Rotax 912 i Series Installation Manual page 18

NOTE:
Auxiliary equip-
ment tested
The following auxiliary equipment has been tested on ROTAX engine
type 912 i for safety and durability to the standards of aviation.
The furnishing of proof in accordance to the latest FAR or EASA has to be
conducted by the aircraft manufacturer.
- external alternator
- oil cooler with connections
- coolant radiator
- coolant overflow bottle
The following auxiliary equipment has not been tested on ROTAX
Auxiliary equip-
ment not tested
engine type 912 i for safety and durability to the standards of avia-
tion.
- intake filter
- shock mount
Effectivity: 912 i Series
Edition 1/Rev. 0
BRP-Powertrain
INSTALLATION MANUAL
The following equipment is not included as part of the stan-
dard engine version!
Any equipment not included as part of the standard en-
NOTICE
WARNUNG
gine version and so does not be part of the engine is
not in the scope of supply.
Components especially developed and tested for this
engine are readily available at BRP-Powertrain.
Non-compliance can result in serious injuries or death!
WARNUNG WARNING
The user assumes all risks possibly arising by utilizing
auxiliary equipment.
The furnishing of proof in accordance to the latest FAR
or EASA has to be conducted by the aircraft manufac-
turer.
00-00-00
page 6
January 01/2012