Hydra has completed Safety of Flight testing for the 60H0037T temperature switch procured by Parker Hydraulics System Division. The switch is used for engine temperature monitoring on the Falcon F7X aircraft.

Hydra begins production deliveries of the 42H0002D delta P differential pressure switch used on the nitrogen-based fuel inerting system developed by Honeywell and Parker Aerospace. Certification has been achieved for the Boeing 747 aircraft with future Boeing commercial models also under consideration.

Hydra completes qualification testing and enters production deliveries of the 83550-2 hydraulic pressure switch. The switch is used on the thrust reverser system developed by Goodrich Actuation Systems and installed on the Bombardier CRJ700 aircraft.

Hydra begins deliveries of 2 pressure and 2 temperature switches for monitoring the main and auxiliary gear box transmission on the Dhruv Advanced Light Helicopter. The switches are procured by Hindustan Aeronautics Limited.

Hydra has entered qualification testing of the 15H0082PH hydraulic pressure switch used by Smiths Aerospace Mechanical Systems on the Airbus A380 LGERS (Landing Gear Extension Retraction System).

Hydra begins production deliveries of the 8H0025-1G low pressure fuel switch procured by the Goodrich Aerostructures Group for use on the CF34-10 nacelle.