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11-17

Utility actuators are used for the movement of structures that do not require precise mid-position control, while still providing reliability and safety features.

Full Product Description

Utility actuators are devices used to control motion of specific aircraft parts. They are commonly used for cabin, cargo and landing gear doors but are also used for retractable stairs, engine tans-cowl doors and landing gear steering and retraction. We can design, manufacture, and validate an actuator from basic hydraulic actuators to locking actuators with electronic feedback.

APPLICATIONS

General and business aviation, and turboprop passenger

FEATURES AND ATTRIBUTES

  • Complete system solutions available
  • Mature designs in use on the world’s most active fleets

OPTIONAL FEATURES

  • Extend and retract-rate controls
  • Alternate emergency pneumatic actuation
  • Single-stage or telescoping
  • Thermal-volume change compensation
  • End-of-stroke snubbing
  • Position locks
  • Hydraulic or pneumatic power sources

Technical Specifications

Bore Diameter: Ø 1.179 IN
Certification Type: FAA-PMA Approved / Installed under aircraft Type Certificate
Fluid Type: MIL-PRF-5606
Operating Temperature Range: -40 °F (-40 °C) to 160 °F (71 °C)
Stroke: 4.990 IN
Platform*: Piper Aircraft (PA-32R-301T)* For reference only. To validate applicability, see “Find by Aircraft“.