Garmin GTX 335, GTX 345R, GTX 330, GTX 33, GTX 345 User manual

GENE
AIRCRAFT SPECIFIC INFORMATION
RAL INFORMATION
Date: / / By:
AIRCRAFT MAKE:
AIRCRAFT MODEL:
AIRCRAFT SERIAL #:
AIRCRAFT REG. #:
HEX ADDRESS:
GTX #1
Unit P/N:
Mod Level:
Unit Model:
Serial #:
GTX #2 [N/A]
Unit P/N:
Mod Level:
Unit Model:
Serial #:
Rev. 7
GTX 33X and GTX 3X5 ADS-B Maintenance Manual190-00734-11
Page A-2
ELECTRICAL LOAD ANALYSIS
ITEMS REMOVED FROM AIRCRAFT
ELECTRICAL LOAD (A) [1]
COMMENT
Subtotal:
ITEMS ADDED TO AIRCRAFT
ELECTRICAL LOAD (A) [1]
COMMENT
Subtotal
Net Change in Bus Load:
[1] Use typical current draw when performing this calculation.
Rev. 7
GTX 33X and GTX 3X5 ADS-B Maintenance Manual190-00734-11
Page A-3
EQUIPMENT INTERFACED TO THE GTX
Document the equipment which is interfaced to the GTX. Use the following guidance when filling out the information.
GTX #1 INTERFACED EQUIPMENT
Audio Panel
Model:
GTX Port Number:
Display
Model:
GTX Port Number:
Altitude Encoder
Model:
GTX Port Number:
GPS #1
Model:
GTX Port Number:
GPS #2
Model:
GTX Port Number:
Heading
Model:
GTX Port Number:
Air Data
Model:
GTX Port Number:
Model(s): Write in the model number or numbers of the equipment which is interfaced to the GTX.
GTX Port Numbers:When applicable, write in the GTX port number or numbers used for the interface.
This column is generally applicable only to serial ports such as RS-232 and ARINC 429.
NOTE
This information is optional and is not required to be completed or maintained with the aircraft records.
7UDIILF
Model:
GTX Port Number:
*'/
Model:
GTX Port Number:
Rev. 7
GTX 33X and GTX 3X5 ADS-B Maintenance Manual190-00734-11
Page A-4
GTX #2 INTERFACED EQUIPMENT
Audio Panel
Model:
GTX Port Number:
Display
Model:
GTX Port Number:
Altitude Encoder
Model:
GTX Port Number:
GPS #1
Model:
GTX Port Number:
GPS #2
Model:
GTX Port Number:
Heading
Model:
GTX Port Number:
Air Data
Model:
GTX Port Number:
7UDIILF
Model:
GTX Port Number:
*'/
Model:
GTX Port Number:
Rev. 7
GTX 33X and GTX 3X5 ADS-B Maintenance Manual190-00734-11
Page A-5
Wire Routing
Single Engine
The following diagram depicts approximate location of all LRUs along with the wire routing for the GTX throughout the aircraft structure for a single-engine aircraft.
Rev. 7
GTX 33X and GTX 3X5 ADS-B Maintenance Manual190-00734-11
Page A-6
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