Teledyne TSIO-360-RB, Maintenance Manual

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5-2
5-1 GENERAL
The scheduled inspection and maintenance described in this section must be complied with
in addition to all aircraft manufacturer and accessory manufacturer inspection and
maintenance requirements. This manual does not contain inspection or maintenance
requirements for supplemental type certificated components or systems. Such information
must be obtained from the supplemental type certificate holder.
Safety, efficiency and engine service life is predicated on compliance with the aircraft and
engine manufacturer's required instructions, inspections and maintenance schedule. The
owner/operator is primarily responsible for maintaining the engine in an airworthy condition,
including compliance with applicable Airworthiness Directives as specified in Part 39 of the
Federal Aviation Regulations (FAR); reference FAR 91.163.
NOTE . . . Engine operational inspection must be performed before and after any 50 or 100-
hour inspections or maintenance in accordance with "Operational Inspection" requirements
described in this manual (See Chapter Contents).
During engine 50 and 100-hour inspections, if engine components must be replaced, refer to
the applicable system maintenance chapter. Adjustment information will be found in the
individual system chapters of this section.
NOTE . . . The figures depicted in this section are for illustration purpose only. They are not
intended to be accurate detailed illustrations of any specific engine model, part or
equipment.
WARNING
When performing any inspection or maintenance, always treat the engine as if the
ignition switch was on. Do not stand or allow anyone else to stand within the arc of
the propeller. A loose or broken wire or a component malfunction could cause the
engine and propeller to rotate and/or the engine to start.
Engines operated in extremely humid locations or in exceptionally cold, damp climates or
coastal areas may require more frequent inspections. If the engine is operated in excess of
100 hours per year, the engine must be inspected at each 100-hour interval in addition to an
annual inspection.
5-2 OVERHAUL PERIODS
Engine Model Overhaul Period
L/TSI0-360-RB 1800 HOURS
NOTE . . . Overhaul periods for the engine include all engine accessories.
5-3 OPERATIONAL INSPECTION
An operational inspection must be performed prior to 50/100-hour inspections.
STARTING
Start engine using the starting procedure given in the airframe manufacturers Airplane Flight
Manual (AFM).