Aircraft Hydraulic Power Control
The AP09V-1-05 Hydraulic Pump is a high-performance, aircraft-grade hydraulic power unit designed to provide consistent pressure and fluid flow for flight control systems, landing gear, brakes, and other hydraulically actuated aircraft components. Known for its durability and efficiency, this pump is ideal for both OEM installations and aftermarket replacements.
Part Number: AP09V-1-05
Functions & Key Features:
- Hydraulic Power Supply: Provides pressure for flight control, gear, brake, and utility systems
- Precision Engineering: Built for consistent output under variable load conditions
- Compact & Lightweight Design: Ideal for space-constrained airframe installations
- High Reliability: Designed for extended service intervals and rugged flight environments
- OEM-Compliant Build: Meets aerospace performance and certification standards
Applications:
- Fixed-wing and rotary-wing aircraft requiring onboard hydraulic power
- Primary or backup hydraulic system use
- Commercial, general aviation, and military aircraft platforms
Typical systems powered by this pump include:
- Flight control actuators
- Landing gear extension/retraction
- Brake systems and steering
- Cargo door or ramp actuation systems
Actual aircraft applicability depends on model configuration and certification.
PAG Support:
We provide full support for the AP09V-1-05 Hydraulic Pump through:
- OEM-authorized sales, exchange units, and repairs
- In-house hydraulic system test and overhaul capabilities
- Component tracking and traceability
- FAA/EASA/TCCA certified maintenance
- AOG support and worldwide logistics services
- Decades of experience in aircraft hydraulic systems
PAG ensures high availability and reliable turnaround times to minimize aircraft downtime.
Contact Us for Related Parts & Compatible Components:
- AP09V-1-06 – Alternate configuration of hydraulic pump
- 2008131-1 – Hydraulic reservoir or accumulator
- 407-075-002-107 – Hydraulic actuator assembly
- 41011300-105 – Tail Rotor Servo (T/R Hydraulic Servo)
- 406-010-413-137 – Pitch Link (flight control connection)
- Servo Test Benches – For pump and actuator functional validation
