Garmin AT Inc. AT7000 Manual De Usuario

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Installation Manual
Troubleshooting
560-0405-00 Rev –
December 14, 2001
Page 45
© 2001 by UPS Aviation Technologies Inc.
Section 9 -  Troubleshooting
9.1  Introduction and Overview
9.1.1 
Introduction
The AT7000 includes a status display located on the unit front panel which provides ad-
ditional information from the status LEDs.  The display is used to display the mainte-
nance information.  The four buttons located below the display are used to scroll through
the available display information.
The maintenance display includes an LED backlight. The backlight turns on when a but-
ton is pushed and remains on for five minutes after the last button is pressed.
9.1.2 
Overview
The AT7000 consists of the following interfaces for the user. On the front panel is a four
line by 16-character LCD display with backlight, five push buttons, and six status LEDs.
These interfaces are used to provide information useful for unit diagnostics, installation
checkout and verifying of aircraft interface inputs.
The maintenance display provides information about the unit, including: software version
number, system failure information, configuration pin inputs, discrete inputs, external
interfaces, and receiver/transmitter enable status.
Figure 14.  AT7000 Mode S Transponder
MAINTENANCE DISPLAY
XPDR PASS
XPDR FAIL
CTRL PNL
ALT
TOP ANT
BOT ANT
TEST
DATA LOADER
AT7000
Mode S Data Link Transponder
barcode of serial number
SN '1234567'
UPS Aviation Technologies,        Salem  OR  USA
Model:
AT7000
PN:
   430-6091 - 00   -   00
SW Mod
TSO-C112 Class 2A7, 121, 011
RTCA/DO-178B Software Level B
RTCA/DO-160D Env. Cat.
FCC ID xxxxxxx
 Mode S Transponder
C
AA
D E
AB
AC
B
A
F G H J K L
Z
Y
X
W
V
U
T
S
R
P
N
M
ADAE AFAG AH AJ AK ALAMAN
HW Mod
C
AA
D E
AB
AC
B
A
F G H J K L
Z
Y
X
W
V
U
T
S
R
P
N
M
ADAE AF AGAH AJ AK ALAMAN
Software
Map/Database
Weight
10.0 lbs.