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IM2830-AXS4
IM2830-AXS4M.DOC, DIR. 962830A-X-S-4
Shadin Avionics
Sec: VII
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
Page: i of vi
PAGE CONTROL CHART
SECTION
NO.
DESCRIPTION
PAGE
REVISION LOG
1.0
2.0
OVERVIEW
1-1
1.1
1.2
1.3
1.4
1.5
1-1
1-1
1-2
1-3
1-3
The Manual
Product Information
System Configuration
Fuel Totalizer Configuration
F/ADC2000, Argus Moving Map Configuration
FUEL AND AIR DATA SYSTEM SPECIFICATIONS
2-1
2.1
2.2
2-1
2-1
2.2
2-2
2-3
2-4
2-5
2-5
2-5
2-5
2-6
2.6
2-7
2-8
2-8
2-8
2-8
2-8
2-9
2-10
2-11
2-12
2-13
2-14
2-14
2-14
2-14
2-15
2-15
2-15
2-16
2-16
2.3
2.4
2.5
2.6
2.7
2.8
2.9
Input Data Range
Output Data Range
Table 1 – Calibrated Airspeed Tolerance
Table 2 – Pressure Altitude Tolerance
Table 3 – Vertical Speed Tolerance
Table 4 – MACH Tolerance
Dimensions
Power Requirements
Output Data
2.5.1 Serial Output Data Parameters
2.5.2 ARINC 429 (GAMA) Output Labels
Table 5 – ARINC Label Configuration
2.5.3 ARINC 429 Labels Associated with Switch Settings
2.5.4 Start-Up Temperature and Times for Output Data Valid
Limitations
2.6.1 Warm-up Time
2.6.2 Supplemental Equipment
2.6.3 Static/Pitot Source Error Correction (SSEC/PSEC)
2.6.4 SSEC/PSEC Listing
2.6.4 SSEC/PSEC Listing (Continued)
2.6.4 SSEC/PSEC Listing (Continued)
2.6.4 SSEC/PSEC Listing (Continued)
Part Numbering Scheme
Electrical Interface Specifications
2.8.1 Heading Interface
2.8.2 Fuel Flow Interfaces
2.8.2.1 Digital Fuel Flow
2.8.2.2 Sine Wave Fuel Flow
2.8.2.3 DC Voltage Fuel Flow
2.8.3 Baro Interface
Statistical Specifications
2.9.1 Mean Time Between Failures
3.0
CERTIFICATION
3-1
4.0
PLACING AN ORDER
4-1