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In a previous article, "Peter Duniho" said:
And actually, while I haven't flown the Pipers you're referring to, my understanding is that the gear extension was based on airspeed, not engine power. Your comment about the behavior of such systems in icing conditions The POH for the Lance isn't 100% clear on this, but my understanding is that with the emergency gear extension, the gear will come down if you go below a certain manifold pressure at one speed, or will come down regardless of the manifold pressure at a lower speed. The POH says "Some aircraft also incorporate a pressure sensing device in the system which lowers the gear regardless of gear selector position, depending upon airspeed and engine power (propellor slipstream). Gear extension is designed to occur, even if the selector is in the up position, at airspeeds below approximately 103 KIAS with power off. The extension speeds will vary from approximately 91 kts to approximately 103 KIAS depending on power settings and altitude." Actually, reading that again, it's possible that what is happening isn't that it comes on at a lower speed if you have power on, but that the propellor slipstream holds the gear up against the springs if you have power on. Sometimes I learn more answering other people's questions than I do getting answers to my own. -- Paul Tomblin http://xcski.com/blogs/pt/ If you're not part of the solution, you're part of the precipitate. |
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