PIPER AIRCRAFT, INC.
PA-28-161, WARRIOR III
MAINTENANCE MANUAL
PAGE 1
Nov 30/06
5D21
77-00-00
GENERAL
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.)
1. Description
NOTE: In S/N’s 2842218 and up, for airplanes equipped with the Avidyne Entegra EFIS, engine data is
collected by the Data Acquisition Unit (DAU) and is displayed on the Multi-Function Display
(MFD) and Primary Flight Display (PFD). See Electronic Flight Instrument System, 34-20-00,
and 91-77-40.
These airplanes use traditional 3-inch analog engine instruments, which are electrically or mechanically
actuated. These instruments and their specific functions are addressed in 77-10-00, 77-20-00, and
79-30-00.
2. Remo
val and Installation
See Face Mounted Instruments, 39-10-00.
This chapter gives information on service and replacement procedures of the engine indicating system.
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