BRP Rotax 915 i A Series Maintenance Manual page 60

Aircraft engine
Table of Contents

Advertisement

Points of Inspection
* no periodic maintenance (require-
ment after the first 25 hours of
operation)
Inspect temperature sensors and oil
pressure sensor for secure fit and
signs of wear.
Inspect all coolant hoses of the engine
for damage, including leakage, harden-
ing from heat, porosity, loose connec-
tions and secure attachment. Verify
routing is free of kinks and restrictions.
Carry out visual inspection of leakage
bore at the base of the water pump for
signs of leakage.
Inspect the expansion tank for damage
and abnormalities. Check coolant lev-
el, replenish as necessary. Inspect ra-
diator cap. Inspect protection rubber
on expansion tank base for correct fit.
Check steel fuel rails for any cracks
and/or scuffing marks.
Inspect the wiring (wiring harness) and
its connections for secure fit, damage
and signs of wear.
Check the airbox (GENUINE ROTAX®
part) incl. throttle body actuation. In-
spect sensors for tight fit, damage from
heat, damage and signs of wear.
Inspection of the GENUINE ROTAX®
exhaust system included in the stand-
ard delivery.
NOTE
If there is no standard/genuine ex-
haust system in use, the specifica-
tions of the manufacturer must be
observed.
05–20–00
Page 10
June 01 2019
BRP-Rotax
MAINTENANCE MANUAL LINE
Interval Operating hours
25*
50
100
X
X
X
X
X
X
X
X
X
X
X
X
X
Chapter
Reference
200
600
1000
12–20–00
Leakage
12–20–00
Leakage
12–20–00
Expansion
tank, radiator
12–20–00
Checking the
fuel lines
X
12–20–00
Check of
Signa-
ture
check
check
cap
wiring
Effectivity: 915 i A Series
Rev. 1

Advertisement

Table of Contents
loading

Table of Contents