AlliedSignal KAP 140 Manual de Instalação descarregar pdf (Página 22)

BENDIX/KING

KAP 140

Page 2--2

Revision 6, Oct 2002

CS:00991I06.IDU

2.3.2 KC 140 Installation

The KC 140 installation will conform to standards designated by the customer, installing agency,

and existing conditions as to the unit location and type of installation. However, the following

instructions will assure a more satisfactory performance from the equipment. Mounting locations

are provided near the front and rear of the mounting rack. It is necessary to utilize both the front

and rear mounting locations when installing the KC140 mounting rack.

CAUTION

For two axis installations the static port on the rear of the

KC140 is designed to float to ensure alignment with the static

port on the mounting rack. Do not attempt to tighten the

mounting screws for the KC140 static port.

W ARNING

FOR TWO AXIS INSTALLATIONS REMOVAL OF THE KC 140

FROM ITS MOUNTING RACK IN THE AIRCRAFT PANEL OPENS

THE STATIC AIR SYSTEM TO THE AIRCRAFT CABIN. AFTER

REINSTALLATION OF THE KC140, VERIFY THAT THE STATIC

AIR SYSTEM COMPLIES WITH F.A.R. 91.411.

NOTE

The following information is provided in the event that the o--ring on

the KC140 static port requires replacement. The o--ring is 70

durometer EPDM material, AS568A--006 size. The AlliedSignal part

number is 187--01004--0013. The o--ring should be greased with

AlliedSignal part number 016--01210--0000, Dow Corning 55 o--ring

Lubricant (Mil--G--4343) or equivalent grease.

2.3.3 Installation Procedures

Refer to the appropriate STC installation manual.

The first time the AFCS is turned on in a new installation, the FCC must be configured through an

RS232 interface. The FCC provides an RS232 interface for diagnostic and installation capabilities.

2.3.3.1 RS232 Interface

The RS232 interface to the computer is through a Remote Terminal Interface (RTI) connector

located in the cockpit. A terminal or PC with terminal emulation must be connected to this port. Set

the communication parameters as follows: 9600 baud rate, no parity , 8 data bits, and one stop bit.

IMPORTANT: System configuration cannot be accomplished without using the RTI. Use computer

cable assembly PN 155--02794--0001, to connect PC communications port to the RTI connector.

2.3.3.1.1 RTI Main Menu

Apply power to the flight computer. Preflight test will attempt to run, but will fail if the unit has not

been previously installed. After a few seconds, the main menu should appear on the terminal. If it

does not, press CTRL--W to refresh the screen. If communications cannot be established, check

the RS232 interconnect and terminal setup.

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