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

Page: 969 / 1956

PAGE 23
Feb 28/07 5E3
34-20-00
PIPER AIRCRAFT, INC.
PA-46-350P, MALIBU MIRAGE
MAINTENANCE MANUAL
d Save Configuration:
Adjust the GAIN controls for a GAIN POT /2 setting to 4- or 5-.
The FAULTS field will display GYRO.
Set the TILT SETTING to 15.0 DOWN. The fault fields will flash indicating that
your settings are being saved. If the save procedure is successful the GYRO fault
will disappear and the azimuth count will cycle through its entire number range.
NOTE: Transmitter FAULTS with the Radar OFF.
If the GYRO fault remains, set the TILT to 0 and repeat the previous step.
Enter EXIT.
After the Calibration is completed then enter SAVE.
Return to the RADAR Setup Page and change Park Position to Centered and
SAVE.
10 See Chart 9 for Port Information.
(c) Data Acquisition Unit (DAU)
The DAU is mounted underneath the instrument panel on the right aft side of the forward
pressure bulkhead (F.S. 100.00) (see Figure 1). Maintenance is on condition.
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.
Configuration/calibration procedures are in 28-40-00.
(d) Magnetometer/OAT Sensor Assembly
See information under Primary Flight Display, above. Removal, installation, and calibration
instructions are provided under “Magnetic Heading Systems - S/N’s 4636375 and up,”
below.
(3) Component Locator
See Figures 1 and 5.
Port Used By
RS232 1 Broadcast
RS232 2
RS232 3
Lightening
RS232 4 Engine
RS232 5 Datalink
RS232 6 Datalink
ARINC 429 RX1 GPS 1
ARINC 429 RX2 GPS 2
ARINC 429 RX3 Traffic
ARINC 429 RX4 PFD Link
Port Used By
ARINC 429 TX1 Radar
ARINC 429 TX2 TAWS
ARINC 429 TX3
ARINC 429 TX4
ARINC 453-1 Radar
ARINC 453-2 TAWS
CHART 9
PORT INFORMATION PAGE