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General| Bore | 5.125 in (130.2 mm) |
|---|---|
| Compression Ratio | 8.5:1 |
| Oil System | Wet sump |
| Cooling System | Air cooled |
| Displacement | 5.9 L |
| Fuel Type | 100LL Avgas |
Defines the manual's coverage of maintenance and installation for the L/TSIO-360-RB engine.
Lists essential related engine and accessory manuals for comprehensive information.
Explains the process for receiving and incorporating manual updates to ensure currency.
Categorizes and defines various types of service documents issued by TCM.
Breaks down the engine model designation to explain its components.
Clarifies terminology such as front, rear, and cylinder numbering for engine orientation.
Details key design characteristics of the L/TSIO-360-RB engine and its components.
States that operating limits and specifications apply to L/TSIO-360-RB engines and refers to other manuals.
Provides detailed technical specifications for the engine's cylinders, bore, stroke, and horsepower.
Lists critical operating parameters like RPM, manifold pressure, fuel, and oil limits for safe engine operation.
Specifies the essential tools and equipment a mechanic should have for engine servicing.
Lists companies that supply specialized tools, aiding in procurement.
Details specific tools or their equivalents required for engine overhaul and maintenance.
Provides a comprehensive list of aviation engine oils, including manufacturer and brand names.
Details preservative oils for temporary and indefinite storage applications.
Lists various lubricants and their suggested sources and applications on engine components.
Continues the list of lubricants, covering approved dispersant oils and specific thread lubricants.
Details sealants for engine components like crankcase parting faces and oil seals.
Lists sealants for pipe threads, ignition harness terminals, and stud holes.
Lists adhesives and primers for securing engine components like studs and flanges.
Covers miscellaneous items like high-temperature paint and lockwire for engine maintenance.
States that the engine does not contain components with mandatory replacement times per type certification.
Clarifies that specific inspection intervals are not required by type certification for this engine.
Mentions that ADs may specify other procedures not covered here.
Explains that changes to limitations require FAA approval and will be published in ADs.
Emphasizes compliance with manual requirements and aircraft/accessory manufacturer's needs for safety.
Specifies the engine overhaul period and notes it includes all accessories.
Outlines the requirement for an operational inspection before 50/100-hour inspections and starting procedures.
Provides a checklist for recording system data during operational inspections.
Lists critical operating parameters like RPM, manifold pressure, fuel, and oil limits for safe engine operation.
Details inspection procedures and maintenance information based on time intervals.
Covers 50-hour inspection procedures, including thorough inspection and operational run-up.
Addresses unscheduled maintenance events, including propeller strikes and foreign object damage.
Introduces the troubleshooting chart, explaining its purpose and structure.
Provides a guide for diagnosing engine problems, listing probable causes and corrective actions.
Emphasizes the need for technicians to have knowledge of safe procedures for engine installation.
Provides step-by-step instructions for unpacking the engine from both cardboard and wooden containers.
Details procedures for safely handling the engine after unpacking, emphasizing care due to its weight.
Outlines procedures for crating and shipping the engine in both cardboard and wooden containers.
Details steps for preparing the engine for service if installation is delayed after unpacking.
Provides instructions for installing the engine into the airframe and making necessary connections.
Describes the critical procedure for pre-lubricating engine parts before initial operation.
Covers preflight checks and run-up procedures, especially for new or overhauled engines.
Outlines procedures and considerations for conducting test flights after maintenance.
Provides instructions and cautions for servicing the engine oil system to maintain proper levels.
Lists approved ashless dispersant oils and approved mineral oil conforming to MIL-C-6529 Type II.
Specifies the minimum aviation fuel grade and warns against using incorrect fuel types.
Details how to inspect the oil filter element for signs of internal engine wear.
Explains the process and benefits of spectrographic oil analysis for monitoring engine wear.
Discusses the susceptibility of aircraft engines to corrosion and the owner's responsibility for precautions.
Explains how corrosive attack affects engines and the primary method to reduce it.
Provides detailed procedures for preparing the engine for temporary storage, including pre-flight and post-flight steps.
Details the preparation procedures for storing the engine indefinitely to prevent degradation.
Outlines the inspection schedule for cylinder dehydrator plugs and corrosion preventive mixture.
Provides comprehensive steps for returning a stored engine to service, including checks and test flights.
Emphasizes proper reinstallation, tagging of parts, and preventing foreign matter entry into the engine.
Explains the purpose and technique of lockwiring for securing parts and preventing loosening.
Details the installation and use of tab washers for securing bolts and nuts in TCM engines.
Describes the correct procedure for installing cotter pins to secure fasteners.
Provides guidance on the proper use of adhesives and sealants to prevent engine malfunction.
Outlines procedures for inspecting, preparing, and installing gaskets to prevent leaks.
Directs users to overhaul manuals for component removal and replacement, and to other sections for inspections.
Describes the components of the exhaust system and how they function during engine operation.
Provides a detailed explanation of the turbocharger's construction, lubrication, and operation.
Explains the function and operation of the exhaust by-pass valve (wastegate) in controlling turbocharger speed.
Details the VAPC's role in maintaining deck pressures for altitude compensation and its connection to the wastegate.
Describes how pressurized oil is supplied to and returned from the turbocharger.
Outlines 50-hour and 100-hour inspection procedures for the exhaust system and its components.
Provides a chart for diagnosing common exhaust system problems, their causes, and corrections.
