Ultrasonic inspection procedures for examining the wing spar attachments on a Viscount aircraft are presented. Procedures are applied primarily to the top and bottom boom joints and lugs. (Author)
Ultrasonic Inspection of Wing Spar Attachments - Top and Bottom Boom Joints and Lugs
1972
10 pages
Report
No indication
English
Fatigue strength of riveted joints and lugs
Engineering Index Backfile | 1956
|Engineering Index Backfile | 1919
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