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B
Due to tolerances in the TAS Processor analog I/O hardware, the accuracy for
the 0 - 100 foot range may be ± 10 feet.
E. On Ground Display Mode; TAS in Standby Mode On-Ground or TAS in
TA Only Mode On-Ground.
The On Ground Display Mode will indicate to the processor whether
the system will go to Standby Mode when on the ground or that the
system will go to TA Mode (with aurals and voice inhibited due to alti-
tude defined by TAS logic) when the aircraft is on the ground.
F.
Baro Altimeter Type; Gillham, ARINC 575, ARINC 706.
The Barometric Altimeter Type program will indicate the type of baro-
metric altimeter source [either Gillham/Gray Code, ARINC 575 (ARINC
419) or ARINC 706 (ARINC 429)] that interfaces to the TAS Processor.
G. Controller Type; ARINC 735 Protocol, or Discrete Control.
The Controller Type will determine the type of control data, either the
Control Panel to the TAS Processor via the CNTL HD RX (ARINC 429)
input bus or via Discrete Control switches.
H. Ground Headphone Volume; 1.25, 2.5, 5, 10, 20, 40, 80, 100 mw.
The on ground headphone level will be configurable to the above lev-
els.
I.
Airborne Headphone Volume; 1.25, 2.5, 5, 10, 20, 40, 80, 100 mw.
The airborne headphone level will be configurable to the above levels.
J.
Airborne Functional Test; Inhibited or Allowed.
When the Airborne Functional Test is inhibited, the TAS Processor will
inhibit Functional Test while in the air.
When the Airborne Functional Test is allowed, the TAS Processor will
allow Functional Test in the air.
K. ATE Output; Enabled or Disabled.
The ATE Output will be used to enable the ATE lines for the Anechoic
Chamber and the RGS stations.
Rev 3, August/2002
NOTE
10609I03 CDL
KMH 880/KTA 870
Page 4-17
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