The main features of the design concepts for the Saab 340 and Saab 2000 aircraft are described with respect to structural integrity and high reliability. Also described is the approach taken at Saab Aircraft to ensure structural integrity and high reliability. The concepts of global and local loads and sequences, and the fatigue and damage tolerance sizing and their verification are discussed. Also described is quality assurance in the production and structural maintenance program. Structural repair and feedback from operators are also covered.
Manufacturer's Approach to Ensure Long Term Structural Integrity
1992
27 pages
Report
No indication
English
Construction Equipment, Materials, & Supplies , Quality Control & Reliability , Nondestructive Testing , Aircraft maintenance , Quality control , Reliability , Saab aircraft , Structural failure , Manufacturing , Aircraft industry , Damage , Loads (Forces) , Production planning , Sequencing , Tolerances (Mechanics) , Foreign technology
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