Effectivity: 914 Series
Edition 2 / Rev. 0
d04282
page 119
July 01/2008
BRP-Rotax
INSTALLATION MANUAL
▲ WARNING: All connections have to be established by the aircraft manufac-
turer in compliance with regulations such as FAR or EASA and
the effective wiring diagram (Fig. 69).
▲ WARNING: An essential point is according to regulations, that the fuel
pumps are connected on two completely independent power
supplies.
19.4.8) Turbo Control Unit (TCU)
See Fig. 80.
- voltage: 12 V/DC min. 6 V
max. 18 V
- current input: see section 19.5.
◆ NOTE: At wrong polarity of the supply voltage both lamps will light up.
- operating temperature range: min. - 25 °C (-13 °F)
max. +70 °C (+160 °F)
- storage temperature range: min. - 40 °C (-40 °F)
max. +70 °C (+160 °F)
- weight: approx. 425 g (1 lb)
- dimensions and attachment: see sketch (Fig. 80)
- place of installation:
▲ WARNING: Installation in the engine compartment is not permitted
since the TCU is not of a fire resistant construction.
A recommendable location is in the cockpit, below the instru-
ment panel.
The TCU has to be in an area were it is protected against
moisture.
◆ NOTE: Place of installation is limited by the length of the wiring
harness.
Support of the TCU on the 4 rubber shock mounts which ensures an
attachment free of vibrations.
▲ WARNING: If the standard attachment should not be utilized or changed,
certification to the latest requirements such as FAR or EASA
has to be conducted by the aircraft manufacturer
To Next Page
Loading...
Need help?
General
