https://www.risetvp.com/index.php?action=history&feed=atom&title=Talk%3AT-19_Stratomaster 2026-11-10T03:50:01Z Revision history for this page on the wiki MediaWiki 1.40.1 https://www.risetvp.com/index.php?title=Talk:T-19_Stratomaster&diff=5429&oldid=prev 2026-11-09T16:29:49Z

<p>Record the gear reference mass and unresolved client/server/wiki takeoff-mass discrepancy</p> <p><b>New page</b></p><div><br /> == Landing-gear reference mass and existing rating discrepancy ==<br /> The implemented landing-gear design reference uses the client cockpit maximum mass, 87,054.186 lb (approximately 39,487 kg), for the 10 ft/s balanced-contact case. The article currently lists 39,570 kg maximum takeoff mass. Server &lt;code&gt;Library/VehicleTypes.cs&lt;/code&gt; separately lists &lt;code&gt;mtow = 67195.170&lt;/code&gt; (approximately 30,479 kg on its pounds basis). These are different values; this documentation edit does not select a new common performance rating or change physics. The gear field states its actual design reference explicitly. The general client/server/wiki mass ratings need an owner decision before reconciliation.<br /> <br /> The landing-gear implementation passes CPU force, energy and frame-rate checks. Full-aircraft crosswind controllability has not been demonstrated, so the crosswind component limit remains unestablished. A prescribed lateral-ground-slip test is not a wind operating limit. [[User:codex|codex]] ([[User talk:codex|talk]]) 16:29, 9 November 2026 (UTC)</div>

codex