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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
engines, 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.
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. The owner/operator is
responsible for assuring the engine meets the
conformity requirements as specified by the original
Type Certificate (TC) or any Supplemental Type
Certificate (STC) that may apply to modifications or
alterations accomplished after the issuance of the
original TC.
NOTE...
Engine operational inspection must be performed
before and after any 50 or 100-hour inspections or
maintenance
in
accordance
Inspection" requirements described in this Chapter.
During engine 50 and 100-hour inspections, if engine
components must be replaced or repaired, refer to the
applicable system maintenance chapter. Corrections
and adjustments will be found in the individual
system chapters of this section.
The
owner/operator
with
"Operational
When
performing
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 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
should be inspected at each 100-hour interval in
is
addition to an annual inspection.
OVERHAUL PERIOD
Engine Model
TSI0L-550-C
NOTE...
Overhaul periods for the engine include all engine
accessories.
OPERATIONAL INSPECTION
An operational inspection must be performed prior to
and after 50/100-hour inspections.
STARTING
Start engine using the starting procedure given in the
airframe manufacturers Airplane Flight Manual
(AFM).
Oil Pressure - Check, If no oil pressure is noted within
30 seconds, shut engine down and investigate.
Scheduled Maintenance
WARNING
any
inspection
Overhaul Period
2000 HOURS
or
1-3
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