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Table of Contents
Related Manuals for uAvionix AV-20
Summary of Contents for uAvionix AV-20
- Page 1 AV-20 / AV-20-S Installation Manual UAV-1003613-001 Rev D...
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Page 2: Legal Notices
Warnings / Disclaimers uAvionix is not liable for damages arising from the use or misuse of this product. This equipment is classified by the United States Department of Commerce's Bureau of Industry and Security (BIS) as Export Control Classification Number (ECCN) 7A994. -
Page 3: Table Of Contents
10/03/2018 Updated for initial NORSEE certification, latest UI for Software Release 1.0. Updates from FAA Review. 11/24/2019 Release as uAvionix UAV-1003613-001 with updated device part numbers 11/18/2020 Remove pressurized aircraft limitation. Add guidance for OAT installation and AV-20 mounting. Update mechanical drawing. -
Page 4: System Description
1 System Description The uAvionix AV-20 and AV-20-S Multi-Function Displays provide a wide array of supplemental flight information. Features Include: • AoA Display (Voice Alerting & Peaks) • G-Meter Display (Voice Alerting & Peaks) • Attitude (Roll / Pitch) •... -
Page 5: Model Variants & Required Interfaces
2 Model Variants & Required Interfaces The AV-20 is available in two configurations: • AV-20 (Part Number UAV-1003591-001 or U-1001-0): The base model does not include internal inertial sensors or pitot-static sensors. Functions are limited to those indicated below. •... -
Page 6: Equipment Connections
This is provided for upgrade purposes and are plugged from the factory. Do not remove the plugs. Do not connect Pitot and Static in the AV-20 Base model units. Pitot and Static connections ARE required in the AV-20-S Model for proper functionality. -
Page 7: Manufacturing Port
No operational credit may be taken for installation of the system. The AV-20 and AV-20-S are limited to installation in Part 23, Class I and II aircraft. Installation in other categories of aircraft may require additional certification activities. -
Page 8: Operating Limits
4 Operating Limits The following operational limitations are applicable: Operating Limits Angle of Attack Range 0° to +30° Angle of Attack Resolution 1° Angle of Attack Operation +35 to +300 Knots Angle of Attack Accuracy 2.5° Density Alt Range (Accuracy) -1,000 to +25,000 Feet (±... -
Page 9: System Specifications
1000 cd/m Viewing Angle Left/Right 60° Viewing Angle Up 45° Viewing Angle Down 10° Backlight Lifetime (Typical) 50,000 Hrs Table 3 - System Specifications 6 Intended Function Reference the “AV-20 Pilot’s Guide” UAV-1003614-001 Section 2 for intended functionality. UAV-1003613-001 Rev D... -
Page 10: Installation
Mount the unit to the instrument panel with supplied screws • Apply power and perform setup Proper mounting orientation is important to ensure performance of the AV-20. Confirm the unit is oriented level in the roll-axis when installed in the panel. 7.2 Mechanical Drawing... -
Page 11: Wiring Diagram
7.3 Wiring Diagram IMPORTANT! CONNECT PITOT AND STATIC **ROTATING THE PLASTIC TUBE WHILE REMOVING WILL QUICK CONNECT: MINIMIZE RISK OF DAMAGING THE QUICK-CONNECT FITTING ** IN AV-20-S MODEL ONLY PUSH RELEASE RING IN TOWARD UNIT TO RELEASE AV-20 AIRCRAFT STATIC... -
Page 12: Setup
To Aircraft Ground Table 4 – Connector Pinout 7.4 Setup Refer to “AV-20 Pilot’s Guide” UAV-1003614-001 for detailed setup options and procedures. All options are available to the pilot to configure as desired. A summary of the options are as follows:... -
Page 13: Instructions For Continued Maintenance & Operation
The AV-20 system may be used for supplemental information but may not replace any equipment required under 14 CFR 91.205. • The AV-20 system is not a required system and may not be used as a substitution for the certificated aircraft system. •... - Page 14 o During power on, the ALIGNING mode on the Attitude Indicator page remains for more than 2 minutes. Note the Hard Calibration must be performed while not in flight, and with as little aircraft motion present. Preferred location is inside a hanger with doors closed. The aircraft does not need to be leveled prior to calibration.