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
Lamp Format 2 - the warning alert discrete output (RTP-13D) are grounded only
for the warning audio messages containing the phase “PULL-UP” or “AVOID
TERRAIN and the caution alert discrete output (RTP-13B) is used for all other
alert messages.
(4) Spare Configuration/Automatic CPA-THD Deactivation/CPA-THD Function. (See
Table 4-22.)
Table 4-22: Spare Configuration/Automatic CPA/OCPA-THD/OHD Deactivation/ Spare
Configuration
Number
Spare
Automatic
CPA/OCPA-THD/OHD
Deactivation
Spare
Connect RTP
7C to:
1
Disable
Active
Disable
Open
2
Disable
Not Applicable
Enable
RTP-13B
3
Disable
Inactive
Disable
RTP-13C
4 Disable Not Applicable Enable RTP-13D
5 Enable Active Disable RTP-13E
6
Enable
Not Applicable
Enable
RTP-13F
7
Enable
Inactive
Disable
RTP-13G
8
Enable
Not Applicable
Enable
RTP-13H
9 (Invalid) Invalid Invalid Invalid RTP-13K
AUTOMATIC CPA/OCPA-THD/OHD DEACTIVATION:
Inactive - Inhibits the automatic deactivation of CPA/THD functions when the
FMS position error is higher than the position accuracy required by the CPA/THD
functions. (Pilot monitors the position accuracy and manually inhibits the
CPA/THD function via the TERR OFF pushbutton - RTP-11E). Only GPWS
modes 1 to 5 remain active, TERR NOT AVAIL monitor output is set.
Active - Automatic deactivation of CPA/THD functions when the FMS position
error is higher than the position accuracy required by the CPA/THD functions.
(5) Alternate Alert Priority Management/Predictive Windshear Present/Bank Angle
Function. (See Table 4-23.)
Pub. No. 8600200-001, Revision 004
34-45-29
4-125
04 Nov 2014
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