External Alternator (Optional Extra); Technical Data; Connections - Rotax 912 i Series Installation Manual

4) External alternator (optional extra)

See
General note
4.1)

Technical data

NOTE:
General note
Output: Max. 550 W/DC at 6000 r.p.m. (complies ~ 4800 r.p.m. crank-
Output
shaft speed)
Output voltage: 13.5 V
Output voltage
Ambient temperature:
Ambient tempera-
ture range
See chap. 72-00-00 section 2) Subsection 2.1: Weight.
Weight
4.2)

Connections

Power supply wires to external alternator (1) have to be installed depen-
Power supply
wires ding on the mounting position and according to the regulations of the
aircraft manufacturer.
Positive terminal (2):
Positive terminal
- M6 screw connection suitable for cable terminal according to DIN
Via engine block.
Grounding
Control wiring (3):
Control wiring
- via supplied standard plug (Sumitomo 6111-2568) and 6.3 x 0.8
Effectivity: 912 i Series
Edition 1/Rev. 2
BRP-Powertrain
INSTALLATION MANUAL
Fig. 7.
The voltage regulator is integrated in the alternator.
46225 (tightening torque 4 Nm (35 in.lb)).
Faston connectors (female).
Min. -30 °C (-22 °F)
Max. +90 °C (194 °F)
24-00-00
Page 15
January 01/2014