THRUSH AIRCRAFT, INC – MODEL S2R-G10
AIRCRAFT MAINTENANCE MANUAL
C: ENGINE OIL SYSTEM (Continued)
Daily
50
hrs
100
hrs
400
hrs
4.
Check the chip detector for continuity using a
suitable ohmmeter. An open circuit condition,
which indicates no ferrous contamination at pole
tips, must exist.
X
5.
Inspect oil cooler for damage, cleanliness, leaks,
and security.
X
6.
Inspect oil cooler scoop inlet area to ensure good
airflow through cooler.
X
D. ENGINE FUEL SYSTEM
Daily
50
hrs
100
hrs
400
hrs
1. Check the fuel for presence of water. X X
2.
Check the fuel pump for security and fuel
leakage.
X
3.
Engine Fuel Filter – remove, inspect and replace
paper fuel filter element.
X
* NOTE *
On new aircraft, check the filter after each flight
until there is no evidence of contamination.
Check the filter after the first flight or ground run
when any upstream component is replaced.
4.
Check the fuel control unit for security, linkage
and pneumatic tubes.
X
5.
For improved hot section durability. It is
recommended that the fuel nozzle assemblies are
inspected and functional tested in accordance
with time limits set forth in the engines
appropriate maintenance manual.
X X
E. IGNITION SYSTEM
Daily
50
hrs
100
hrs
400
hrs
1.
Check the ignition exciter for security and
condition.
X
2.
Check the ignition cable for chafing, wear and
security.
X
3.
Check the spark igniters for cleanliness and
erosion. Perform an operational test..
X
Effective: 03/26/2010 Page 2-17
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