STEMME S12 User Manual

F S12 MAIN SYSTEM  DC GENERATION
27.03.2017 Gulbe
P308-124910
00
DE.21G.0068 EASA 21J.250
01
Date
Name
checked
drawn
Title
Doc Number
Page
Rev. Change
P069-E074-196
S12 Main System
DC Generation
27.03.2017 Baum
V
Volt/Ampere
2a
2b1a
1b
12
3a
3b
3
A
PX1P
PX2P
PX20P
PX2PN
PX30P
PX3P
PX20PN
PX6P
MAIN BUS - INSTRUMENT PANEL
PX10P
refer to: P308-124.920
S12 Engine System -
DC Generation
99
1
1
45
5
PX3Ps PX30Ps
PX6Ps
Instrument Panel
50A
PP1F
VV10F
Shunt
PX4F
PX5F
Steel Frame GND
#9, 2A
#10, 2A
50A
OVP-1
yellow
red
blue
yellow
2
PC6FN
PC7F
PC9F
PC8F
VV11F
2b
2a1b
1a
12
Master
Split Switch
PP2PN
AVIONICS BUS - INSTRUMENT PANEL
VV14P
red
G
Alternator
B+
E1A
L
IG
E217E216
2a
2b1a
1b
12
MAIN BUS - SYSTEM BOX
VV12F
VV13P
Steel Frame GND
PC60F
22.000µF
PC60FN
PP2P
ALT
ON
Ext Alt Lamp
Ext Alt Field
2 x 56
PC3P
PC1P
PC4P
PC4PN
PC2P
PC5P
refer to: P308-124.921
S12 Engine System -
Engine Monitoring and Control
UE3P
Engine Compartment
Main System Box
#XX, 2A
#3, 2A
External
Generator
Warning
#2, 5A
Charge Controller
Solar Cells
+
-
#8, 10A
Engine Cowl
01
P061-2016-102
PL6F
PL5F PL5FN
#7, 5A
USB Charge Socket
Charge Controller
USB Cable
36 37
36 37
Charge Socket
PL3P
PL3FN
CPC
37pol
Center Console
PC6F
2 x 831.697
02
P061-2017-039
optional

STEMME S12 Specifications

General

Brand	STEMME
Model	S12
Category	Aircrafts
Language	English