INSTALLATION OF PA-44-180T EGT PROBE. (Refer to Figure 77-4)
When routing lead cable, leave a minimum of 1/2 inch slack
between the engine and the engine mount to compensate for
engine shock movement.
1. Install the probe in the exhaust stack.) Maintaining the 2.75 inch dimension indicated, secure the probe
by tightening the jam nut.
DO NOT KINK OR PINCH THE LEAD WIRE. MINIMUM
BEND RADIUS OF THE LEAD WIRE IS 1/8 INCH.
2. Secure the lead cable to the engine mount and route cable through the leading edge of the wing and into
the fuselage to the rear of the EGT gauge.
3. Attach the lead wires to the appropriate terminals of the gauge.
PIPER AIRCRAFT
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
— NOTE —
— CAUTION —
— END —
3H17
77-32-04
Page 77-15
Revised: June 20, 1995