Piper Aircraft Corporation Malibu Mirage PA-46-350P, Airplane Maintenance Manual

Page: 964 / 1956

PAGE 18
Feb 28/07
5D22
34-20-00
PIPER AIRCRAFT, INC.
PA-46-350P, MALIBU MIRAGE
MAINTENANCE MANUAL
B. Avidyne Entegra Electronic Flight Instrument System (EFIS) (S/N’s 4636375 and up.)
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 FlightMax Entegra Electronic Flight Instrument System (EFIS) is installed as standard
equipment. See 28-40-00 and 34-10-00 for more info.
(1) Description (See Figure 1.)
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.
(2) Maintenance
The Instructions for Continued Airworthiness (ICA) published by Avidyne provide the
necessary information for maintaining this system as installed in Piper airplanes, except as
noted below.
(a) Primary Flight Display (PFD)
(PIR-PPS60227, Rev. B.)
Use 700-00006-0XX PFD & 700-00011-000 Mag/OAT ICA, Avidyne Document No.
AVPFD-174, latest revision, with the following exceptions:
1 In para 6, Troubleshooting Information, in the chart where it says “OAT (Optional),”
cross out “optional.” The OAT is standard in the Piper installation.
2 In para 7.2 and Figure 7, where the standard Avidyne installation describes
alignment pins and retaining clips on the sides of the PFD, the Piper installation uses
a single alignment pin on the top of the PFD engaging a slot in the upper rear cross
bracket.
3 In para 7.5.2.2, in the “Main RS232 Configuration Page” table, for CHNL 3 under GNS-
430 No 2, both Input and Output should read “Crossfill” instead of “Off.”
4 In para 7.5.4.3, below the heading “Autopilot Unit - STEC Autopilots,” insert the
following:
“If the PFD is replaced, the IRU calibration and Magnetometer calibration must be
completed before continuing with the following steps.”
5 Replace para 7.5.5.1, Barometric Unit Setting, with the following:
a Press LSK L1, labeled “Trim Ann”, as required until “Show” is displayed.
b Press LSK L2, labeled “A/P Annun”, as required until “Show” is displayed.
c Press LSK L3, labeled “V-Speeds”, as required until “Show” is displayed.
d Press LSK R1, labeled “Baro Unit”, as required until “in.Hg”, or “mb” if foreign, is
displayed.
e Press LSK R2, labeled “Horiz Marks”, as required until “Show” is displayed.
f Press LSK R3, labeled “ARS”, as required until “Delta” is displayed.