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A manufacturer's approach to ensure long term structural integrityIn the present paper we are as a manufacturer of airliners, certified according to the FAR 25 regulations, describing what considerations in terms of design, sizing, verification, maintenance, etc., that are essential to ensure long term structural integrity.

In the first part we are describing the main features of the design concepts of Saab 340 and Saab 2000 aircraft with respect to structural integrity and high reliability. Secondly we are describing the approach we have adopted at Saab Aircraft to ensure structural integrity and high reliability of Saab Aircraft products. We are describing the concepts of global and local loads and sequences,
the fatigue and damage tolerance sizing and its verification. We are also describing the quality assurance in production and the structural maintenance programme according to the MSG-3. Structural repair and feedback from operators are also covered.
Document ID
19920020890
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Hans Ansell
(Saab (Sweden) Bromma, Sweden)
Billy Fredriksson
(Saab (Sweden) Bromma, Sweden)
Ingvar Holm
(Saab (Sweden) Bromma, Sweden)
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
Air Transportation And Safety
Report/Patent Number
N92-30133
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
92N30133
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Keywords
Aging Aircraft
Structural Airworthiness
Civil aviation
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