THE NEW PIPER AIRCRAFT, INC.
PA-32-301FT / 301XTC
MAINTENANCE MANUAL
PAGE 1
Feb 19/04
3L9
APPENDIX 2
ELECTRONIC FLIGHT DISPLAY SYSTEM
WARNING: FAILURE TO CONSULT APPLICABLE VENDOR PUBLICATION(S), WHEN SERVICING
OR INSPECTING VENDOR EQUIPMENT INSTALLED IN PIPER AIRCRAFT, MAY
RENDER THE AIRCRAFT UNAIRWORTHY. SEE INTRODUCTION - SUPPLEMENTARY
PUBLICATIONS.
The Avidyne Entegra Electronic Flight Display System (EFDS) is available as an option in 6X S/N’s 3232014
and up and 6XT S/N’s 3255015 and up.
1. Description
This system uses two large 10.4-inch diagonal, high-resolution, sunlight-readable full color displays
(PFD and MFD), to provide primary flight and engine information as well as a wide variety of other data.
Standard primary flight instruments (i.e. - airspeed, electric attitude indicator, and altimeter) provide
redundancy. (See Figure 1.)
The EFDS installation consists of the following components Primary Flight Display (PFD), Multifunction
Display (MFD), Data Acquisition Unit (DAU) and associated sensors, and Magnetometer/OAT Sensor
Assembly.
Avidyne Entegra Instrument Panel (Optional)
Figure 1
Eff
ectivity
3232014 & up
3255015 & up
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