Flight
See Also: Flight Inspection, Avionics
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Wireless Electronic Flight Bags
webFB
The ultra-compact webFB easily fits in the palm of the hand, yet incorporates the capabilities of both an AID and a wireless server. The built-in AID safely gathers essential data from the aircraft's ARINC 429 and 717 databuses and conveys it to custom software or EFB apps hosted on the internal server. Using a wireless connection to portable EFB tablets, the webFB securely delivers this valuable information right to the fingertips of the flight crew.
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Distance Sensors
SICK has a wide range of optic and ultrasonic solutions that measure from sub-microns to kilometers. They solve measuring, detecting and positioning applications using triangulation and time-of-flight modes. Sensors using triangulation are ideal for short-range, highly precise measurement. They can inspect miniature parts, thickness and shape, etc. Time-of-flight sensors work at longer distances, are not influenced by reflectivity or ambient light − perfect for positioning AS/RS, rail cars and gantry cranes.
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AC Fuel Flow Signal Generator
TA-100
The TA-100 signal generator was designed to facilitate testing of aircraft fuel flow indicators that require two input signals designated as “Drum” and “Impeller”. This generator provides both signals so as to provide a direct interface to the fuel flow indicator under test. The generator also provides switched power out to the unit under test as well as a 5v source for testing the bezel lighting. The original design was built around the requirements for the AMETEK series indicators (pn: 10171 series). This generator simulates a reference and a time delayed signal of appropriate amplitude for an indication of up to 1200pph for the indicator under test. The “PPH Select” switch provides fixed signal delays representing 0, 200, 400, 800, 1000 and 1200pph flow rates respectively, this provides the mechanic with an expedient check of the indicators accuracy. The “PPH Adjust” control allows the mechanic to vary the signal delay throughout the full range and serves as a good method for checking of pointer smoothness from stop to stop. The unit’s front panel also provides test jacks to monitor the “FDR Output” as well as the drum and impeller signals. The TA-100 requires only 28Vdc to operate. This generator provides a very economical approach to any repair facility or flight department as it becomes an alternative to purchasing two bench top signal generators. The TA-100 generator at the very least can provide a simple functional test and eliminate the high cost of exchanging an indicator as a function of troubleshooting the aircraft system.
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Time-of-Flight Camera
The Basler Time-of-Flight (ToF) Camera provides high resolution 3D images at a very attractive price/performance ratio. It delivers 20 frames per second with VGA resolution and has a working range of 0 to 13 meters.
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Flight-Certifiable SBC
SBC314C
The SBC314C flight-certifiable single board computer is engineered in accordance with DO-178C and DO-254 and is available with supporting artifacts. It delivers great and proven performance thanks to the Power Architecture T2081 processor, and its diverse I/O set brings high functionality to the small form factor. The integrated XMC site allows even more connectivity, including high-density MIL-STD-1553 and ARINC 429 data bus communications as well as avionics discrete I/O through our RAR15CX flight-certifiable mezzanine.
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Airframe Mounted Gearboxes (AMAD)
Airframe mounted accessory drives (AMADs) — Every TRIUMPH Geared Solutions accessory drive is built to the highest standards of precision and reliability. The AMAD provides power for the aircraft’s hydraulic pumps, auxiliary fuel pumps and electrical generators. It also provides engine starting capability by transmitting power from auxiliary power units. Our AMADs incorporate carburized and ground gearing and, if the specification requires, AGMA Class 14 standards. Each drive is designed for high power density to minimize weight. Special features such as self-pressurizing lubrication systems assure proper operation at all altitudes within a given flight envelope. The AMADs also contain a disconnect feature which allows ground crews to disconnect the unit for maintenance and performance of electronic and hydraulic systems checks without the engine running.
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MCDU Simulator
Square Peg Communications Inc.
The Multi-Function Control and Display Unit (MCDU) is an input device for the flight management system and other computer systems of modern aircraft. It consists of a screen and an alphanumeric keyboard and can be found within reach of the pilot in the cockpit of the aircraft. The operation of the MCDU is described in the ARINC 739 specification.
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Digital Map Systems
Elbit Systems of America’s Global Digital Map Unit is built on a proven design that accommodates multiple data formats and provides unmatched situational awareness to aircrews. The GDMU displays detailed map, flight plan, and threat information to aircrews. Each system performs interactive functions with the mission computers and generates digital video map data for head down displays.
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Pitot Static Tester
ADSE 650
The ADSE 650 caters fully for all aircraft types and the different electrical power supplies.It can be used for testing high performance civil and military aircraft, fix and rotary wings. This Pitot Static Tester is designed primarily for flightline use to cover the testing of all barometric and manometric pressure instrument systems.The large touch screen display, with on-screen help ,enables all checks to be carried out easily on the flight deck or in the cockpit, by a single operator.
