199-76 conversion kit - Cleveland Wheel & Brake Systems

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FAA-PMA AIRCRAFT WHEEL & BRAKE DIVISION PARKER HANNIFIN CORPORATION AVON, OHIO PARTS LIST 199-76 CONVERSION KIT CESSNA MODELS 340, 340A, 401, 401A, 401B, 402, 402A, 402B, 402C, 411, 411A, 414, 414A, 421, 421A, 421B, 421C PART NUMBER DRAWING REVISION DESCRIPTION QUANTITY 30-100 Rev. D dated 06-21-2006 Brake Assembly 2 40-135A Rev. E dated 11-22-2006 Wheel Assembly 2 067-04300 Rev. A dated 09-15-1978 Spacer 2 104-00200 ------------------------------ Fitting (AN815-4D) 2 101-00700 ------------------------------ O-Ring (MS28775-012) 2 104-02000 ------------------------------ Elbow Fitting (AN837-4D) 2 094-90500 ------------------------------ Nut (AN924-4D) 2 Publication Package (P/N PP199-07600) 50-47 Rev. G dated 10-27-1988 Installation Drawing (Two Sheets) SA197GL Last amend date 1-26-83 Supplemental Type Certificate (Cessna Models 401, 401A, 401B, 402, 402A, 402B, 402C, 411, 411A, 414, 414A, 421, 421A, 421B, 421C) SA664GL Issue date 2-24-83 Supplemental Type Certificate (Cessna Models 340, 340A) PRM14A ----------------------------- Metallic Brake Lining Conditioning Procedure PRM69 ----------------------------- General Maintenance Information ------- Product Registration Card NOTES: 1. This kit will convert one aircraft to Cleveland Wheels and Brakes. 2. For use with MIL-H-5606 (Red Fluid). REV. G 05-08-2007 (0374-74) REV. F 10-27-1988 (293-17) REV. E 12-20-1982 (271-39) 199-76 ClevelandWheels & Brakes Parker Hannifin Corporation Aircraft Wheel & Brake 1160 Center Road Avon, Ohio 44011 USA 1-800-BRAKING (272-5464) 216-937-1272 l FAX 216-937-5409 PRODUCT REFERENCE MEMO Initial Release December 12, 1983 Rev A July 1, 1995 PRM14A Page 1 of 1 METALLIC BRAKE LINING CONDITIONING PROCEDURE The brake lining material used in this brake assembly is an iron based metallic composition. This material must be properly conditioned (glazed) in order to provide optimum service life. Dynamometer tests have shown that at low braking energies, unglazed linings experience greater wear and the brake discs can become severely scored. Conditioning may be accomplished as follows: 1. Perform two (2) consecutive full stop braking applications from 30 to 35 kts. Do not allow the brake discs to cool substantially between stops. 2. On aircraft with tail wheels, exercise caution during stopping to prevent tail lifting. Due to the efficiency of these brakes, extremely hard braking could result in lifting the tail from the ground. This conditioning procedure will wear off high spots and generate sufficient heat to glaze the linings. Once the linings are glazed, the braking system will provide many hours of maintenance free service. Visual inspection of the brake disc will indicate the lining condition. A smooth surface, 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 evident. Light use, such as in taxiing, will cause the glaze to be worn rapidly. Use caution in performing this procedure, as higher speeds with successive stops could cause the brakes to overheat resulting in warped discs and/or pressure plates. ClevelandWheels & Brakes Parker Hannifin Corporation Aircraft Wheel & Brake 1160 Center Road Avon, Ohio 44011 USA 1-800-BRAKING (272-5464) 216-937-1272 l FAX 216-937-5409 PRODUCT REFERENCE MEMO Initial Release February 01, 1997 PRM69 Page 1 of 1 AVAILABILITY OF GENERAL MAINTENANCE INFORMATION AND TORQUING PROCEDURES EFFECTIVITY: All Parker Hannifin (Cleveland Wheels & Brakes) External Disc Design wheel & brake assemblies. APPLICABILITY: Aircraft converted per STC approved kits to use Cleveland External Disc Design wheel & brake assemblies. REASON: This PRM is issued to inform Wheel & Brake Conversion Kit users and installers that information regarding general maintenance and proper bolt / nut torquing procedures is available. This information is contained in the Cleveland Wheels & Brakes Component Maintenance Manual (CMM) and in the Cleveland Technicians Service Guide, PRM64. Most Cleveland Conversion Kits were designed prior to creation of the CMM. Parker Hannifin is in process of upgrading kit paperwork to include a requirement to use the CMM and PRM64 as wheel & brake service information. This PRM serves the same purpose for kits whose paperwork has not yet been upgraded. DESCRIPTION: The Cleveland Wheels & Brakes Component Maintenance Manual and PRM64, Technician’s Service Guide shall be used as service information when performing general maintenance on Cleveland External Disc Design wheels & brakes. Particular attention should be paid to instructions regarding wheel bolt torquing procedures. NOTE: Refer to the CMM or PRM64 to determine the required torque procedure (Dry or Lubtork). While using the required torque procedure, observe the torque required to turn the nut (free running torque). This value must be added to the value stated on the casting or nameplate (or in the CMM or PRM64) to obtain a true torque value. Proper torque is imperative to prevent premature bolt or mating component failure. COMPLIANCE: Highly Recommended. APPROVAL: The engineering contents of this Product Reference Memo are FAA DER approved. WEIGHT & BALANCE: Not applicable. PUBLICATIONS: Cleveland Wheels & Brakes Component Maintenance Manual and PRM64 are available from: Customer Support Parker Hannifin Corporation Aircraft Wheel & Brake 1160 Center Road Phone: 1-800- BRAKING (272-5464) Avon, Ohio FAX: 216-937-5409 1 Parker Hannifin Corporation Aerospace/Aircraft Wheel & Brake 1160 Center Road Avon, OH 44011 Date: _ _/_ _/20_ _ Subject: Letter of Authorization for Installation of STC’d Conversion Kits To whom it may concern: Parker Hannifin Corporation, Aircraft Wheel & Brake Division, hereby states that the following item(s): KIT NUMBER: 199-___________ FAA APPROVAL: 1) STC # ________________________ NO OTHER APPROVALS NECESSARY