User's Manual Part 1

CAS / Part No. 9000000

SYSTEM DESCRIPTION AND INSTALLATION MANUAL

34-43-20

15 Feb 2003

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TC--6

Section

Page

4. System Self--Te sts 5--3.........................................................

A. TCAS Flight Deck Display Test Modes 5--3...................................

(1) Short Test Mode 5--3...................................................

(2) Extended Test Mode 5--4...............................................

B. TAWS/RWS Flight Deck Display Test Modes 5--5..............................

(1) Standard Test Mode 5-- 5...............................................

(2) Extended Test Mode 5--7...............................................

C. T

CAS Computer Unit Self--Test 5--9.........................................

5. Return to Service Test 5--11.....................................................

6. Operational Software Loading Using an ARINC Portable Data

Loader, RS232 Port or Compact Flash Card 5--11..................................

A. Current Software Verification 5--12............................................

(1) TCAS Software Verification 5-- 12.........................................

(2) TAWS/RWS Software Verification 5 --12....................................

B. Portable Data Loader -- TCAS Operational Software Loading

(While Installed on Aircraft) 5--12.............................................

C. Compact Flash Card -- TAWS/RWS Operational Software/ACD/ASDB

Loading (While Installed on Aircraft) 5--13.....................................

D. RS232 -- TAWS/RWS APM Configuration Data and APM

Application Data Loading 5--15...............................................

E. Updated Software Verification 5--15...........................................

(1) Software Verification Using Flight Deck Systems ONLY 5--15................

(2) TCAS Software Verification Using a Stand-- Alone PC ONLY 5--15............

(3) TAWS/RWS Software Verification Using a Stand--Alone PC ONLY 5--17.......

(4) TCAS Software Verification Using a Software Verification Fixture ONLY 5--18..

(5) TCAS Software Verification Using a Remote Connected VSI/TRA ONLY 5--18.

FAULT ISOLATION 6--1...........................................................

1. General 6--1..................................................................

2. Equipment and Materials 6-- 1...................................................

3. Procedure 6--1................................................................

A. CMC or CFDS 6--1........................................................

B. Flight Deck Initiated Self-- Test/Fault Display Systems 6--1......................

(1) TCAS 6--1............................................................

(2) TAWS/RWS 6--2.......................................................