Covers maintenance for exhaust system components, including collector, turbochargers, and wastegate.
Describes the Slick 6224 Series pressurized magnetos used for engine ignition.
Explains the magneto drive assembly and its components housed within the accessory case.
Outlines 50-hour and 100-hour inspection procedures for the ignition system, including magneto checks.
Provides a troubleshooting guide for ignition system failures, covering causes and corrections.
Covers maintenance for harness assemblies, magnetos, and magneto drive assemblies.
Details procedures for removing, cleaning, gapping, and installing spark plugs.
Provides a step-by-step procedure for correctly timing the magnetos to the engine.
Outlines instructions for preparing and installing the ignition harness assemblies.
Describes the overall fuel system, its components, and how fuel flows from the pump to the injectors.
Details the fuel pump, its operation, relief valve, and check valve functions.
Outlines 50-hour and 100-hour inspection procedures for the fuel servo and injection system components.
Provides a chart for diagnosing fuel system issues, including probable causes and corrective actions.
Covers maintenance procedures for the fuel servo, manifold valve, and fuel injection nozzles.
Explains the components of the induction system and the flow of compressed air to the cylinders.
Describes the overboost valve, its components, and its function in preventing excessive deck pressure.
Outlines 50-hour and 100-hour inspection procedures for the induction manifold and related components.
Provides a chart for diagnosing induction system problems, including causes and corrections.
Covers maintenance for induction system components and connections.
Mentions the engine's use of a mounting kit for customer-supplied AC compressors.
Details the compressor mounting kit, accessory drive adapter, and mounting brackets.
Outlines 50-hour inspection procedures for the compressor bracket assembly and drive components.
Refers users to the airframe manufacturer's instructions for troubleshooting the AC system.
Covers maintenance for compressor mounting kit components and drive belts.
Explains the provision for mounting a belt-driven alternator and its function in powering the aircraft.
Refers to TCM Form No. X30531-3 for detailed descriptions of TCM alternators.
Outlines 50-hour and 100-hour inspection procedures for the alternator and its mounting hardware.
Refers users to airframe manufacturer instructions for troubleshooting the charging system.
Covers maintenance and repair of TCM alternators and drive belt inspection.
Describes the electric starter motor, right-angle drive adapter, and their components.
Explains the starter adapter assembly, worm drive, and clutch mechanism.
Outlines 50-hour and 100-hour inspection procedures for the starter and adapter.
Provides a chart for diagnosing starting system issues, including probable causes and corrections.
Covers maintenance and repair procedures for the starter motor and starter adapter.
Describes the accessory case as an aluminum casting attached to the rear of the crankcase.
Explains accessory locations, mounting bosses, and the internal machining for oil pump gears.
Outlines 50-hour and 100-hour inspection procedures for accessories, gaskets, and studs on the accessory case.
Provides a chart for diagnosing accessory case oil loss and loose accessory issues.
Covers maintenance for the accessory case, including gasket replacement, studs, engine mounts, and separation.
Explains the engine oil supply path from the sump, through the pump, cooler, and galleries.
Details the oil pump, its components, and how it regulates oil pressure.
Describes the oil cooler and oil temperature control valve operation.
Outlines 50-hour inspection procedures for the oil sump, drain plug, and oil filter adapter.
Provides a chart for diagnosing lubrication system issues like oil leaks, consumption, and temperature.
Covers maintenance for the oil pump, oil filter adapter, oil filter, oil sump, and oil cooler.
Explains how cylinder cooling is achieved through airflow directed by cowling and baffles.
Describes the cylinder assembly, including the head, barrel, valves, and rocker arms.
Details the piston assembly, including rings, pin, and oil scraper.
Describes the hydraulic tappet assembly and its function in valve train operation.
Outlines 50-hour and 100-hour inspection procedures for cylinder heads, barrels, and related components.
Explains the use of the Master Orifice Tool for calibrating compression testing equipment.
Provides procedures for conducting cylinder leakage tests, including static and dynamic seal checks.
Offers a troubleshooting guide for issues identified during cylinder compression tests.
Provides a chart for diagnosing cylinder assembly problems like rough idling and high head temperature.
Lists service limits for cylinder and head assembly components, including bore, roughness, and valve seats.
Continues listing service limits for pistons, rings, pins, and valve train components.
Covers single cylinder reassembly, reinstallation, and hydraulic valve tappet maintenance.
Describes the crankcase's function in providing enclosure and support for internal engine parts.
Explains the crankcase's construction from two aluminum castings and its features like bearing saddles and tappet guides.
Outlines 50-hour and 100-hour inspection procedures for the crankcase, focusing on cracks.
Provides a chart for diagnosing crankcase issues like oil loss and excessive pressure.
Covers maintenance for the crankcase, including gasket replacement, studs, engine mounts, and separation.
Explains how torque is transmitted from the starter to the crankshaft and how other components are driven.
Outlines 50-hour and 100-hour inspection procedures for the crankshaft exit area and propeller installation.
Provides a chart for diagnosing engine drive train issues, focusing on oil loss.
Covers maintenance procedures for the crankshaft nose oil seal.
Details procedures for starting the engine after maintenance and performing an operational inspection.
Covers oil pressure adjustment and engine fuel system adjustments.
Details fuel system adjustments, including engine-driven fuel pump and idle mixture settings.
Provides steps for checking and adjusting engine idle speed and full power settings.
Outlines procedures and considerations for conducting test flights after engine adjustments.
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