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Federal Aviation Administration's approach to engine rotor integritySections of the U.S. Airworthiness Standards which contribute to rotor integrity are explored. Reports published under NASA's Rotor Burst Protection program are included in current FAA studies to determine the weight penalty for two different levels of increased containment, and the penalty associated with protecting critical structure and systems, the passenger cabin, and the flight deck by strategic location of armor shields or deflector plates. Findings of the two studies will be used to propose revisions to regulations to reduce uncontained rotor failures.
Document ID
19780002126
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Forney, A. K.
(Federal Aviation Administration Washington, DC, United States)
Date Acquired
August 9, 2013
Publication Date
March 1, 1977
Publication Information
Publication: MIT An Assessment of Technol. for Turbojet Engine Rotor Failures
Subject Category
Aircraft Propulsion And Power
Accession Number
78N10069
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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