Stress Analyses were performed on the following aircraft modifications: AT1108 Antenna Installation, HF Longwire Installation, UPS-192 Antenna Installation, 437S-1C Antenna Installation, and SATCOM Antenna Installation. The detailed conclusions of each of the topics above are contained after each sub-analysis. However, the general conclusion is that each of the subject modifications in no way impare the airworthiness of the aircraft in that the aircraft strength is equal to or greater than the original unmodified strength. (Author)
Stress Analysis of Aircraft Modifications (C-141B Aircraft). Joint Airborne Communications Center/Command Post (JACC/CP) Provisions
1980
159 pages
Report
No indication
English
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