20010425CW003](https://openairdocs.org/sdr/20010425CW003), Apr 5, 2001: PISTON. STUCK. THE CONTROLLER PISTON STICK IN. A SPLIT IN POWER SETTING IN FLIGHT AND ON THE GROUND CONTROLLER REPLACED.
- [SDR 20010411CW012](https://openairdocs.org/sdr/20010411CW012), Feb 6, 2001: SERVO. INOPERATIVE. COULD NOT ADJUST OVERLY RIGHT MIXTURE. SENT FOR FACTORY SERVICE. INSTALLED ON AIRCRAFT STILL COULD NOT ADJUST. SENT BACK TO FACTORY FOR REPAIRS. NOTE THESE UNIT
- [SDR 20001102SH002](https://openairdocs.org/sdr/20001102SH002), Oct 12, 2000: CONTROLLER. STUCK. THE CONTROLLER PISTON STICK IN. A SPLIT IN POWER SETTING IN-FLIGHT AND ON THE GROUND. CONTROLLER REPLACED. (X)
- [SDR 20001102SH003](https://openairdocs.org/sdr/20001102SH003), Oct 11, 2000: SERVO. INOPERATIVE. UNABLE TO ADJUST MIXTURE AND IDLE WILL NOT STAY SET. (X)
- [SDR 20001019SH017](https://openairdocs.org/sdr/20001019SH017), Sep 21, 2000: SERVO. MALFUNCTIONED. IN-FLIGHT, WHEN MIXTURE WAS LEANED TO CRUISE SETTING AT ABOUT 9 GALLON/HOUR, THE MIXTURE WENT UP TO 3 GALLONS PER HOUR. SERVO REMOVED AND A NEW ONE INSTALLED IA
- [SDR 20001017SH009](https://openairdocs.org/sdr/20001017SH009), Sep 20, 2000: CONTROLLER. MALADJUSTMENT. THE CONTROLLER PISTON STICK IN. A SPLIT IN POWER SETTING IN-FLIGHT AND ON THE GROUND. CONTROLLER REPLACED. (X)
- [SDR 20001017SH020](https://openairdocs.org/sdr/20001017SH020), Sep 15, 2000: SERVO. FAILED. ENGINE DIED AT IDLE, UNABLE TO ADJUST MIXTURE. (X)
- [SDR 20001017SH019](https://openairdocs.org/sdr/20001017SH019), Sep 8, 2000: CONTROLLER. STUCK. THE CONTROLLER PISTON STICK IN. A SPLIT IN POWER SETING IN-FLIGHT AND ON THE GROUND. CONTROLLER REPLACED. (X)
- [SDR 20001019SH021](https://openairdocs.org/sdr/20001019SH021), Sep 8, 2000: CONTROLLER. STUCK. THE CONTROLLER PISTON STICK IN. A SPLIT IN POWER SETTING IN-FLIGHT AND ON THE GROUND. CONTROLLER REPLACED. (X)
- [SDR 20000913SH030](https://openairdocs.org/sdr/20000913SH030), Aug 30, 2000: SERVO. INOPERATIVE. UNABLE TO ADJUST FUEL FLOW AND IDLE MIXTURE. NEW SERVO. (X)
- [SDR 20000913SH031](https://openairdocs.org/sdr/20000913SH031), Aug 30, 2000: SERVO. MALFUNCTIONED. FUEL FLOW RIGHT ENGINE DROP 3 GALLONS PER HOUR. IN-FLIGHT, CHT AND TIT TEMP WENT HIGHER THAN THE OTHER ENGINE. ENGINE STARTED TO RUN ROUGH. ENGINE WAS SHUT DOWN
- [SDR 20000912SH025](https://openairdocs.org/sdr/20000912SH025), Aug 24, 2000: PUMP. FAILED. WITH TOP END FUEL PRESSURE SET IAW SPEC, AT IDLE, THE PUMP PRESSURE DROPS TO LOW. LESS THAN 25 PSI TO OPERATE FUEL SERVO AT IDLE. (X)
- [SDR 20000911SH033](https://openairdocs.org/sdr/20000911SH033), Aug 21, 2000: SERVO. FAULTY. ENGINE RUNNING RICH AND BLOWING BLACK SMOKE. UNABLE TO ADJUST MIXTURE. REMOVED AND SENT BACK TO TCM. (X)
- [SDR 20000925SH032](https://openairdocs.org/sdr/20000925SH032), Aug 17, 2000: SERVO. FAILED. THROTTLE HARD TO MOVE IN FLIGHT, SERVO REMOVED AND A NEW ONE INSTALLED. OVER FOUR POUNDS TO MOVE CONTROL. (X)
- [SDR 20000925SH033](https://openairdocs.org/sdr/20000925SH033), Aug 17, 2000: TUBE. CRACKED. NR 2 INTAKE TUBE ON RIGHT ENGINE CRACKED AT THE FLANGE WHERE IT MOUNTS TO THE CYLINDER . INTAKE TUBE WAS REPLACED AND TCM HAS BEEN INFORMED. (X)
- [SDR 20000925SH034](https://openairdocs.org/sdr/20000925SH034), Aug 17, 2000: TUBE. CRACKED. NR 6 INTAKE TUBE ON RIGHT ENGINE CRACKED AT THE FLANGE WHERE IT MOUNTS TO THE CYLINDER. INTAKE TUBE WAS REPLACED AND TCM HAS BEEN INFORMED. (X)
- [SDR 20000925SH039](https://openairdocs.org/sdr/20000925SH039), Aug 17, 2000: TUBE. CRACKED. THE PILOT REPORTED THE RIGHT ENGINE RUNNING ROUGH AND VIBRATION. THE ENGINE WAS SHUT DOWN AND A SAFE LANDING WAS MADE. AIRCRAFT WAS TAKEN TO MAINTENANCE AND INS
- [SDR 20000925SH040](https://openairdocs.org/sdr/20000925SH040), Aug 17, 2000: SERVO. FAILED. WHEN BOOST PUMP IS TURNED ON, FUEL FLOW DROPS, ENGINE RUNS ON THE LEAN SIDE. REPLACED SERVO. (X)
- [SDR 20000925SH036](https://openairdocs.org/sdr/20000925SH036), Aug 16, 2000: SERVO. FAILED. STIFF THROTTLE ARM, OVER 4 POUNDS TO MOVE CONTROL. (X)
- [SDR 20000919SH020](https://openairdocs.org/sdr/20000919SH020), Aug 8, 2000: PUMP. INOPERATIVE. IDLE PRESSURE WAS LOW AND UNABLE TO ADJUST HIGHER. (X)
- [SDR 20000919SH022](https://openairdocs.org/sdr/20000919SH022), Jul 27, 2000: PUMP. INOPERATIVE. IDLE PRESSURE WAS LOW AND UNABLE TO ADJUST HIGHER. (X)
