Bell 212/412 Auxiliary Hydraulic System
The performance and dependability of the hydraulic system can dramatically improve the productivity of the aircraft. An integrated rotor braking system eliminates maintenance from the original disc style and provides smooth chatter-free braking with absolutely no pilot technique required. The system is certified to FAR 29 criteria and is eligible for use with the aircraft in standard category.
Bell 212/412 Auxiliary Hydraulic System
Model 35000, 35100, 35250
FAA STC SR01369SE
System Components and Features
- Hydraulic Pump Drive
- Reservoir
- Hydraulic Control Manifold
- Cockpit Controls
SPECIFICATIONS
MODEL 35000, 35100, 35250
Hydraulic Output…………………………………..up to 25 GPM
System Weight (dry)………………………………………84 LBS
Electric Requirements………………………….7 Amps @ 24 VDC
Hydraulic Oil………………………………………ISO 32 thru 68
KAWAK AVIATION TECHNOLOGIES QUALITY STATEMENT
All components designed and built to provide the utmost in reliability and longevity. Manufactured under FAA/PMA approved quality control system, your satisfaction is guaranteed.
