Honeywell International Inc. 9PGTPL-100A 用户手册

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页码 180
Page 2009
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.
right middle plug (RMP)
left top plug (LTP)
right top plug (RTP). 
Table 2002 lists the MILACAS-FR Processor connector pin assignments.
(b) Directional Antenna Connectors
Four coaxial cables with TNC connectors connect the ANT-81A directional 
antenna connectors J1 through J4 to the MILACAS-FR Processor, shown in 
Figure 2001 and 2002.
D. Wire Strapping Options
MILACAS-FR system wire strapping options are implemented by externally connecting pins 
on the MILACAS-FR system connectors. The configurations of the straps are identified by 
the software in the particular unit. In most cases, the selected strap is connected to a 
common ground pin on the associated connector but in some instances may be connected 
to aircraft ground.
(1)  MILACAS-FR Processor Straps
(a) Cable Delay Program Straps
Three straps, on RBP pins 7G, 7H, and 7J, are selectively connected to a common 
ground on RBP pin 7K, to compensate for the differences in coaxial cable lengths 
between the top and bottom TCAS antennas (up to a maximum of 300 
nanoseconds). See the interconnect diagram, Figure 2002, for strapping details.
(b) Aircraft Altitude Limit Program Straps
Some aircraft may not be able to achieve a 0.25 G vertical acceleration to a 1500 
FPM climb rate for an altitude gain of 750 feet above a certain altitude under all 
circumstances. The logic is made aware of these conditions by the altitude limit 
straps so that a resolution advisory such as "Don't Climb" is issued. These 
program pins select the "can't climb" altitude in 2000 foot increments up to 62,000 
feet. Jumper wires from pins RMP-6E through RMP-6J to RMP-6K are necessary 
to program the required altitude. The limits set by the pins represent the worst 
case. The limits set by the pins must be used as a default when the flight 
management computer indicates that the climb must be limited. If no jumpers are 
installed, the altitude will be zero feet.