- [SDR 20000912SH026](https://openairdocs.org/sdr/20000912SH026), Jul 25, 2000: PUMP. FAILED. IDLE PRESSURE WAS LOW AND UNABLE TO ADJUST HIGHER. PRESSURE WAS ALSO ERRATIC. (X)

## STCs that may be installed (OpenAirDocs) (15)

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 SE5583SW](https://openairdocs.org/stc/SE5583SW): Installation of fuel flow transducers (true-flow totalizer). Alcor LLC. Lists LTSIO-360 Series
- [STC SE04349CH](https://openairdocs.org/stc/SE04349CH): Installation of SureFly electronic ignition. SureFly Partners Ltd
- [STC SE02352CH](https://openairdocs.org/stc/SE02352CH): Installation of Challenger cleanable oil filter assembly. Challenger Aviation Products Inc
- [STC SE03309CH](https://openairdocs.org/stc/SE03309CH): Installation of Engine Preheat Kit, p/n TSP6CYL-2927-115 for 115 volt application. Hartzell Propeller Inc
- [STC SE04577CH](https://openairdocs.org/stc/SE04577CH): Install an electronic engine ignition system. Electroair Acquisition Corp
- [STC SE01966WI](https://openairdocs.org/stc/SE01966WI): Use of GAMI G100UL High Octane Unleaded Avgas in spark ignition piston aircraft engines. General Aviation Modifications Inc
- [STC SE02598CH](https://openairdocs.org/stc/SE02598CH): ONE ONLY STC; S/Ns 807783-R and 818341-R: Installation of AIR BP piston engine lubricating oil MDM100-QB2050AD-01 in Teledyne Continental Motors model TSIO-360-EB and LTSIO-360-EB horizontally opposed reciprocating engines. Air BP Lubricant
- [STC SE1780NM](https://openairdocs.org/stc/SE1780NM): Installation of Precise Flight standby vacuum system (SVS III). Precise Flight Inc
- [STC SE5743NM](https://openairdocs.org/stc/SE5743NM): Intallation of adapter for externally mounted oil filter. Aviation Development Corporation
- [STC SE09963SC](https://openairdocs.org/stc/SE09963SC): Installation of modified fuel injector nozzles. General Aviation Modifications, Inc
- [STC SE09513SC](https://openairdocs.org/stc/SE09513SC): Installation and usage of Exxon 20W50 Multigrade aircraft engine oil conforming to Exxon Oil Formulation WS-3013. Exxon Company USA. Lists LTSIO-360 Series
- [STC SE452NE](https://openairdocs.org/stc/SE452NE): Installation and usage of 'Mobil AV 1' aviation oil. Mobil Research & Development Corp. Lists LTSIO-360 Series
- [STC SE5879SW](https://openairdocs.org/stc/SE5879SW): Use of Phillips X/C II 20W-50 and25W-60 oil (OSS 55875) in all Avco reciprocating aircraft engines from 65 to 450 BHP. Phillips Petroleum Co. Lists LTSIO-360 Series
- [STC SE244NE](https://openairdocs.org/stc/SE244NE): Installation of Mattituck plasma flame sprayed cylinder barrels in Teledyne reciprocating engines. Mattituck Airbase, Inc. Lists LTSIO-360 Series
- [STC SE80NE](https://openairdocs.org/stc/SE80NE): Installation and usage of Bel-Ray synthetic aviation oil, Bel-Ray Aero 1, (nonsupercharged), horizontally opposed direct drive, aircraft engines of 350 hp. or less. Bel-Ray Company, Inc. Lists LTSIO-360 Series

## PMA parts (OpenAirDocs) (340, 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.

- [CF643093](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID164619900220251205185208.0001): Plug, Fuel Injection. PRECISION AIRMOTIVE LLC · PMA PQ0111NM · Replaces 643093 · Nov 26, 2025
- [CF646044](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID144974039620251205185208.0001): Screw, Idle Adjustment. PRECISION AIRMOTIVE LLC · PMA PQ0111NM · Replaces 646044 · Nov 26, 2025
- [CF521693-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID119767613520251205185207.0001): Ring, Internal Retaining. PRECISION AIRMOTIVE LLC · PMA PQ0111NM · Replaces 521693-3 · Nov 26, 2025
- [CF633298](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID113488815020251205185208.0001): Bushing, Idle Adjustment Spring. PRECISION AIRMOTIVE LLC · PMA PQ0111NM · Replaces 633298 · Nov 26, 2025
- [AE45BS-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID102351889020250908153032.0001): Brush Rack Assembly. Aerospace Turbine Rotables · PMA PQ3736CE · Replaces Prestolite Part Number ALU-1045BS · Aug 27, 2025
- [HSS](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID138215977120250923185924.0001): Engine Preheat Kit. Hartzell Propeller LLC · PMA PQ2040CE · Modification part · Aug 4, 2025
- [ES917](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID192492107120251216184202.0001): Impulse Coupling Spring. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces M917 · May 20, 2024