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SparkFun ToF Range Finder Sensor for VL6180
VL6180
This is the SparkFun "Time-of-Flight" Range Finder, a sensor board for the VL6180 distance sensor. Unlike most distance sensors that rely on reflected light intensity or reflected angles to determine range, the VL6180 uses a precise clock to measure the time it takes light to bounce back from a surface. This affords the ToF Range Finder and VL6180 a great benefit over other methods because it can be much more accurate and more immune to noise. Does this technology sound familiar? Well it should, it's the same means cellphones use to detect when the caller is holding their phone to their ear.
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One, Two, or Four Dual Redundant Interface MIL-STD-1553A/B Test & Simulation Module for PXI Express
PXIe-1553
Avionics Interface Technologies
1, 2, or 4 dual redundant MIL-STD-1553 bus interfaces Concurrent BC, multiple RT (31), and BM operations Full error injection and detection • Data capture filtering, 100% bus recording, and physical bus replay Multi-level Trigger for Capture/Filtering IRIG-B Time Encoder/Decoder Real-Time Recording and Physical Bus Replay Application interfaces supporting C, C++, C#, and .NET development Device Driver Support for: Windows, Linux, and LabVIEW Real Time (others provided on request) 10 high voltage (up to 30V) programmable DIO lines Flight Simulyzer GUI Analyzer software
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Dual Payload Drone Gimbal
FLIR XT2
The FLIR XT2 integrates a high-resolution FLIR thermal sensor and a 4K visual camera with a leading stabilization and machine intelligence technology to quickly transform aerial data into powerful insights. The advanced thermal sensor provides high sensitivity imaging for infrastructure monitoring, energy inspections, firefighting, search and rescue missions, and more. With a fully-integrated dual payload, professionals can now capture actionable thermal and color visible data in a single flight, saving time, money, and lives.
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GCxGC Time-of-Flight Mass Spectrometer
PEGASUS® BT 4D
The Pegasus BT 4D offers enhanced sensitivity by coupling our benchtop Pegasus BT with our high performance GCxGC thermal modulation system. This combination gives the Pegasus BT 4D the ability to interrogate challenging samples where the best sensitivity is needed. Unique and powerful software and hardware features simplify quantitation, while also dramatically making GCxGC easy to use and understand.
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MIL-STD-1553 Test & Simulation Interface for PCI Express
PCIe-C1553
Avionics Interface Technologies
Dual redundant, single, dual or quad stream configurationsSoftware selectable Transformer, Direct, and Bus Stub Coupling Modes - Concurrent Bus Controller, 31 Remote Terminals, & Bus monitor operation - Full error injection and detection - Multi-level triggers for capture and filtering - Ten high voltage (up from 30V) programmable DIO lines - IRIG-B time code encoder/decoder with free-wheeling mode - Real-Time recording and physical bus replay - x1 Lane PCI Express Host Interface (x4 Physical edge connector) - Application interface supporting C, C++, C#, and .NET development - Device driver support: Windows, Linux, LabVIEW Real-Time (others on request) - Compatible with AIT’s Flight Simulyzer GUI Bus Analyzer Software
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Weather Radar
Honeywell Aerospace Technologies
Weather has long been one of the biggest barriers to the success of a commercial flight or military mission. As weather patterns become increasingly unpredictable, pilots can rest assured knowing that Honeywell’s weather radar solutions will help them navigate the skies safely and efficiently in even the most hazardous conditions.
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TOFD Method of Acoustic Control
Time-of-flight diffraction method of acoustic control is a software and hardware suite used for material strength testing based on TOFD method of acoustic control.
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Aircraft SATCOM Antenna Integrations
SATCOM
Never miss a connection with Astronics AeroSat aircraft SATCOM antenna systems. Available for linefit or retrofit applications, these certified HTS-ready solutions have provided seamless inflight connectivity through millions of flight hours for more than a decade.
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Go No Go Testers
Go No Go Testers are developed in portable formats. Typically these are utilized at 'I' Level and 'O' Level test requirements and clear the aircraft LRU for flight.
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High-Power Flight Termination Systems
Kratos Defense & Security Solutions, Inc.
The Kratos Flight Termination System (FTS) is a turnkey system capable of transmitting MONITOR, ARM, and TERMINATE flight termination encoded command signals, as well as 20 individual IRIG tones (up to 6 simultaneously).
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Skylark I-LE Family
The Skylark I-LE leverages the heritage of the operationally-proven Skylark®1 Unmanned Aerial System (UAS) that is employed across the world by many coalition partners. The long endurance (LE) version of the Skylark extends the endurance of the system to approximately three hours. The system couples various gimballed payload options with proven flight control algorithms derived from the Hermes® 450 UAS to provide effective target detection, target tracking, and low operator workload for Intelligence, Surveillance, and Reconnaissance (ISR) missions. This portable Group 1 Small UAS (SUAS) offers capabilities that are normally found in larger unmanned systems.
