THRUSH S2R – G10 Maintenance Manual page 34

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