uAvionix AV-30-S Manuale utente
UAV-1003947-001, AV-30-C, Installation Manual 1 Revision C
AV-30-C
Installation Manual
UAV-1003947-001, AV-30-C, Installation Manual 2 Revision C
© 2020 uAvionix Corporation. All rights reserved.
Except as expressly provided herein, no part of this guide may be
reproduced, transmitted, disseminated, downloaded or stored in any
storage medium, for any purpose without the express written permission
of uAvionix. uAvionix grants permissions to download a single copy of
this guide onto an electronic storage medium to be viewed for personal
use, provided that the complete text of this copyright notice is retained.
Unauthorized commercial distribution of this manual or any revision
hereto is strictly prohibited.
uAvionix® and Ping® are registered trademarks of uAvionix Corporation
and may not be used without express permission of uAvionix.
AV-30, AV-30-E, and AV-30-C are trademarks of uAvionix Corporation
and may not be used without express permission of uAvionix.
Patent uavionix.com/patents
UAV-1003947-001, AV-30-C, Installation Manual 3 Revision C
1 Revision History
Revision Date Comments
A 4/24/2020 Initial release
B 7/13/2020
Added installation log-book entry requirement.
Added method to determine proper screw
length. Highlighted primary functions. Added
items included in the ICA. Added startup time
and AoA reference per MOPS requirement.
Added reference to CFR 23.1321.
C 8/10/2020
Added reference to AoA operation in inverted
flight and operation in excess of G limits.
Added reference to utilize wire type in
accordance with
AC 43.13
-
1B
.
UAV-1003947-001, AV-30-C, Installation Manual 4 Revision C
2 Warnings / Disclaimers
All device operational procedures must be learned on the ground.
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.
These items are controlled by the U.S. Government and authorized for
export only to the country of ultimate destination for use by the ultimate
consignee or end-user(s) herein identified. They may not be resold,
transferred, or otherwise disposed of, to any other country or to any
person other than the authorized ultimate consignee or end-user(s),
either in their original form or after being incorporated into other items,
without first obtaining approval from the U.S. government or as otherwise
authorized by U.S. law and regulations.
UAV-1003947-001, AV-30-C, Installation Manual 5 Revision C
3 Table of Contents
1 Revision History .............................................................................. 3
2 Warnings / Disclaimers .................................................................... 4
3 Table of Contents ............................................................................ 5
4 AV-30-C System Information ........................................................... 7
4.1 System Description .................................................................... 7
4.2 System Functions ...................................................................... 9
4.3 System Specifications .............................................................. 10
5 Certification ................................................................................... 11
5.1 Mechanical Instrument Replacement ....................................... 12
5.2 Non-Required Instrument Addition ........................................... 12
5.3 Vacuum System Removal ........................................................ 12
5.4 Applicable Performance Standards .......................................... 13
6 Installation Limitations ................................................................... 14
6.1 Installation Approval Limitations ............................................... 14
7 Installation Locations & Operating Modes ..................................... 15
7.1 Installation Locations ............................................................... 15
7.2 Operating Mode Configuration ................................................. 16
8 Functionality and Required Interfaces ........................................... 17
8.1 Aircraft Systems Connections .................................................. 17
8.2 Feature Matrix ......................................................................... 18
8.2.1 Power Input (Required) ...................................................... 19
8.2.2 Pitot and Static Interfaces (Required/Optional) .................. 19
8.2.3 Outside Air Temp Input (Optional) ...................................... 19
8.2.4 Audio Output (Optional) ..................................................... 20
8.2.5 GPS Interface (Optional) .................................................... 20
8.3 Internal Battery Operation ........................................................ 21
8.3.1 General .............................................................................. 21
9 Equipment Installation ................................................................... 22
9.1 Overview .................................................................................. 22
9.2 Supplied Components ............................................................. 22
9.3 Non-Supplied Components ...................................................... 22
9.4 Installation Records ................................................................. 22
9.5 Mechanical Drawing ................................................................ 23
9.6 Mounting Screw Length Restriction ......................................... 24
9.7 Wiring Diagrams ...................................................................... 25
UAV-1003947-001, AV-30-C, Installation Manual 6 Revision C
9.8 Bonding Requirements ............................................................ 27
9.9 Unit Pinout ............................................................................... 28
10 Setup & Configuration ................................................................ 29
10.1 Startup and Common Controls ........................................... 29
10.2 Available Menus................................................................. 30
10.3 Install Menu Activation ....................................................... 31
10.4 Install Menu Settings .......................................................... 32
10.5 Mandatory Settings ............................................................ 33
10.5.1 Unit Function ................................................................. 33
10.5.2 Function Lock ................................................................ 33
10.5.3 Trims ............................................................................. 33
10.5.4 V-Speeds ...................................................................... 33
10.5.5 Display Units ................................................................. 34
10.5.6 Serial Inputs .................................................................. 34
10.5.7 Demo Mode ................................................................... 34
10.6 System Checkout ............................................................... 34
10.6.1 Alignment ...................................................................... 34
10.6.2 OAT Interface ................................................................ 35
10.6.3 GPS Navigator Interface ................................................ 35
10.6.4 EMC Checkout .............................................................. 36
11 Troubleshooting ......................................................................... 38
12 Instructions for Continued Maintenance & Operation ................. 39
13 Aircraft Flight Manual Supplements............................................ 39
14 Serial Interface Specification ...................................................... 40
15 Field Update Capability .............................................................. 41
UAV-1003947-001, AV-30-C, Installation Manual 7 Revision C
4 AV-30-C System Information
4.1 System Description
The uAvionix AV-30-C is a fully digital multi-mode instrument that
mounts in the legacy 3 1/8” round instrument panel. It can be field
configured as either an Attitude Indicator (AI) or a Directional Gyro
(DG) indicator. It is fully self-contained with dual-precision inertial and
pressure sensors and allows for a wide variety of pilot customization.
