A Cost-Effective Solution for Next Generation Flight Decks
Universal Avionics’ AHS-525 Attitude Heading Reference System (AHRS)
presents the superb reliability of Micro-Electromechanical Systems (MEMS)
technology needed to support NextGen flight decks. MEMS-based technology
combines the computational ability of microelectronics with the
acuity and control of micro-sensors and micro-accelerometers.
The AHS-525 contains multiple rate gyros to measure angular aircraft motion
in the pitch, roll and yaw axes and several accelerometers to measure aircraft
linear motion along the longitudinal, lateral and vertical axes of the aircraft.
This allows a single AHS-525 to replace multiple Line Replaceable Units
(LRU) found in a typical aircraft installation that would be performing the
same functions. Therefore, there is a reduction in the LRU footprint, weight,
wiring and power requirements.
A fixed mounting plate incorporating two precision alignment pins allows the unit to be easily removed for service and replaced without repeated and time-consuming system realignment and calibration. In addition, a straightforward calibration process reduces service time.
Incorporated into the AHS-525 is one “solid-state” main MEMS-based
component, using digital electronic subcomponents. In comparison
to older mechanical “spinning” gyroscopes, the MEMS-based AHS-525
produces a significant advantage in overall reliability.
The AHS-525 features digital, analog, discrete and synchro inputs and
outputs (I/O) to support a wide variety of interfaces on Part 23 and Part 25
Fixed Wing aircraft, and Part 27 and Part 29 Rotorcraft.
Simplifying retrofit installations, equating to significant installation and
operating cost savings, the AHS-525 is a clear choice for operators
seeking a cost-effective and reliable AHRS solution.
Micro-Electromechanical Systems (MEMS)-Based Technology
Increased Reliability Over Analog Directional and Vertical Gyros
Stable and Accurate Analog and Digital Pitch, Roll and Heading Measurements
A Multitude of Analog and Digital Outputs for Interface to Existing Avionics
Compact Size Lends Flexibility to Installation
Ease of Alignment Procedures
5.31 in. H x 5.25 in. W
(with Mounting Plate)
5.00 in. H x 5.25 in. W
(without Mounting Plate)
Depth: 8.65 in.
7.5 lbs. (with Mounting Plate)
6.5 lbs. (without Mounting Plate)
- Attitude Heading Reference Unit (AHRU)*
- Magnetic Sensing Unit (MSU) for magnetic heading data
- Attitude Heading Configuration Module (AHCM) to store configuration data
and alignment offset values
- AHRU Aircraft Mounting Plate that is permanently affixed to the aircraft
- Universal Avionics Electronic Flight Instrument System (EFIS) or
Discrete Inputs for Operator Control
*As with any AHRS installation, dual AHRU installation is required for Part 23 Class 3 and 4 and
Part 25 Fixed Wing aircraft. It is also required for Part 27 and Part 29 Rotorcraft AHRS installation.
3 ARINC 429 input ports
4 ARINC 429 output ports
1 RS-232 input/output port (bi-directional)
1 RS-485 input/output port (bi-directional) (MSU)
1 Input Manchester bus port
6 3-Wire Synchro output ports
4 2-Wire Synchro output ports (configurable)
6 Gnd/Open discrete input ports
1 Open/+28 VDC discrete input port
6 Open/+28 VDC discrete output ports
3 26 VAC 400 Hz Synchro Reference input ports
3 Analog DC differential output ports (configurable)
2 ±10 VDC Analog DC output ports (configurable)
2 2-Wire Analog DC input ports
Primary Input: 28 VDC standard
TSO-C3e: Turn and Slip Indicator Performance
TSO-C4c: Bank and Pitch Instruments
TSO-C6e: Direction Instrument, Magnetic (Gyroscopically Stabilized)
In accordance with the US/EU Bilateral Agreement on Cooperation In The Regulation of Civil Aviation Safety, Technical Implementation Procedure, IP Rev. 5, dated 15-Sep-2015 and signed by the EU Bilateral Oversight Board on 02-Mar-2016, Section 2.5.1 TSO/ETSO Articles Accepted under Reciprocal Acceptance (AHS-525), are qualified to be installed in EASA member states aircraft based on FAA TSO Authorization (TSOA).
The AHS-525 interfaces with several aircraft systems, including,
but not limited to, the following:
- Electronic Flight Instrument System (EFIS)
- Flight Data Recorder (FDR)
- Weather Radar
- Autopilot/Flight Director
- Enhanced Ground Proximity Warning System (EGPWS)
- Flight Management System (FMS)
- Air Data Computer (ADC)
- Terrain Awareness and Warning System (TAWS)
- Traffic and Collision Avoidance System (TCAS)
- Radio Magnetic Indicator (RMI)
- Attitude Direction Indicator (ADI)
- Horizontal Situation Indicator (HSI)