Schempp-Hirth Flugzeugbau Ventus-2cM Flight Manual page 133

SCHEMPP-HIRTH FLUGZEUGBAU GmbH., KIRCHHEIM/TECK
Ventus-2cM
VIII
Fuse console at panel base
14 15 1 2 3
50 7.5 15
7 8 9
1 POWER PLANT MASTER SWITCH (CIRCUIT BREAKER 50 A)
This circuit breaker disconnects the power plant from its power source
(battery M).
For the gliding avionics a separate main switch is provided – see (2).
2 AVIONIC MAIN SWITCH (CIRCUIT BREAKER 7.5 A)
Power for the avionics is provided by a battery situated at the base of the
instrument panel and/or by up to two batteries located on the r.h.s. of the
main wheel housing or/and a battery in the vertical fin.
The power plant batteries, however, may also be used for feeding the
avionics by actuating the selector switch – see (13).
3 CIRCUIT BREAKER 15 A
Power on, this circuit breaker must always be depressed, otherwise the
power plant batteries (located in the fuselage nose cone) will not be
recharged by the generator.
November 2003
Revision --
4 5 6
12 5 2
10 11 12 13
1 Circuit breaker - 50A (power plant master switch)
2 Circuit breaker - 7.5A (avionic main switch)
3 Circuit breaker - 15A (generator)
4 Circuit breaker - 12A (spindle drive)
5
Circuit breaker - 5A (power plant system)
6
Circuit breaker - 2A (fuel pump)
7 LED signal (water pump defective)
8 Circuit breaker - 2A non-autom. (water pump)
9
Circuit breaker - 4A non-autom. (emergency system)
10
Circuit breaker - 4A non autom.
(charg. socket avionic batt.)
Circuit breaker - 4A non-autom. (charg. socket
11
power plant batteries / fire warning dev.)
Circuit breaker - 6.3A non autom. (avionic batt.)
12
Battery selector switch (power plant / avionic batt.)
13
Charging socket (power plant battery)
14
15 Charging socket (avionic battery)
FLIGHT MANUAL
7.3.8