Rotax 912 i Series Maintenance Manual page 116

Installation-related point
Control unit (ECU) connections checked for secure
connection. Connector lock!
See also section 71-00-00 Power plant.
Laying of wiring harness checked.
Grounding cable checked according to aircraft manu-
facturer's specifications. Allocation checked.
See documentation of aircraft manufacturer.
Fuel pump connection checked.
See also section 71-00-00 Power plant.
Fuel system checked for leaks.
See section 12-20-00 Planned maintenance.
Fuel filter checked for blockages.
See section 12-20-00 Planned maintenance.
Propeller installed according to the aircraft manufactu-
rer's and propeller manufacturer's specifications.
See "Documentation of aircraft manufacturer".
Lubrication system filled.
To do this, see section 12-10-00 Adding operating
fluids.
Engine test run/functional test.
See also section 12-20-00 Planned maintenance.
General notes/remarks:
(Please fill in using block capitals!)
(Please fill in using block capitals!)
Location: __________________ Date: __________________ Signature: _________________________
Effectivity: 912 i Series
Edition 1/Rev. 0
BRP-Powertrain
MAINTENANCE MANUAL
OK Remark
71-00-00
Page 6
July 01/2012