- [ES3019](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID190822192120251216184207.0001): Nut. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces M3019 · May 20, 2024
- [AM-3217](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID190801817120251216184156.0001): Wave Spring Washer. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces M-3217 · May 20, 2024
- [AM3611](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID190443277420251216184158.0001): Cam. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces M3611, M1522 · May 20, 2024
- [AM-3215](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID186810273420251216184147.0001): Brush Assy, Distributor. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces M3215 · May 20, 2024
- [AK-3975](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID182506865320251216184200.0001): Coil, Ignition. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces M3009, M3114, M3525, K3975, K3975 · May 20, 2024
- [ES3307](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID182005482120251216184214.0001): Gasket Pressure Kit. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces K3307 · May 20, 2024
- [AM-3020](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID175941851820251216184145.0001): Screw. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces M3020 · May 20, 2024
- [AM-2556](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID163056043620251216184154.0001): Cotter Pin. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces M2556 · May 20, 2024
- [ES3018](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID159518890720251216184203.0001): Clamp, Bearing Cap. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces M3018 · May 20, 2024
- [AM-3021](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID155587978420251216184143.0001): Screw Distributor Block. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces M3021 · May 20, 2024
- [ES3050](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID155180936920251216184217.0001): Impulse Coupling Assy.. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces M3050 · May 20, 2024
- [ES3180](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID154737934920251216184210.0001): Tube Fitting, Pressure. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces M3180 · May 20, 2024
- [ES3179](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID151924957720251216184210.0001): Vent Plug, Pressure. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces M3179 · May 20, 2024
- [AM-3485](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID151658177120251216184155.0001): Bearing Cap, Assembly. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces M3485 · May 20, 2024
- [AM-3006](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID146130218820251216184150.0001): Bearing. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces M3006 · May 20, 2024
- [ES3221](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID141393701020251216184227.0001): Screw. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces M3221 · May 20, 2024
- [ES3828](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139833534820251216184220.0001): Rotor Gear. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces K3828 · May 20, 2024
- [ES3172](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139528495120251216184209.0001): Washer. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces M3172 · May 20, 2024
- [AM2536](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID136517725820251216184151.0001): Woodruff Key. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces M2536 · May 20, 2024
- [A-13081K](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133214336820251216184146.0001): Contact Assembly. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces M3081 · May 20, 2024
- [AM-3062](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID128762119920251216184153.0001): Oil Seal. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces M3062 · May 20, 2024
- [ES3040](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID128685841620251216184204.0001): Coil Wedge. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces M3040 · May 20, 2024
