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Performance of fuselage pressure structureThere are currently more than 1,000 Boeing airplanes around the world over 20 years old. That number is expected to double by the year 1995. With these statistics comes the reality that structural airworthiness will be in the forefront of aviation issues well into the next century.

The results of previous and recent test programs Boeing has implemented to study the structural performance of older airplanes relative to pressurized fuselage sections are described. Included in testing were flat panels with multiple site damage (MSD), a full-scale 737 and 2 747s as well as panels representing a 737 and 777, and a generic aircraft in large pressure-test fixtures.

Because damage is a normal part of aging, focus is on the degree to which structural integrity is maintained after failure or partial failure of any structural element, including multiple site damage (MSD), and multiple element damage (MED).
Document ID
19920020866
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
James R. Maclin
(Boeing Commercial Airplane Group Seattle, WA, United States)
Date Acquired
September 6, 2013
Publication Date
November 19, 1991
Publication Information
Publication: 1991 International Conference on Aging Aircraft and Structural Airworthiness
Publisher: National Aeronautics and Space Administration
Volume: NASA-CP-3160
Issue Publication Date: January 1, 1992
URL: https://ntrs.nasa.gov/citations/19920020863
Subject Category
Structural Mechanics
Air Transportation And Safety
Report/Patent Number
N92-30109
Meeting Information
Meeting: International Conference on Aging Aircraft and Structural Airworthiness
Location: Washington, D.C.
Country: US
Start Date: November 19, 1991
End Date: November 21, 1991
Sponsors: Federal Aviation Administration, National Aeronautics and Space Administration
Accession Number
92N30109
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Aging Aircraft
Structural Airworthiness
Civil aviation
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