Rudder Bias Actuation System
1 / 1Pagine

Aggiungi ai preferiti

{{requestButtons}}

Estratti del catalogo

^—Rudder Bias Actuation System The Rudder Bias Actuator is a pneumatic actuator installed on the rudder control system of a business jet plane. In the event of an engine failure, the rudder bias actuators provide additional yaw control power to alleviate pilot effort. Each actuator is balanced at its neutral position using low pressure bleed air from each engine regulated by spool and sleeve valves. Operating Temperature:

Aprire il catalogo a pagina 1

Tutti i cataloghi e le schede tecniche FIMAC SPA

1. 

   FIAMC S.p.A. Presentation

   58 Pagine

2. 

   Liquid Cold Plate

   1 Pagine

3. 

   Integrated Auxiliary Power Unit and Cooling System

   1 Pagine

4. 

   ECU for Radar Rack Compartment

   1 Pagine

5. 

   Environmental Control Unit

   1 Pagine

6. 

   Rudder Bias Actuator

   1 Pagine

7. 

   Landing Gear Control Lever and Valve

   1 Pagine

8. 

   Pressure Switches

   1 Pagine

9. 

   Sprag Lock Valve

   1 Pagine

10. 

    Tail Shut-Off Valve

    1 Pagine

11. 

    Cabin Cooling System

    1 Pagine

12. 

    Krueger Flap Actuator

    1 Pagine

13. 

    In-Flight Refuelling Probe Selector Valve

    1 Pagine

14. 

    Hydraulic Shut-Off Valve

    1 Pagine

15. 

    Hydraulic Actuator

    1 Pagine

16. 

    Air Brake Actuator

    1 Pagine