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
CLIMB INH
0000
Climb Inhibit inputs:
RMP-1J, RMP-13G, RBP-5J, RBP-5K.
INC CLIMB INH
0000
Increase Climb Inhibit inputs:
RBP-5E, RBP-5F, RBP-5G, RBP-5H
ADVISORY INH
0000
Advisory Inhibit inputs:
RBP-5A, RBP-5B, RBP-5C, RBP-5D
RADIO ALT TYPE
1
0000
Analog Radio Altimeter Type: RMP-12B
ARINC 552/552A (0), Collins BCA (1)
VOICE DELAY
ENABLE
0
Voice Delay option: RBP-7D
Enabled = (1), Disabled = (0)
AUDIO PROG PINS
000
Audio output level selection inputs:
RBP-7A, RBP-7B, RBP-7C
CANCEL DISCRETE
2
0
Advisory Cancel Discrete option: RMP-3D (0)
allows advisories to be cancelled. A (1) does not
allow advisories to be cancelled.
DTIF PIN
0
DTIF Enabled Option: RMP-5E
Selection of code 0005 displays the second of four pages that define the
Program Pins status. See Figure 6-7.
Figure 6-7: Typical Program Pins 2/4 Page
Where more than one program pin is indicated, the listed connector pins
correspond to the display digits read from left to right. A one (1) indicates
the associated pin is grounded. A zero (0) indicates open.
Selection of code 0006 displays the third of four pages that define the
Program Pins status. See Figure 6-8.
6-24
04 Nov 2014
34-45-29
Pub. No. 8600200-001, Revision 004
Use or disclosure of information on this page is subject to the restrictions in the proprietary notice of this document.