Figure 1 - AV-30-C Multi Mode AI/DG – Basic Display
When configured as an AI, primary attitude and slip are always
displayed. The un-used portions of the display area can be customized
by the pilot to show a variety of textual and graphical data-overlay
fields. Three pages may be customized by the pilot while a fourth page
presents a fully decluttered view of only attitude and slip.
When configured as a Directional Gyro (DG), direction of flight
information is presented. The flight direction can be configured to be
presented as non-slaved heading or inertially stabilized GPS track
when connected to an external GPS navigator. Multiple display
presentations, including compass rose, GPS HSI, and GPS Arc views
can be selected by the pilot. The un-used portions of the display area
can similarly be configured for a variety of textual data-overlays.
In both operating modes, the pilot may select from multiple visual styles
which are intended to improve visual compatibility with legacy aircraft
UAV-1003947-001, AV-30-C, Installation Manual 8 Revision C
instrumentation and preserve the look-and-feel of older aircraft
applications.
A wide variety of supplemental functions, including audio alerting,
derived angle of attack presentation, g-load display, and more are
provided. An internal, rechargeable LiPo battery allows for operation
for a nominal 2 hours in the event of aircraft power loss and 30 minutes
minimum under all temperature conditions.
See UAV-1003946-001, AV-30-C, Pilot’s Guide for detailed
functionality.
UAV-1003947-001, AV-30-C, Installation Manual 9 Revision C
4.2 System Functions
Primary Functions:
- Primary Attitude (AI Mode)
- Primary Slip (AI Mode)
- Primary Direction of Flight Indication (DG Mode)
Supplemental Functions:
- Indicated Airspeed
- Altitude
- V-Speeds
- Angle Of Attack
- Vertical Trend
- Vertical Speed
- Set Altitude
- Heading
- Bus Voltage
- G Load
- Outside Air Temp
- True Airspeed
- Density Altitude
- GPS Navigator / Waypoint Data
- GPS Navigator Nav Data
- GPS Navigator Route Line
- Heading Bug
Audio and Visual Alerting Functions:
- AoA Alerting
- G Limit Alerting
- Excessive Roll Alerting
Misc. Functions:
- Internal Battery Operation
- Auto / Manual Brightness
UAV-1003947-001, AV-30-C, Installation Manual 10 Revision C
4.3 System Specifications
Electrical Attributes
Input Voltage Nominal +10 to +32 VDC
Input Voltage Max +60 VDC
Input Power Nominal 6 Watts (0.5 Amps @ 12VDC)
Input Power Max 12 Watts (1.0 Amps @ 12VDC)
Required Circuit Breaker 2 Amp
Operation on Battery 2 Hrs Typ @ 20°C / 30 Min Minimum @ -20C
Physical Attributes
Mounting Configuration 3 1/8” Round Instrument Hole
Dimensions wo/Connector 3.38 x 3.38 x 1.6 Inches
Weight 0.56 Lbs.
Electrical Connector 15 Pin Male D-Sub
Pneumatic Connectors ¼” OD Quick Connect
Mounting (4X) #6-32 Machine Screws
Case Material Billet Aluminum
Environmental
Ground Survival Low -55°C
Operating Low -20°C
Ground Survival High +85°C
Operating High +55°C
Startup Time < 3 Minutes
Altitude 25,000 Feet Max
Optical Characteristics
Diagonal Size 3” Circular
Contrast Ratio (Typical) 500
Brightness (Typical) 1000 cd/m2
Viewing Angle Left/Right 60°
Viewing Angle Up 45°
Viewing Angle Down 10°
Backlight Lifetime (Typical) 50,000 Hrs
Table 1 - System Specifications
Indice
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