mau - flight data · data to be transferred to a flight data recorder (fdr) or other avionics...

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WWW . FLIGHTDATA . AERO | AUSTRALIA | UNITED KINGDOM | USA MAU CAPABILITIES • Lightweight and compact • Modular hardware and software design • Software-defined data acquisition • Safety critical soft-core processor for customer loadable analysis software • Internal ambient temperature sensor • Aircraft-specific configuration • Data output via ARINC 717 and 429 • Flange mount in any attitude • Qualified to DO-160G and MIL-STD-810F / 461F / 704F • Internal, non-volatile memory Modular Acquisition Unit ANALOG AND DIGITAL DATA ACQUISITION AND PROCESSING FOR AIRCRAFT APPLICATIONS The MAU is an easily customizable data acquisition system designed for extremely harsh environments that gathers aircraft data to be transferred to a Flight Data Recorder (FDR) or other avionics systems on an aircraft. It is able to capture ARINC 429, ARINC 717 and MIL-STD-1553 digital data, as well as analog and discrete sensor inputs including synchros and LVDTs. The MAU provides 24 channels in the base module with 24 additional channels per expansion module. RS-422 data can also be acquired on an aircraft-specific basis. The MAU’s rugged aluminum flange-mount housing, along with MIL-DTL-38999 connectors, provides an environmentally-sealed enclosure that can be mounted in any attitude and is ideal for most operational settings. This includes both commercial and military fixed-wing and rotarywing aircraft. Because of its small size the MAU can be readily mounted on the airframe and does not require a pressurized location. Expansion of the MAU’s capabilities includes the following modules: • Expanded Data Acquisition with ARINC 717 and 429 output ARINC 717, ARINC 429 and MIL-STD-1553 inputs Analog/Discrete inputs • Pneumatic (Pitot-Static) • Quick Access Recorder (QAR) • GPS Splitter & Receiver Unit • Emergency Locator Transmitter • Wireless Data Transfer • Available 4.3-inch EMI-shielded touch screen LCD with optional NVG Class A capability Expansion modules for the MAU: GPS Splitter & Receiver Unit (left), expanded MAU with QAR (back), MAU with user interface (front) and expanded MAU (right)

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Page 1: MAU - Flight Data · data to be transferred to a Flight Data Recorder (FDR) or other avionics systems on an aircraft. It is able to capture ARINC 429, ARINC 717 and MIL-STD-1553 digital

w w w . f l i g h t d ata . a e r o | a u s t r a l i a | u n i t e d k i n g d o m | u s a

MAU

CAPABILITIES

• Lightweight and compact

• Modular hardware and software design

• Software-defined data acquisition

• Safety critical soft-core processor for customer loadable analysis software

• Internal ambient temperature sensor

• Aircraft-specific configuration

• Data output via ARINC 717 and 429

• Flange mount in any attitude

• Qualified to DO-160G and MIL-STD-810F / 461F / 704F

• Internal, non-volatile memory

Modular Acquisition Unit ANALOG AND DIGITAL DATA ACQUISITION AND PROCESSING FOR AIRCRAFT APPLICATIONS

The MAU is an easily customizable data acquisition system designed for extremely harsh environments that gathers aircraft data to be transferred to a Flight Data Recorder (FDR) or other avionics systems on an aircraft. It is able to capture ARINC 429, ARINC 717 and MIL-STD-1553 digital data, as well as analog and discrete sensor inputs including synchros and LVDTs. The MAU provides 24 channels in the base module with 24 additional channels per expansion module. RS-422 data can also be acquired on an aircraft-specific basis.

The MAU’s rugged aluminum flange-mount housing, along with MIL-DTL-38999 connectors, provides an environmentally-sealed enclosure that can be mounted in any attitude and is ideal for most operational settings. This includes both commercial and military fixed-wing and rotarywing aircraft. Because of its small size the MAU can be readily mounted on the airframe and does not require a pressurized location.

