| AIRCRAFT BRAKE LINING CONDITIONING PROCEDURES |
|||
|
|||
 |
|||
|
Brake Lining Conditioning Procedures When new linings have been installed, it is important to condition them properly to obtain the service life designed into them. The metallic and organic linings are not conditioned in the same manner because they have different operating characteristics. Separate conditioning procedures are given for metallic and organic linings. These conditioning procedures will wear off high spots and generate sufficient heat to create a thin layer of glazed material at the lining friction surface. Normal brake usage should generate enough heat to maintain the glaze throughout the life of the lining. Properly conditioned linings will provide many hours of maintenance free service. A visual inspection of the brake disc will indicate the lining condition. A smooth surface, one without grooves, indicates the linings are properly glazed. If the disc is rough (grooved), the linings must be reglazed. The conditioning procedure should be performed whenever the rough disc condition is observed. Light use, such as in taxiing, will cause the glaze to be worn rapidly. CAUTION: Due to the efficiency of these brakes, extremely hard braking on aircraft with tailwheels could result in lifting the tail from the ground. Nonasbestos Organic Linings Conditioning Procedures 1. Taxi aircraft for 1500 feet with engine at 1700 rpm applying brake pedal force as needed to develop a 5-10mph taxi speed. 2. Allow the brakes to cool for 10 to 15 minutes. 3. Apply brakes and check for restraint at high static throttle. If brakes hold, conditioning is complete. 4. If brakes cannot hold aircraft during static run up, allow brakes to completely cool and repeat steps 1 through 3. Metallic Linings Conditioning Procedures 1. Perform two (2) consecutive full stop braking applications from 30 to 35 knots. Do not allow the brake discs to cool substantially between the stops. 2. Allow the brakes to cool for 10 to 15 minutes. 3. Apply brakes and check for restraint at high static throttle. If brakes hold, conditioning is complete. 4. If brakes cannot hold aircraft during static run up, allow brakes to completely cool and repeat steps 1 through 3. |
|||
|
AIRCRAFT PARTS by CATEGORY ---- Aircraft Parts Quick Reference ----- Frequently Asked Maintenance Questions ----- How To Tips Airworthiness Directives & Service Bulletins (Parts & Kits) ----- Aircraft Parts & Aviation Links ----- *APEX Aircraft Parts Kiosk Locations*
CAPS was designed and is intended to be used as a guide only to aid in finding the part numbers needed for your application. The part numbers provided are derived from factory specifications of your aircraft and may not provide correct part numbers for any modified aircraft including STC's, Field Approvals or any other modifications. Aircraft Parts Express, Inc. will not be held liable for any misrepresentations, errors or omissions of information contained in this program. In accordance with FAR 91.403 it is the responsibility of the installer/owner operator to confirm the use of the correct part and its installation. © 2007-2010 Aircraft Parts Express, Inc./CAPS All rights reserved. Copyright (c) 2007 Aircraft Parts Express, Inc. All Rights Reserved. |
