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A33369 - Safran Landing Systems Wear Indicator

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A33369 – Safran Landing Systems Wear Indicator

Available now through the AirParts Aero marketplace.

Overview Section

The Safran Landing Systems A33369 is a high-precision Brake Wear Indicator (also referred to as a "Wear Index" or "Wear Pin") engineered specifically for the carbon brake assemblies of the Airbus A320 family. Manufactured by Safran—the world leader in aircraft landing and braking systems—this component is a vital maintenance tool that provides a direct visual or electronic measurement of the remaining thickness of the carbon brake disc stack.

The A33369 is a hollow steel rod (hollow rod design) that protrudes through the brake’s torque plate or housing. As the carbon discs wear down during repeated landing and taxi cycles, the indicator pin moves or retreats relative to a reference point. This allows ground crews and maintenance technicians to accurately determine the service life of the brake assembly without requiring a full disassembly of the landing gear.

Key Features Section

  • Steel Hollow Rod Construction: Fabricated from high-strength, corrosion-resistant steel to ensure structural integrity in the extreme thermal environment of an aircraft brake (where temperatures can exceed 800°C).

  • OEM Accuracy: Designed by the Original Equipment Manufacturer (Safran/Messier-Bugatti-Dowty) to match the specific wear limits and certification standards of the Airbus A320 series.

  • Proximity Sensor Compatibility: Engineered to interface with modern brake monitoring systems, allowing for precise measurements that can be relayed to the cockpit or maintenance computers.

  • "Check-at-a-Glance" Design: Provides an immediate visual indicator for pre-flight and post-flight inspections, ensuring the aircraft remains compliant with Minimum Equipment List (MEL) requirements.

  • Corrosion Resistance: Specially treated to resist the de-icing fluids and atmospheric moisture common in commercial aviation hub operations.

  • Lightweight Efficiency: Weighing approximately 0.6 kg, this pin is optimized to contribute to the overall weight-reduction goals of modern fuel-efficient narrow-body aircraft.

Technical Specifications Section

SpecificationDetail
Part NumberA33369
ManufacturerSafran Landing Systems (formerly Messier-Bugatti-Dowty)
Component TypeBrake Wear Indicator / Wear Index
MaterialHigh-Grade Stainless Steel
GeometryHollow Rod / Pin
Aircraft CompatibilityAirbus A320 Family (A318, A319, A320, A321)
Weight0.6 kg (Approx. 1.32 lbs)
CertificationEASA Form 1 / FAA 8130-3 (Revision dependent)

Aircraft Compatibility Section

The A33369 is the standard wear indicator for the global fleet of Airbus A320 aircraft, a staple of the AirParts Aero commercial inventory:

  • Airbus A320ceo/neo: Used across both the Current Engine Option and New Engine Option variants for brake monitoring.

  • Airbus A319/A321: Essential for the varied fleet configurations of short-to-medium haul operators.

  • Commercial Civil Aviation: Directly listed as a maintenance part for A320 series civil aviation aircraft globally.

Technical Applications & Safety

The brake wear indicator is the "fuel gauge" for your stopping power. In the high-cycle environment of an A320, the carbon heat sink (the disc stack) gradually oxidizes and wears away with every application of the pedals. The A33369 ensures that the brake is never operated beyond its minimum certified thickness.

Safety Warning: A brake stack that is worn past the limit indicated by the A33369 may not have sufficient thermal mass to absorb the energy of a Maximum Weight Rejected Takeoff (RTO). If the pin is flush with the reference housing, the brake assembly must be removed for overhaul or replacement immediately to prevent a total loss of braking authority or a catastrophic brake fire.

Technical Engineering Insight

The engineering excellence of the Safran A33369 lies in its Thermal Expansion Management. Carbon brakes can fluctuate from freezing temperatures at cruise to white-hot during heavy braking. The A33369 is manufactured with a coefficient of thermal expansion that prevents the pin from "seizing" or binding in the brake housing, which would otherwise provide a false "safe" reading to the maintenance crew.

The Hollow Rod design is not only a weight-saving measure; it also serves to isolate the measurement pin from the extreme heat of the disc stack, protecting any electronic proximity switches it may interface with. By choosing the genuine Safran A33369 through AirParts Aero, you ensure that your A320 fleet maintains the "Brake Life" accuracy required for computerized maintenance tracking and EASA-compliant flight operations.

Installation & Maintenance Addendum

  1. Measurement Check: Wear should only be measured when the parking brake is SET (pressurized), as the disc stack must be compressed to provide an accurate reading.

  2. Surface Inspection: Ensure the indicator pin moves freely. If the pin is bent or covered in excessive carbon dust, it should be cleaned or replaced to prevent "hung" readings.

  3. Proximity Calibration: If the aircraft is equipped with an electronic Brake Wear Monitoring System, ensure the computer is reset and calibrated to the new pin's position during brake replacement.