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Altitude Test Chamber
Aircraft and its components are subject to extreme pressure and climatic conditions during flights. These parameters have a significant influence on the functioning of individual components, and they must be monitored and measured for safety reasons. CME Altitude chamber allow for the testing of aerospace components in an environment with controlled pressure, temperature and humidity parameters. An altitude of 100,000 feet [10 mbar] can be simulated in the test space.
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Data Monitoring System
1S663-001
The 1S663-001 Data Monitoring System was specifically developed for the Cessna Citation X and serves as the primary diagnostic tool for the aircraft?? electronic Logic Modules. The system is FAA certified for airborne operation. Aft compartment and cabin modules can be tested two at a time while remaining in place. The system is also capable of monitoring the fuel quantity system during flight.
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Rapid Evaporative Ionization Mass Spectrometry
REIMS
The innovative iKnife hand-held sampling device produces information-rich vapor directly from the surface of the sample, which when analyzed by a time of flight (Tof) MS, provides analysts with an accurate molecular profile in seconds.
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Flight Test Switches
Curtiss-Wright Defense Solutions
Our compact, deterministic flight test switches have been qualified to reliably deliver high-speed, real-time data with a wide temperature operation ranging from -40 to 85°C. Their rapid boot-up capability minimizes data loss from power outages, while their flexible forwarding and filtering configurations can send what is required to multiple destinations for real-time monitoring, recording, and transmission.
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Temperature & Pressure Switches
Pressure switches survive shock and vibration during all operating conditions and phases of flight and have been qualified to temperature conditions that exceed RTCA DC-160 requirements. Testing and design that goes above and beyond what is required has helped to make Measure Tech the "go to" manufacture when airlines need a new switch to help improve dispatch reliability.
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Pitot Static Tester / AoA TESTER
ADSE 744
This tester was specifically designed for the new-generation pitot tubes that integrate sensing probes, pressure sensors and powerful air data computer processing to provide all critical air data parameters including Pitot and static pressure, airspeed, altitude, and angle of attack. This Pitot Static tester is designed primarily for flightline use to cover the testing of all barometric and manometric pressure instrument systems. The AoA Channel behaves as a second Ps channel, in order to create a differential pressure between the 2 Ps Channel, allowing to performsimulations of different Angles of Attack. The large touch screen display, with on-screen help, enables all checks to be carried out easily on the flight deck or in the cockpit, by a single operator. The ADSE 744 is robust and housed in amobile weatherproof case. An attached bag contains the pressure hoses and electrical cables.
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Dynamic Gravity Meter
TAGS-7
TAGS-7 represents the latest development in a long line of LaCoste-based airborne gravity systems, stretching back to the first successful airborne gravity flights in 1958 and building on the success of the TAGS System. For over 50 years, LaCoste gravimeters have acquired hundreds of thousands of line kilometers of gravity data during academic, government, and commercial surveys. TAGS-7 blends the latest in GPS and data acquisition technology with the solid foundation of the LaCoste dynamic gravimeter.TAGS-7 is an upgrade to the TAGS-6 gravity meter, and is designed specifically for airborne operations. The system incorporates a time-tested, low-drift, zero-length-spring gravity sensor mounted on a gyro-stabilized gimbal platform. The sensor has a worldwide gravity measuring range (no reset necessary) of 500,000 milliGals.
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IEEE 1394b/AS5643 Mil1394 (FireWire), Triple-Node Multi-Port, Communications
FW3
The FW3 function module provides IEEE 1394b/AS5643 (Mil1394) support on each of its three nodes, which are configured as 2 nodes with 3-ports and 1 node with 2-ports. AS5643 defined flight ready robustness and active transformer isolation to enable longer cable lengths (20 meter) between nodes. Together these standards provide the deterministic and redundant communications protocol required for Vehicle System (Flight Control) Networks. The FW3 multiple ports per node configuration allows the user to create tree, daisy-chain and looped topologies needed to optimize cable length and weight while creating redundancy.
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Ultrasonic Gas Flow Sensor
GB Series
Panasonic Industrial Devices Sales Company of America
A compact, dual-function Ultrasonic Gas Flow Sensor that measures gas flow and gas concentration for flow rates from 1 to 25 Liters per minute. This Ultrasonic Gas Flow Sensor uses a unique time-of-flight design with an onboard processor to make highly accurate measurements of both gas flow and concentration. Suitable for use with many gases in an easy to implement format.





























