THE NEW PIPER AIRCRAFT, INC.
PA-32-301FT / 301XTC
MAINTENANCE MANUAL
PAGE 2
Feb 19/04
3I2
34-20-00
2. Standby
Attitude Indicator
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.)
In 6X S/N’s 3232014 & up and 6XT S/N’s 3255015 & up with the optional Avidyne Entegra Electronic
Flight Display System installed, an electric standby attitude indicator is installed to the left of the Primary
Flight Display (PFD).
Other than removing and replacing the unit itself (see 39-10-00), the only line replaceable part is the
emergency power battery which is located under the instrument panel mounted to a bracket on the left
side of the fuselage. See Appendix 2 (grid 3L3) for an illustration.
Required periodic maintenance is listed in 5-20-00 and 5-30-00. Checkout and test procedures and
Instructions for Continued Airworhiness are provided in Mid-Continent Instruments Manual No.
90157262.
3. Electronic Flight DIspla
y System
W
ARNING: 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.)
6X S/N’s 3232014 & up and 6XT S/N’s 3255015 & up may be equipped with the Avidyne Entegra
Electronic Flight Display System as an optional installation. If so, see Appendix 2 (grid 3L3).