8) Turbo Control Unit (Tcu) - Rotax 914 F Installation Manual

19.4.8) Turbo Control Unit (TCU)

Date
Page
1996 05 10
84
See Ill. 63.
voltage:
current input:
NOTE: At wrong polarity of the supply voltage both lamps will light
up.
operating temperature range:
storage temperature range:
weight:
dimensions and attachment: see sketch (Ill. 63)
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
instrument panel.
NOTE: Place of installation is limited by the length of the wiring
harness.
Support of the TCU on the 4 silent blocks 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 JAR has
to be conducted by the aircraft builder.
WARNING: Choose place of installation such, that operation is within the
specified temperature limits.
Install
914 F
12 V/DC min. 6 V
max. 18 V
see chapter 19.5.
min.
max. +70° C (+160° F)
min.
max. +70° C (+160° F)
approx. 425 g (1 lb)
Reference
- 25° C (-13° F)
- 40° C (-40° F)
Ill. 63
Modification-No.
- 0 -