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 4-1: T
3
CAS Computer Unit Interface Description (cont)
(Applicable to Part No. 9005000-10000, -10101, -10202, -10204, and -11203)
Connector
Pin
Designation
Functional Description
RBP-1E
Reserved
RBP-1F, G
GPS #2 Time Mark Input: [RBP-1F (A), RBP-1G (B)]
These RS422 differential pair inputs are provided to receive the Time Mark signal
from an external GPS receiver in order to provide synchronization with other
aircraft systems. This signal is also used to remove the latency error from GPS
when available.
RBP-1H
RA Data Word 270 Bit 18 Discrete Output
This discrete output provides RA information to the ARINC 573 flight recorder. The
output goes to the “ground” state each time its associated bit within the advisory
field of the RA output words changes from a “zero” condition to a “one” condition.
The output remains in the “ground” state for as long as the associated RA bit
remains non-zero. This output is read by the flight recorder as either a series or
shunt output.
NOTE: The discrete is pulled up to +28 V dc in the “open” state.
RBP-1J
RA Data Word 270 Bit 19 Discrete Output
See RBP-1H.
RBP-1K
RA Data Word 270 Bit 20 Discrete Output
See RBP-1H.
RBP-2A
Program Pin Parity Input
RBP-2B
Program Pin Parity Input
RBP-2C
THRU
RBP-2G
Reserved for TCAS/ADS-B Pin Strobing.
RBP-2H
RA Data Word 270 Bit 21 Discrete Output
See RBP-1H.
RBP-2J
RA Data Word 270 Bit 22 Discrete Output
See RBP-1H.
RBP-2K
RA Data Word 270 Bit 23 Discrete Output
See RBP-1H.
RBP-3A, 3B
Radio Altimeter No.2 ARINC 552/Analog Input: [RBP-3A (HI), RBP-3B (LO)]
See RMP-2H and -2J.
RBP-3C
Radio Altimeter No.2 Valid Discrete Input (PO)
See RMP-2H. Valid condition is greater than +18.5 V dc. Invalid is open.
RBP-3D, 3E
Radio Altimeter No.2 Input: [RBP-3D (A), RBP-3E (B)]
See RMP-13H. Also see RMP-2H.
Pub. No. 8600200-001, Revision 004
34-45-29
4-25
04 Nov 2014
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