
Landing Flap Lever
Functional Tester (FCT)
Based on the requirements of a leading aerospace manufacturer a functional test system for a landing flap lever was developed. The main objective of the application was the electrical and mechanical function testing including the position detection. In addition, the integrated corner sensor was selected and the absolute position of the lever checked.
Function Test example:
- Programmable AC Source: 115V / 400Hz
- Programmable DC Power Sources: 2x 0-35V, 0-8V 2x
- Fixed voltage sources 5V, 3.3V, 15V
- Central system power supply incl. emergency stop circuit as well as internal system supply voltages
- Multifunction DAQ (16-bit, 1.25 MS / s)
DUT (Device Under Test) Communication: ARINC 429
Other communication Interfaces supported: Arinc 615A Ethernet / AFDX, ARINC 664, MIL-STD-BUS 1553MIL, Fibre channel, HS1760 / MIL-STD-1760E, AS6802 Deterministic Ethernet