Expansion of the MAU’s capabilities includes the following modules:

• Expanded Data Acquisition with ARINC 717 and 429 output − ARINC 717, ARINC 429 and MIL-STD-1553 inputs − Analog/Discrete inputs

• Pneumatic (Pitot-Static)

• Quick Access Recorder (QAR)

• GPS Splitter & Receiver Unit

• Emergency Locator Transmitter

• Wireless Data Transfer

• Available 4.3-inch EMI-shielded touch screen LCD with optional NVG Class A capability

Expansion modules for the MAU: GPS Splitter & Receiver Unit (left), expanded MAU with QAR (back),

MAU with user interface (front) and expanded MAU (right)

Page 2: MAU - Flight Data · data to be transferred to a Flight Data Recorder (FDR) or other avionics systems on an aircraft. It is able to capture ARINC 429, ARINC 717 and MIL-STD-1553 digital

MAUModular Acquisition Unit

TYPE DESCRIPTION

Inputs (Up to 24 bit with ARINC 717, ARINC 429, MIL-STD-1553 2 megasamples/second Analogs, Discretes, Synchros, LVDT per channel) Remote Data Concentrator (RDC)

Outputs ARINC 429, ARINC 717

Additional Capabilities • Pneumatic (Pitot-Static) • Quick Access Recorder (QAR) • GPS receiver • Emergency locator transmitter • Wireless data transfer • 115 VAC, 400 Hz power • Available 4.3-inch EMI-shielded touch screen LCD with optional NVG Class A capability • Internal, non-volatile memory (up to 64 GB)

Physical Dimensions (inches): 1.4 in. H (min) x 3.9 in. D x 4.6 in. W Dimensions (millimeters): 35mm H (min) x 100mm D x 115mm W Weight: 1.5 lb. nom.

Power Input Power: 28 VDC Consumption: 5 W

Main Connector MIL-C-38999 Series II, 66-pin

Environmental (D0-160G & MIL-STD-810F / 461F / 704F) Operating Temperature: -55 ˚C to 70 ˚C Non-operating Temperature: -55 ˚C to 85 ˚C Humidity: 100% Operational Altitude: 55,000 ft. Operational Shock: 20 g Vibration: 14 g EMI/EMC: DO-160G, MIL-STD-461F / 704F Reliability: > 12,000 operating hrs. MTBF Cooling: Passive convection

Australia | 31 McGregors Drive, Keilor Park, Victoria 3042, Australia | Phone: +61.3.8331.2900 | Fax: +61.3.9336.1758

UK | Building 9, Britannia Court, The Green, West Drayton, Middlesex UB7 7PN, United Kingdom | Phone: +44.0.2035401777

USA | 6497 Parkland Drive, Suite J, Sarasota FL 34243, USA | Phone: +941.756.9394

www.flightdata.aero | Email: [email protected]

Data, including specif icat ions, contained within this document are summary in nature and subject to change at any t ime without notice at Fl ight Data Systems’ discret ion. Cal l for latest revis ion. Al l brand names and product names referenced are trademarks, registered trademarks, or trade names of their respective holders. Rev 11/17

Flight Data Systems

A V I AT I O N P R O D U C T S & S E R V I C E S F O R C O M M E R C I A L & M I L I TA R Y 2 9 - 0 0 0 2 I s s u e A

SPEC IF ICAT IONS

Quick Access Data Recorder (QAR)

Expanded signal acquistion capability (24 channels per module)

Base module

3.5 in.90.0 mm

4.6 in.118.0 mm

0

0.3 in.8.0 mm

0.8 in.21.3 mm

1.6 in.41.5 mm

0.

15 in

.3.

8 m

m

4.1 in.104.1 mm

0.

4 in

.10

.2 m

m

2.

4 in

.59

.7 m

m

CENTER OF GRAVITY

MAU Dimensions

Top View

Front View

ARINC 429

ARINC 717

GPS

Pitot-Static

Analog & Discretes

MIL-STD-1553

ARINC 429

ARINC 717

QAR

Wireless QAR

MAU

MAU Functional System Block DiagramInputs Outputs