(d) Aircraft Setup
1
From the MFD maintenance page, depress the LSK (R2) for accessing the Aircraft
Setup page.
2
Using the right knob to select the configuration field and the left knob to change the
desired configuration, configure the Aircraft Setup page for the following conditions:
a
Narrowcast, or Datalink: Quake SC
(if Data Link option installed, otherwise “Not Installed”)
b
Port: RS232 6
c
* Broadcast: XM Radio
d
* Port: RS232 1
e
Aux Data: Avidyne PFD (Entegra PFD)
f
Port: ARINC 429 4
g
Dimming Bus Voltage Settings:
Shows current voltage, no setting required (shows 0.0 volts when annunciator
day/night switch on DAY. Dimming bus voltage shown when switch is on NIGHT).
Brightest Dimming Voltage: 24 volts
Darkest Dimming Voltage: 5 volts
h
When the Aircraft Setup has been configured correctly, press Save. If you
decide not to save the changes, press Cancel. Changes will not take effect until
the MFD has been restarted.
* Only with Avidyne software “#530-00177-000” or later.
(e) See 28-40-00 for Fuel Quantity Indication Calibration.
(3) Data Acquisition Unit (DAU)
(a) Use 200-00041-000 DAU ICA, Avidyne Document No. AVSIU-011, with the following
exceptions:
1
In para 6, in “Table 2 - DAU Pinout,” pins J1-2 and J1-21 have “No Connection” in the
Piper installation.
2
In para 6, in “Table 4 - DAU Sensor Compatibility,” parameter “VAC” is not used in the
Piper installation.
(b) Removal and Installation
The DAU is mounted on the left forward side of the frame assembly at F.S. 128.737 (see
Figure 2, Sheet 2, View B-B). Remove the rear seats and floor panel for access.
(4) Magnetometer/OAT Sensor Assembly
See information under Primary Flight Display, above. Removal and installation instructions are
provided under “Magnetometer/OAT Sensor Assembly,” below.
C. Component Locator
See Figure 2.
PIPER AIRCRAFT, INC.
PA-28-161, WARRIOR III
MAINTENANCE MANUAL
PAGE 7
Nov 30/06
3H7
34-20-00
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