User's Manual
Table Of Contents
- T3CAS_Section_5
- 5 Adjustment/Test
- 1. General
- 2. Equipment
- 3. Initial Harness Checkout (New Installations Only)
- 4. System Self-Tests
- 5. Return-to-Service Test
- 6. Operational Software Loading Using an ARINC 615A Portable Data Loader or Compact Flash Card
- 7. Downloading Information from the TP3PCAS Using a CF Card
- 1. Obtain a New or Blank Compact Flash (CF) card.
- 2. Copy to the New or Blank CF card the appropriate ‘Header File’
- a) Header files are files copied to the New or Blank CF card that will instruct the computer unit what is desired to be downloaded.
- b) Header files needed to download Maintenance Data, Event Data and CRC Part Numbers can be obtained from ACSS Customer Services at +1-623-445-7070 or crc.acss@l-3com.com.
- 3. For downloading Maintenance Data, Event Data or CRC Part Numbers the aircraft does not need to be in an on-ground configuration.
- 4. Apply power to the computer unit.
- 5. Insert the CF card.
- 6. For ACSS part numbers 9005000-10000, -10101, -10202, and -10204 the DATA STATUS LED will UblinkU green once; this indicates the unit recognized that a CF card was inserted.
- 7. For ACSS part numbers 9005000-11203, -11801 and -55801 the DATA STATUS LED will UblinkU green while reading the header file and performing the action defined in the header file.
- 8. Flight Data Recording
- 1. T3CAS part numbers 9005000-10000, -10101, -10202, and -10204 only support FAT16 CF card formatting. T3CAS part numbers 9005000-11203, -11801 and -55801 support both FAT16 and FAT32 CF card formatting.
- B. Flight Data
- 1. Obtain a New or Blank CF Card.
- 2. Copy to the New or Blank CF Card the Appropriate Header File.
- 3. Header files are files copied to the New or Blank CF card that will instruct the computer unit what is desired to be downloaded.
- 4. For Flight Data Recording, the aircraft does not need to be in an on-ground configuration.
- 5. Apply power to the computer unit.
- 6. Insert the CF card.
- B. Flight Data
- 9. Downloaded Maintenance Data, Event Data And Flight Data May Be Sent To ACSS Customer Services For Analysis
- 5 Adjustment/Test
- T3CAS_Section_6
- T3CAS_Section_7
- 7 Maintenance Practices
- 1. General
- 2. Equipment and Materials
- 3. Procedure for the TP3PCAS Computer Unit
- 4. Procedure for the APM (Not applicable for part numbers 9005000-10000, -10101, -10202, -10204, or -11203)
- 5. Procedure for the Directional Antenna
- 6. Procedure for the Omnidirectional Antenna (Applicable to part numbers 9005000-11203, -11801 and -55801)
- 7. Procedure for the Control Panel
- 8. Procedure for the VSI/TRA Display
- 9. Instructions for Continued Airworthiness, FAR Part 25.1529
- 7 Maintenance Practices
- T3CAS_Section_8
- T3CAS_Section_9
- T3CAS_Section_10
- T3CAS_Appendix_A
SYSTEM DESCRIPTION AND INSTALLATION MANUAL
T
3
CAS/Part No.9005000
Table 4-42: In-Trail Procedures Enable/Disable Configuration
(Applicable to 9005000-10000, -10101, -10202, -10204, or -11203)
Configuration
Number
Spare ITP Enable Spare
Connect
RBP-2A to:
1
Disable
Disable
Disable
Open
2 (Spare Conf)
Disable
Disable
Enable
RMP-1G
3
Disable
Enable
Disable
RMP-1H
4 (Spare Conf) Disable Enable Enable RMP-2E
5 (Spare Conf) Enable Disable Disable RMP-3E
6 (Spare Conf)
Enable
Disable
Enable
NA
7 (Spare Conf)
Enable
Enable
Disable
NA
8
Enable
Enable
Enable
RBP-7K
9 (Invalid) Invalid Invalid Invalid NA
(24) CDTI Assisted Visual Separation/Spacing Enable/Disable Configuration.
(SeeTable 4-43)
Table 4-43: CDTI Assisted Visual Separation/Spacing Enable/Disable Configuration
(Applicable to 9005000-10000, -10101, -10202, -10204, or -11203)
Configuration
Number
Spare CAVS Enable Spare
Connect
RBP-2B to:
1
Disable
Disable
Disable
Open
2 (Spare Conf)
Disable
Disable
Enable
RMP-1G
3 Disable Enable Disable RMP-1H
4 (Spare Conf) Disable Enable Enable RMP-2E
5 (Spare Conf) Enable Disable Disable RMP-3E
6 (Spare Conf)
Enable
Disable
Enable
NA
7 (Spare Conf)
Enable
Enable
Disable
NA
8
Enable
Enable
Enable
RBP-7K
9 (Invalid) Invalid Invalid Invalid NA
(25) This section defines the Aircraft Altitude Limit Pin Programming. These inputs
indicate the altitude above which, under worst case conditions, the aircraft cannot
climb at a rate of 1500 feet per minute (457.2 meters per minute) or greater (see
ARINC 735B for more details).
4-138
04 Nov 2014
34-45-29
Pub. No. 8600200-001, Revision 004
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