poadeleted20
Deleted
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- Apr 8, 2005
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- 31,250
Try pulling your seat forward another notch.I did land our C-177B with around a 17kt component once. My left foot was almost straight out.
In any event, since it's not a limitation, there isn't much incentive for the manufacturer to go a whole lot farther in the maximum crosswind component demonstration than the regulatory minimum of 0.2 Vs0 (see 14 CFR 23.233). About 0.3 Vs0 seems to be about the norm. But if the aircraft meets all the other directional control requirements, it will probably have a lot of rudder in reserve even with the crosswind at 0.3 Vs0, and my C-177 experience suggests that it can handle at least 50% more than the book demonstrated value, although pilot skill is being seriously taxed at that point.
Nevertheless, my instructing experience suggests that the average nonprofessional light plane pilot (the 50 hr/year crowd) is generally wise to set the book demonstrated value as their own limit in Standard category aircraft. OTOH, my LSA experience suggests that any demonstrated crosswind value in the book there should be taken a lot more seriously by even the most skilled and proficient pilots, probably because of the relative paucity of certification standards in that area for LSA's.
Of course, what a pilot can handle and what the airplane can handle are often two different things, with the average pilot's proficiency level usually being too low to safely fly the plane to its physical/aerodynamic limits. But don't blame the airplane if the pilot isn't capable of flying it to its limit, and don't suggest to pilots that reduced flap setting will make a significant difference in their ability to handle crosswinds.