Maintenance and Diagnostics for Aerospace Systems
The O-level tester verifies the status of weapon stations on the A-10C PE aircraft using discrete data acquisition and through the MIL-STD-1760 bus.
SwRI developed TPS for the IFFCC central processing unit, voice message unit, symbol generator/stroker, A/D-D/A, Command A, Command B, Discrete 1, Discrete 2, Heading, and 1553B R/T circuit card assemblies.
SwRI developed this depot power supply tester for F-15 aircraft support equipment.
This lightweight, ruggedized hand-held device acts as a remote terminal to download enhanced engine data used by the A-10 Engine Structural Integrity Program.
Complex, cutting-edge aerospace systems require innovative maintenance and diagnostic technologies. Southwest Research Institute (SwRI) develops diagnostic equipment to support all levels of the maintenance process, including
- Large, specialized, ground-based automatic test equipment
- On-board, built-in test systems
SwRI engineers are experienced in the philosophy and use of numerous standards related to the development of electronic test equipment. In some cases, staff members examine reliability and maintainability problems and redesign the system, subsystem or component causing problems.
Tester and Support Equipment Development
- New workload support
- Correction of deficiencies (CND/RTOK)
- Elimination of obsolescence
- Test Program Set (TPS) development or rehosting
- Interface Test Adapter (ITA) development
- Instrument upgrade
- Test stand development/integration
Sample Maintenance and Diagnostics Projects
- A-10 flightline tester
- Depot-level tester for the Integrated Flight and Fire Control Computer (IFFCC)
- IFFCC SRU tester
- F-15 power supplies TPS
- C-5B MADARS
- DTS Rehost
- AIS upgrade for F-16 RSU
- F-15 MSIP TPS
- Gyro ATE upgrades
- Gyro manual tester replacement
Staff members are experienced in the philosophy and use of numerous standards related to the development of electronic test equipment. In some cases, SwRI examines reliability and maintainability problems and may redesign the system, subsystem, or component causing problems.
Engineers developed an operational-level (O-level) tester to provide troubleshooting and diagnostic capabilities for maintenance on the integrated avionics and weapons systems, subsystems and sensors for the A-10A and the A-10C precision engagement (PE) modified aircraft. The O-level tester provides system-level troubleshooting of the line replaceable units (LRU) connected to the MIL-STD-1553B avionics bus, RS-232 and Ethernet. The tester consists of the portable automated test station (PATS) hardware and the operational test program (OTP) software. The O-level tester has the capability to verify the status of weapon stations on the A-10C PE aircraft using discrete data acquisition and through the MIL-STD-1760 bus.
SwRI developed test program sets for the IFFCC central processing unit, Voice Message Unit, Symbol Generator/Stroker, A/D-D/A, Command A, Command B, Discrete 1, Discrete 2, Heading, and 1553B R/T circuit card assemblies. SwRI performed detailed circuit analysis and developed full Test Requirements Documents (TRD) along with detailed Interface Test Adapter (ITA) designs that were approved by the government. The TPS software and ITAs were hosted on the Teradyne Spectrum 9100 test stand.
A lightweight, ruggedized hand-held device acts as a remote terminal (RT) to download enhanced engine data used by the A-10 Engine Structural Integrity Program (ESIP) via the MIL-STD-1553B avionics bus. Equipped with a 5-gigabyte hard drive, Windows CE® operating system, and a touch-screen LCD display, this mobile device enhances efficiency on the flightline while reducing the support equipment footprint.
aerospace systems maintenance •
systems diagnostics techniques •
diagnostic equipment • automatic test equipment • build-in test systems •
electronic test equipment