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Piper PA-28-161 Maintenance Manual

Piper PA-28-161
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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.

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Piper PA-28-161 Specifications

General IconGeneral
ManufacturerPiper Aircraft
ModelPA-28-161 Warrior II
EngineLycoming O-320-D3G
Horsepower160 hp
Seating Capacity4
Wingspan35 ft (10.7 m)
Length24 ft 0 in
Maximum Speed127 knots
Cruise Speed122 knots
Maximum Takeoff Weight2, 325 lb (1, 055 kg)
Fuel Capacity48 US gallons (182 L)

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