FreeFlight 2101 I/O Approach Plus GPS Navigation System
1.3
TECHNICAL CHARACTERISTICS
1.3.1
Receiver/Display Units (P/N 81440-XX)
ENVIRONMENTAL COMPLIANCE
TSO COMPLIANCE
PHYSICAL DIMENSIONS
Height
Width
Depth
WEIGHT
TEMPERATURE
Navigation Unit
Database Card
ALTITUDE
MAXIMUM TRACK VELOCITY
MOUNTING
POWER REQUIREMENTS
External Interfaces:
TYPE
Synchro
Voltage Ratio
ARINC 429
Discrete
Synchro
Autopilot
Analog Deviation
Digital ARINC
Discrete Output
Serial
Page 1-4
* Complies with USA export requirements
I/O
NO.
Input
4
Input
1
Input
4
Input
9
Output
3
Output
1
Output
3
Output
3
Output
15
Input/Output
3
See Appendix A
C129 (A1)
3.0 in (7.62 cm)
5.70 in (14.48 cm)
7.68 in (19.50 cm)
3.25 lbs (1.48 kg)
-20° to +70° C
0° to +55° C
-1000 ft to +50,000 ft
800 knots*
Dzus Rail
1.5 A @ 28 Vdc
PARAMETER
TAS
HDG
Altitude (2)
TAS
High or Low Speed
Various, including Spares
Programmable Synchro/Resolver Output
Roll Sum Steering
Cross Track
Glideslope
Autopilot Left/Right
419/429 (2)
561/568 (1)
Various, including Spares
Differential GPS
Air Data Computer
Test and Maintenance
Altitude Encoder
Data Logging
Revision E
May 31, 2006
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