1.
GENERAL
Refer to Chapters 6.3.17 and 6.3.19 for servicing of the electrical systems. No major repair or
alterations, as outlined in ASTM F2483, FAR 43, or in this manual are authorized at this time.
To obtain engineering approvals for any major repairs or alterations, please contact Cub
Crafters at:
Cub Crafters, Inc.
th
1918 South 16
Avenue
Yakima, WA. 98903
Tel: 509-248-9491
support@cubcrafters.com
2
ELECTRICAL POWER SYSTEMS
(1) GENERAL
The aircraft uses a 14 volt DC electrical system with the power supplied by a 30 amp engine-
driven alternator and a 12 volt storage battery.
In addition to the alternator and the battery, the electrical system consists of a solid-state linear
regulator, master and starter solenoids, circuit breakers, and switches. The battery is located
underneath the pilot's seat. Refer to Chapter 6.3.19 for the maintenance of electrical power
systems.
5.4.14
Page: 2
CUB CRAFTERS, INC.
CC11-100 MAINTENANCE MANUAL
Manual number SC10000AMM
Date: 08/02/2010