APS - BRAKE LININGS - APS66-06200
FAA-PMA Part
Description: BRAKE LININGS
Part number: APS66-06200
OEM: Parker Hannifin Corp
OEM part number: 066-06200
FAA-PMA Eligibility: [ Click Here ]
APS BlackSteel offers semi-metallic (organic) and metallic linings for your specific application. The semi-metallic linings are impregnated with Kevlar® fibers for optimum performance.
APS metallic linings are constructed from an innovative design and from more durable materials than other brands so you get longer wear and superior stopping power for greater safety.
Fits for the following aircraft models:
- •B-N Group Ltd. (BN-2, BN-2A, BN-2A-6, BN-2A-8, BN-2A-2, BN-2A-9, BN-2A-3, BN-2A-20, BN-T-4R, BN-2A-21, BN-2A-26, BN-2A-27, BN-2B-20, BN-2B-21, BN-2B-26, BN-2B-27, BN-2T)
- •Cessna Aircraft Co. (P210N, T303, LC40-550FG)
- •Cirrus Design Corporation (SR22)
- •General Avia (F22B, F22C, F22R)
- •Piper Aircraft, Inc. (PA-23-250, PA-E23-250, PA-24-400, PA-30, PA-39, PA-32-260, PA-32-300, PA-32R-300, PA-32-301, RA-32-301T, PA-32RT-300, PA-32RT-300T, PA-32R-301 (SP), PA-32R-301 (HP), PA-32R-301T, PA-34-200, PA-34-200T, PA-34-220T, PA-44-180, PA-44-180T, PA-46-310P, PA-46-350P PA-46-500TP, PA-46R-350T)
- •Socata, G.A (GA-7)
- •Vulcanair S.p.A (P68, P68B, P68C, P68C-TC)
BREAK-IN PROCEDURES
Conditioning Procedure for APS Linings
Metallic Linings
NOTE: APS linings are an iron based, metallic compound. These linings must be properly conditioned in order to provide optimum performance and service life.
1. Taxi Aircraft at a high rate of speed (30-35 kts.).
2. Apply brakes with a slightly heavier than normal pressure.
3. Repeat the above operation for a second consecutive time. Do not let the brakes cool between stops.
4. Allow brakes to cool for 10-15 minutes.
5. Apply brakes to confirm that normal pressure will hold the aircraft at high level static run-up power settings. If brakes hold, conditioning procedure is complete. If brakes do not hold, allow brakes to cool completely and repeat steps 1-3.
Semi-Metallic Linings*
Taxi aircraft for 1500 feet with engine at 1700 rpm applying brake pedal forces needed to develop a 5-10 mph taxi speed.
1. Allow brakes to cool for 10-15 minutes.
2. Apply brakes to confirm that normal pressure will hold the aircraft at high level static run-up power settings. If brakes hold, conditioning procedure is complete. If brakes do not hold, allow brakes to cool completely and repeat steps 1-3.
*Semi-metallic linings are suitable for use with all types of steel or chrome plated brake discs.