EasyManuals Logo

Piper Warrior III User Manual

Piper Warrior III
1104 pages
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Page #571 background imageLoading...
Page #571 background image
PIPER AIRCRAFT, INC.
PA-28-161, WARRIOR III
MAINTENANCE MANUAL
PAGE 3
Nov 30/06
3H3
34-20-00
GMA-340
SYSTEM 55X
GNS-430 #1
GNS-430 #2
ALT
ASI
ADI
ADF
(OPT)
PFD DISPLAY
MFD DISPLAY
101901-SHT 5-N
GTX-330
TRANSPONDER
ADF RECEIVER
(OPTIONAL)
DME
(OPTIONAL)
EFIS Panel (Optional)
Figure 1
Effectivity
with Avidyne Entegra
3. Electronic Flight Instrument System
(EFIS)
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 Instrument System (EFIS) is available as an option in S/N’s
2842218 and up.
A. Description (See Figures 1, 2 and 3.)
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.
The EFIS 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.

Table of Contents

Questions and Answers:

Question and Answer IconNeed help?

Do you have a question about the Piper Warrior III and is the answer not in the manual?

Piper Warrior III Specifications

General IconGeneral
BrandPiper
ModelWarrior III
CategoryAircrafts
LanguageEnglish

Related product manuals