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#1
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http://www.duluthsuperior.com/mld/du...or/9723097.htm
I'm a bit concerned that I never heard about another recent deployment... "Still, the parachute system has not proven a cure-all, as evidenced by the Sept. 10 crash of a Cirrus SR22 in Park Falls, Wis. That crash claimed the life of Gerald Miller, 60, of Seboygan, Wis." It doesn't make clear whether the old fellow in Sheboygan deployed... |
#3
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("C Kingsbury" wrote)
snip What I'd wonder about, were I wealthy enough to have problems like this, is what about more marginal cases. Let's say I'm flying up here in densely populated New England, on top of an overcast at 4000' at night, and the engine quits. Let's say I've got 1500' ceilings. Do I pull the plug right away, or do I drop down through? How high do I have to be for the chute to open properly? Anything I can do to position myself so that the chute puts me down in that parking lot, rather than on I-95, or into some hospital building? From the Cirrus web page: http://www.cirrusdesign.com/servicec...ml/pohmain.asp (Same link as above) http://makeashorterlink.com/?T27445959 (I put you in an SR20. Hope that's ok) SR20 POH Section 3 - Emergency Procedures (randomly cut/pasted) Emergency Landing (Engine-out): Flaps Up................................................ ...................... ........86 KIAS Flaps 50%............................................... ...................... ......81 KIAS Flaps 100%.............................................. ...................... .....75 KIAS Maximum Glide Ratio ~ 10.9 : 1 .. Note . With a seized or failed engine, the distance that the airplane will glide will be more than the distance it would glide with the engine at idle, such as during training. If the propeller is windmilling, some additional glide range may be achieved by moving the Power Lever to idle and increasing airspeed by 5 to 10 knots. (Cirrus Airplane Parachute System - CAPS) The minimum demonstrated altitude loss for a CAPS deployment from a one-turn spin is 920 feet. Activation at higher altitudes provides enhanced safety margins for parachute recoveries. Do not waste time and altitude trying to recover from a spiral/spin before activating CAPS. (V-PD) Maximum Demonstrated Parachute Deployment Speed is the maximum speed at which parachute deployment has been demonstrated. The maximum demonstrated deployment speed is 135 KIAS. Reducing airspeed allows minimum parachute loads and prevents structural overload and possible parachute failure. Bon voyage :-) Montblack |
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