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FAA AC 25.562-1B Static Interface Loads
Let me give a question about the aircraft seat test criteria. FAA AC AC No: 25.562-1B Dynamic Evaluation of Seat Restraint Systems and Occupant Protection on Transport Airplanes d. Structural Tests for seats with the family design concepts (see §§ 25.562(c)(7) and (8)). (1) Substantiation of...- 60NUAGE
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- Replies: 11
- Forum: Aircraft engineering
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Compression Warp
Could anybody help me understanding the 'compression warp' of propeller of Hamilton Sundstrand 568F? - What part of propeller is it? Your kind answer or comments will be highly appreciated.- 60NUAGE
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- Replies: 5
- Forum: Aircraft engineering
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FAR PART 25.365 e) Formula
Hi. IS THERE ANYONE WHO CAN ANSWER MY INQUIRY ABOUT THE FAR PART 25.365 e) The size Ho must be computed by the following formula: Ho = PAs Where - Ho = Maximum opening in square feet, need not exceed 20 square feet. P =As/6,240 + .024 As = Maximum cross-sectional area of the pressurized shell...- 60NUAGE
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- Replies: 6
- Forum: Aircraft engineering
