d05781.fm
INSTALLATION MANUAL
BRP-Powertrain
Effectivity: 912 i Series
Edition 1/Rev. 2
24-00-00
Page 15
January 01/2014
4) External alternator (optional extra)
General note See Fig. 7.
4.1) Technical data
General note NOTE: The voltage regulator is integrated in the alternator.
Output Output: Max. 550 W/DC at 6000 r.p.m. (complies ~ 4800 r.p.m. crank-
shaft speed)
Output voltage Output voltage: 13.5 V
Ambient tempera-
ture range
Ambient temperature: Min. -30 °C (-22 °F)
Max. +90 °C (194 °F)
Weight See chap. 72-00-00 section 2) Subsection 2.1: Weight.
4.2) Connections
Power supply
wires
Power supply wires to external alternator (1) have to be installed depen-
ding on the mounting position and according to the regulations of the
aircraft manufacturer.
Positive terminal Positive terminal (2):
- M6 screw connection suitable for cable terminal according to DIN
46225 (tightening torque 4 Nm (35 in.lb)).
Grounding Via engine block.
Control wiring Control wiring (3):
- via supplied standard plug (Sumitomo 6111-2568) and 6.3 x 0.8
Faston connectors (female).
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