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
If set to 0, GCAM will disable Mode 2 when CPA is active.
Figure 6-45: ACD Option Page (Page 21/25) – Mode 2 Activation Vertical Offset
The Maintenance ACD Options Page 22/25 displays the ACD Narrow TAL Roll Limit
Options, as shown in Figure 6-46. This ACD option sets the roll angle at which the sensor
begins to draw TAL in the direction of the turn.
Figure 6-46: ACD Option Page (Page 22/25) – Narrow TAL Roll Limit
The Maintenance ACD Options Page 23/25 displays the ACD TAL ILS Deviation Limit
Options, as shown in Figure 6-47. TAL inhibition glideslope deviation limits when
glideslope and localizer are both valid (units of ddm). When the absolute value of the
glideslope deviation is greater than this value, TAL is not inhibited. When the absolute
value of glideslope deviation is less than this value, TAL is inhibited. If “Disable TAL
Approach Inhibition” is disabled, this setting is irrelevant. 1 dot = 0.0875 ddm.
Figure 6-47: ACD Option Page (Page 23/25) – TAL ILS Deviation Limit
The Maintenance ACD Options Page 24/25 displays the ACD Display Alert Line Aperture
Options, as shown in Figure 6-48. This parameter sets the width of the look-ahead
sensor used to generate the TAL.
6-52
04 Nov 2014
34-45-29
Pub. No. 8600200-001, Revision 004
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