1) Connections for instrumentation
General note
For notes regarding the electric rev counter consult the chap. Electric
system.
1.1)
Sensor for cylinder head temperature
See
General note
NOTE:
The temperature sensor (1) is directly fitted into cylinder head i.e. a direct
Technical data
temperature reading of the cylinder head material is taken.
Location
Connection
Grounding
Position temperature sensor:
Position
Cylinder head
2
3
Graph of sensor resistance over temperature:
Graph resistance
See
Effectivity: 912 Series
Edition 2/Rev. 0
BRP-Powertrain
INSTALLATION MANUAL
These connections to be established in accordance to
NOTICE
WARNUNG
certification and/or national specifications.
The certification for connections and connection lines
have to be conducted by the aircraft manufacturer to
the latest requirements like FAR and EASA.
Fig. 1.
A direct reading of the coolant temperature is not provided
for.
In the cylinder head of the cylinder 2 and 3
Spade terminal 6.3x0.8 DIN 46247
Via engine block
x-axis
-200.0 mm (-7.88 in)
-387.0 mm (-15.24 in) -241.0 mm (-9.49 in) -157.0 mm (-6.18 in)
Fig. 1.
The graph resistance over temperature has been de-
NOTICE
WARNUNG
termined, and is effective at the following conditions
only:
Ambient temperature: 20 °C (68 °F)
Tolerance: Max ±10 %
Axes
y-axis
241.0 mm (9.49 in)
-157.0 mm (-6.18 in)
76-00-00
z-axis
page 3
August 01/2012