The computer aided engineering approach can produce a reasonably complete airplane loads report. Weight may be reduced with stress analysis or testing only after calculating accurate loads.Īlthough there are no FAR certification requirements for loads and strength analysis for this category in the US, there should be great concern for flight safety in this freedom from regulation. Previous versions of this software have been used as a reference by hundreds of individuals and companies in over 40 countries. The software calculates the loads using methods acceptable to the FAA and actually recommended in the previous CAR3CAM3 CAM4 and FAR 23FAR 25 regulations. The loads on the airplane are determined by (1) the three view drawing, (2) the chosen maximum take-off weight, (3) the chosen category and load factor. Aerostream Wind Tunnel Programs Manual With AdobeĪileron, flap, tab, engine mount, landing and one engine out loads are also calculated.
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