Damage Tolerance Assessment of CASA Landing Gear Willis and Kaplan, Incorporated

Format:

Conference/Event

Author/Creator:

Kaplan, M. P., author.

Conference Name:

SAE Airframe/Engine Maintenance and Repair Conference and Exposition (1997-08-05 : Vancouver, Canada)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1997

Summary:

A study was completed on CASA aircraft to examine the landing gear structural durability. The gear, designed to a safe life criterion, were approaching their replacement time. Damage tolerance methods were used to extend the life of these components. Critical components were examined, measured, and drawings prepared. A loads analysis using FAA criteria was completed, usage determined through pilot interviews and published data, and a loading spectrum prepared. Additionally, a stress analysis was conducted for each component. Finally, tests were completed to determine inspection intervals. Inspection procedures were determined, and an STC issued by the FAA. As a result, the gear no longer need to be retired when they reach their retirement time. Instead periodic inspections are being used to assess their structural life

Notes:

Vendor supplied data

Publisher Number:

972626

Access Restriction:

Restricted for use by site license