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IM2830-AXS4M.DOC
IM2830-AXS4
DIRECTORY: 962830A-X-S-4
Shadin Avionics
INSTALLATION MANUAL
FUEL/AIR DATA COMPUTER
P/N 962830A-X-S-4, 962830A-1-S-4, 962830A-2-S-4, 962830A-3-S-4
Rev: M
2.3
Page: 2-5
Dimensions (including mounting rack)
Size: 7.4" L x 4.3" H x 3.9" W
Weight: 36 oz.
2.4
Power Requirements
System Power required:
2.5
28 VDC @ 1300 mA
14 VDC @ 900 mA
Output Data
1. Electric Format: RS-422 or RS-232
2. ARINC 429 low/high speed GAMA (Has to be configured at the factory)
See paragraph 2.5.3 for ARINC 429 output data capabilities.
2.5.1
Serial Output Data Parameters
Fuel Group
L. ENG. Fuel Flow
R. ENG. Fuel Flow
Fuel Used Total
Total Fuel Used
Fuel Used L. ENG.
Fuel Used R. ENG.
Fuel Remaining
NM/Fuel Unit (ground)
Fuel to Destination
Fuel at Destination
AIR DATA Group
Pressure Altitude (PALT)
Density Altitude
Barometric Corrected Altitude
Indicated Air Speed (IAS)
True Air Speed (TAS)
Vertical Speed
True Air Temperature (TAT)
Outside Air Temperature (OAT)
Drift Angle
Magnetic Heading
Rate of Turn
MACH Number
Wind Direction and Speed
Baro Correction (mb #1)
Baro Correction (hg”)
Note: Not all parameters will be available to all navigational receivers. Contact the manufacturer for display
capabilities.