DESCRIPTION |
FEATURES |
SPECIFICATIONS |
DOCUMENTS |
VIDEO |
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DESCRIPTION
The **Cleveland Master Cylinder (A-049-8)** is a **genuine aircraft brake master cylinder** manufactured by Cleveland Wheels & Brakes for use within approved aircraft hydraulic braking systems. This master cylinder converts pilot brake pedal input into hydraulic pressure, enabling precise and reliable braking during landing, taxi and ground manoeuvring operations.
Designed for integration within aircraft rudder pedal brake systems, Cleveland master cylinders are engineered to provide consistent hydraulic actuation and dependable braking performance across approved aviation applications. This reservoir-type configuration incorporates an integrated fluid reservoir for hydraulic supply and pressure stability. Constructed from lightweight, high-strength materials, it is built for durability, long service life, and ease of maintenance in demanding operational environments.
*Images are representative and may not show the exact product for sale.*
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## Applications
- Provides controlled hydraulic braking for aircraft during landing and ground operations
- Installed within pilot and co-pilot rudder pedal brake control systems
- Suitable for use in approved aircraft hydraulic brake systems
- Used in aircraft brake maintenance, repair and overhaul (MRO) activities
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## Why CJ Aerospace?
CJ Aerospace supplies trusted Cleveland Wheels & Brakes brake components for aviation maintenance and overhaul.
We support operators and MROs with genuine parts, responsive service, and technical product understanding.
- 🇦🇺 **Australian-owned & operated**
- 📦 **Stocked locally in Australia for fast dispatch**
- 🔍 **Specialist knowledge of aviation wheels, brakes & hydraulics**
- 🧰 **Used by leading MROs & maintenance professionals**
> ✉️ [Contact us sales@cjaerospace.com.au](mailto:sales@cjaerospace.com.au)
> Need installation guidance or technical documentation? Contact CJ Aerospace for expert support.
FEATURES
- **Genuine Cleveland hydraulic master cylinder** for approved aircraft applications
- **Incorporates integrated hydraulic fluid reservoir for system supply and pressure stability**
- **Designed for integration with aircraft rudder pedal brake systems**
- **Compatible with standard aircraft hydraulic brake architectures**
- Engineered to support **routine inspection and overhaul**
SPECIFICATIONS
Package Dimensions
| Length | cm |
| Height | cm |
| Width | cm |
| Weight | |
Details
| **Specification** | **Detail** |
|----------------------------------------|-------------------------------------- |
| **Product Number** | A-049-8 (Alt P/N: 10-38) |
| **Component Type** | Master Cylinder Assembly |
| **Actuation Type** | Push-Type (Reservoir) |
| **Fluid Type** | MIL-PRF-5606 |
| **Bore Diameter** | Ø 0.625 inch |
| **Stroke** | 1.250 inch |
| **Rated Pressure** | 750 PSIG |
| **Typical Aircraft Application** | Piper Aircraft (PA-25-235, PA-25-260) Models |
| **Certification Type** | FAA-PMA Approved (Installed under aircraft Type Certificate) |
| **Manufacturer** | Cleveland Wheels & Brakes |
BROCHURES & DOCUMENTATIONS
List of Brochures
List of Documentation
Cleveland Hydraulics Assembly Catalog - AWBPC0001-25
Cleveland Application Chart
10-38 & 10-69_Cleveland Illustrated Parts List
VIDEO
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