Справочник Пользователя для Honeywell International Inc. 9PGTPL-100A
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1 Mar 2006
34-45-54
MAINTENANCE MANUAL
TPL-100A Processor / Part No. 940-0530-001
Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.
Performance limit inputs. These inputs are used as factors in RA computations.
Performance limit inputs include:
Performance limit inputs include:
•
Performance limit discrete input or ARINC 429 input from performance
management computer
management computer
•
Five discrete altitude limit program strap inputs (2000, 4000, 8000,
16,000, and 32,000)
16,000, and 32,000)
•
Four discrete 1500 fpm climb inhibit inputs which are configured by the
user to limit RAs to performance capabilities of aircraft (Example: wing
flap retracted/extended switch can be connected to these inputs or the
increased climb inhibit inputs depending on the characteristics of the
aircraft.)
user to limit RAs to performance capabilities of aircraft (Example: wing
flap retracted/extended switch can be connected to these inputs or the
increased climb inhibit inputs depending on the characteristics of the
aircraft.)
•
Four discrete 2500 fpm increased climb inhibit inputs configured by the
user to limit RAs to performance capabilities of aircraft.
user to limit RAs to performance capabilities of aircraft.
NOTE: Although not specifically a part of performance limits, the discrete input
from the landing gear retracted/extended switch can be used for
performance limit input in conjunction with inputs described in
paragraphs 4 and 5 above. However, this input is intended for other
functions, such as making a bottom directional antenna behave as an
omni antenna in gear-down situations.
performance limit input in conjunction with inputs described in
paragraphs 4 and 5 above. However, this input is intended for other
functions, such as making a bottom directional antenna behave as an
omni antenna in gear-down situations.
•
Discrete input from weight-on-gear (air-ground) strut switch. Notifies
TCAS as to whether own aircraft is in-flight or on-the-ground.
TCAS as to whether own aircraft is in-flight or on-the-ground.
•
Advisory delay discrete inputs from ground proximity and wind shear
system (if applicable)
system (if applicable)
•
Discrete input from optional advisory cancel switch
•
Five discrete inputs from RA/TA intruder display limit straps. These
straps determine the maximum number of aircraft that can be displayed
on the traffic display (from 1 to 30).
straps determine the maximum number of aircraft that can be displayed
on the traffic display (from 1 to 30).
•
Discrete input from ground display mode strap. This input determines if
traffic is displayed when own aircraft is on-the-ground.
traffic is displayed when own aircraft is on-the-ground.
•
Discrete input from RA/TA display all traffic mode strap. This input
determines if all targets are displayed at all times or only when an RA or
TA is present.
determines if all targets are displayed at all times or only when an RA or
TA is present.