Rotax 912 i Series Maintenance Manual page 128

Control unit (ECU)
See also section 76-10-00 Control unit (ECU).
Step
1 Detach the couplers (ECU LANE A1, ECU
LANE A2 and ECU LANE B).
Fig. 14
1. Coupler (LANE A1)
2. Coupler (LANE A2)
3. Coupler (LANE B)
Step
2 Press in the lock so that the clamp can be
rotated.
3 Press the clamp down until it latches.
4 Remove the coupler.
Effectivity: 912 i Series
Edition 1/Rev. 0
BRP-Powertrain
MAINTENANCE MANUAL
Procedure
Procedure
Fig. 15
1. Lock
REMOVAL OF THE POWER PLANT FROM
THE AIRCRAFT
Lift the engine from the aircraft using a crane or
similar lifting gear.
WARNUNG WARNING
Danger of injury due to falling parts!
When the engine is removed there is a risk of
injury due to the engine or its assemblies falling!
Only use permitted lifting gear and special tools
for this work!
Fasten the lifting gear only to the transport brak-
kets. Note center of gravity!
Do not walk under the lifted engine!
Wear protective footwear!
NOTICE
WARNUNG
Danger of damage to the engine and aircraft!
Before the engine is removed, ensure that all
detachable connections between the engine
and the aircraft, i.e. hoses, lines, cables, cable
ties and clamps have been disconnected and
moved out of position so that they do not obst-
ruct removal!
71-00-00
Page 18
July 01/2012