- [AK-3984](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID123559578320251216184159.0001): Capacitor. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces M3183, K3984 · May 20, 2024
- [ES3823](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID116582067520251216184219.0001): Dist. Block & Gear Assy.. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces K3823 · May 20, 2024
- [ES3826](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID114076128220251216184206.0001): Spacer. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces M3826 · May 20, 2024
- [AB-382584](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178585965820251216184454.0001): Ignition ContactAssembly. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces Continental10-382584 · Dec 8, 2023
- [AB-92815-62](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID155604486920251216184503.0001): Retainer Ring. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces Continental10-92815-62 · Dec 8, 2023
- [AB-349326](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID151437189220251216184456.0001): Fish Paper. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces Continental10-349326 · Dec 8, 2023
- [AB-357173](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID150252836920251216184451.0001): Ignition ContactAssembly. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces Continental10-357173 · Dec 8, 2023
- [AB-90751-19](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145549394020251216184501.0001): Cotter Pin. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces Continental 10-90751-19 · Dec 8, 2023
- [AB-400623](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID144957477420251216184444.0001): Ball Bearing. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces Continental… · Dec 8, 2023
- [AB-382585](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID144246197920251216184453.0001): Ignition ContactAssembly. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces Continental10-382585 · Dec 8, 2023
- [AB-349263](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID143018368220251216184505.0001): O-Ring. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces Continental10-349263 · Dec 8, 2023
- [ES10-35936-7](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID134201689020251216184428.0001): Screw. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces Continental 10-35936-7 · Dec 8, 2023
- [AB-349511](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID128303981120251216184439.0001): Washer. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces Continental 10-349511 · Dec 8, 2023
- [AB-357174](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID127763958220251216184450.0001): Ignition ContactAssembly. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces Continental10-357174 · Dec 8, 2023
- [ES6320](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID197217995020240301172629.0001): Magneto. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces 6320 · Dec 1, 2023
- [ES649954](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID185377691220240301172643.0001): Gasket. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces 534750, 649954, M3411, SA534750 · Dec 1, 2023
- [ES1553](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID144237446020240301172642.0001): Screw, Harness Cap. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces M1553 · Dec 1, 2023
- [ES3328](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID130133017720240301172626.0001): Clamp Kit. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces M3328, K3328 · Dec 1, 2023
- [TA2927-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID143910433620231109131600.0001): Engine Preheat Kit. Hartzell Propeller LLC · PMA PQ2040CE · Modification part · Oct 31, 2023
- [TA2927-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID107190435020231109131559.0001): Engine Preheat Kit. Hartzell Propeller LLC · PMA PQ2040CE · Modification part · Oct 31, 2023
- [CF642709](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID164513059120230823124533.0001): Fuel Metering Cover Assembly. PRECISION AIRMOTIVE LLC · PMA PQ0111NM · Replaces 642709 · Aug 10, 2023

All of them: https://openairdocs.org/engine/continental-ltsio-360-rb/pma.md

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