Textron Cessna 182S - FIGURE 01 - MANIFOLD PRESSURE;FUEL FLOW

CESSNA
AIRCRAFT
COMPANY
MODEL 182/T182
WIRING DIAGRAM MANUAL
NOTES:
1. ALL
WIRE 22AWG UNLESS
OTHERWISE NOTED
INSTALL POLARIZING PIN INTO PIN 3 OF J1033.
UN006
FUEL PRESSURE
JN001
TRANSDUCER
Ic
OUTPUT VOLTAGE
5V INPUT
MANIFOLD PRESSURE/FUEL FLOW
Figure 01 (Sheet 1)
©CESSNA AIRCRAFT COMPANY
77-30-01
0770548D1
Figure 01
Page 0
Mar 1/2004