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On Wed, 09 Jun 2004 23:21:25 +0200, CV wrote:
Bela P. Havasreti wrote: On Wed, 9 Jun 2004 07:58:32 -0700, "C J Campbell" wrote: off, you don't lose your nose gear!) At the same time, losing all that weight might improve your glide significantly. No, less weight does not significantly improve glide performance, it just shifts your best glide to a lower speed range. (It will improve your glide downwind though, and make it worse into wind) More important however would be the aerodynamic shape of whatever was left of the nose after having prop, engine and part of the cowling fall off. It is not too bold a bet to say the aerodynamic characteristics will have been clearly worse after the damage than before, thus more drag and worse glide. CV Please watch who you quote (I didn't write that....). Bela P. Havasreti |
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In article , C J Campbell wrote:
I have always been told that it is impossible to pitch down if your engine comes off. You will pitch up, stall, and die. This was something we often discussed in our hangar lying sessions at SPX. There was quite a bit of speculation that if you immediately prevented the stall by pushing forward, you'd be able to survive the loss of the engine. I guess this has been proven, at least for the C170B. off, you don't lose your nose gear!) At the same time, losing all that weight might improve your glide significantly. It would be balanced by the fact the aerodynamically-shaped cowling has gone, and has been replaced by a decidedly un-aerodynamic flat firewall. -- Dylan Smith, Castletown, Isle of Man Flying: http://www.dylansmith.net Frontier Elite Universe: http://www.alioth.net "Maintain thine airspeed, lest the ground come up and smite thee" |
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![]() "Dylan Smith" wrote in message ... In article , C J Campbell wrote: I have always been told that it is impossible to pitch down if your engine comes off. You will pitch up, stall, and die. This was something we often discussed in our hangar lying sessions at SPX. There was quite a bit of speculation that if you immediately prevented the stall by pushing forward, you'd be able to survive the loss of the engine. I guess this has been proven, at least for the C170B. off, you don't lose your nose gear!) At the same time, losing all that weight might improve your glide significantly. It would be balanced by the fact the aerodynamically-shaped cowling has gone, and has been replaced by a decidedly un-aerodynamic flat firewall. The aerodynamic shaped cowling means little in a Cessna. You have that prop that is still spinning and creating as much drag as disk that size. |
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![]() The aerodynamic shaped cowling means little in a Cessna. You have that prop that is still spinning and creating as much drag as disk that size. Not if the engine is gone too. Jose -- (for Email, make the obvious changes in my address) |
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The C-170B must have one helluva lot of elevator authority. I can't belive
that the CG wasn't back in the tail somewhere after losing the whole engine! -- Bob (Chief Pilot, White Knuckle Airways) I don't have to like Bush and Cheney (Or Kerry, for that matter) to love America "C J Campbell" wrote in message ... Both pilots are well known and respected in the Puget Sound area. Amazing that the pilot of the 170 was able to fly his plane at all: NTSB Identification: SEA04FA083B 14 CFR Part 91: General Aviation Accident occurred Sunday, May 16, 2004 in Tenino, WA Aircraft: Cessna 210J, registration: N3329S Injuries: 1 Fatal, 1 Minor. This is preliminary information, subject to change, and may contain errors. Any errors in this report will be corrected when the final report has been completed. On May 16, 2004, approximately 2040 Pacific daylight time, a Cessna 170B, N3510D, and a Cessna 210J, N3329S, collided in flight approximately five nautical miles southeast of Tenino, Washington. The Cessna 170B had departed Roseburg, Oregon, and was en route to the Wax Orchards Airport, Vashon Island, Washington. The Cessna 210J had departed Camas, Washington, and was en route to Paine Field, Everett, Washington. There was one occupant onboard each aircraft. The pilot of the Cessna 210J, a certificated commercial pilot, sustained fatal injuries while the certificated private pilot of the Cessna 170B sustained minor injuries. Visual meteorological conditions prevailed and both aircraft were operated under 14 CFR Part 91 regulations. According to the Federal Aviation Administration (FAA), both pilots received weather briefings but neither pilot filed a flight plan, and neither aircraft had requested or were receiving air route traffic control radar services at the time of the collision. The pilot of the Cessna 170B reported that he was level at 3,500 feet mean sea level and had just changed his heading from 350 degrees to 318 degrees. The pilot stated, "I was looking down at my map as part of this 'normal scan' that I do when the collision occurred." The pilot stated, "I never saw the other airplane." The pilot further stated that the aircraft pitched down and went into an uncommanded left turn, requiring him to stabilize the angle of bank by holding full right aileron. The pilot reported that he then realized that the engine had come off the airplane, but he was still able to maintain the nose down attitude and keep his speed up. The pilot further reported that he then attempted to move the elevator and rudder enough to see if they were responsive, which they were. The pilot stated that as the airplane continued in the left turn through a southerly heading to an easterly heading he saw what appeared to be parts of "something" falling out of the sky below him. The pilot said, "...that's when I thought I'd been hit by another airplane." The pilot reported that as he proceeded turning and losing altitude rapidly, he picked out a field where he thought he could land. The pilot said, "I moved the flap handle a little to see how much they moved, and when I saw they worked I decided to add some flap to reduce my speed as I approached the field." The pilot stated that he then applied right rudder to raise the left wing before "clipping" the tops of some trees and going through one power line wire which bordered the field on the south. The pilot stated that after the airplane impacted the ground and came to rest, he immediately exited the airplane and sought help at a nearby house. The aircraft had come to rest in an inverted position on a magnetic heading of 120 degrees. There was no post impact fire. A witness, who is also a private pilot and the owner of the property where the Cessna 210J came to rest, reported that while in his house he heard an airplane flying around, prompting him to go outside to see what it was. The[i] witness stated that he looked up and thought he heard airplanes overhead, then saw the two accident aircraft coming together. The witness further stated, " saw them about 5 to 8 seconds before they hit. Both were straight and level. Neither took evasive action in any way." The witness stated that one was heading north and the other one was heading northeast when he saw them hit and parts started coming at him. The witness further stated that after the parts hit the ground he looked up again and saw "the silver aircraft" gliding north without an engine before it went out of sight over some trees. The Cessna 170B's engine was located approximately one-half mile southwest of where the aircraft came to rest. The airplane's right cabin door and left lower cowling were found approximately three-quarters of a mile south of this location. The Cessna 210J's engine, propeller, and main cabin area were located approximately one-quarter of a mile south of where the Cessna 170B came to rest. The wing was located approximately 400 feet south of the main cabin area, and the airplane's tail section was discovered in a thick brush area one-half mile south of the main cabin. At 2031, a special aviation surface weather observation taken at the Olympia Airport, Olympia, Washington, located 11 nautical miles northwest of the collision reported wind 220 degrees at 5 knots, visibility 10 statute miles, broken clouds at 2,600 feet, overcast clouds at 4,900 feet, temperature 12 degrees C, dew point 7 degrees C, and an altimeter of 30.03 inches of Mercury. |
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Both pilots are well known and respected in the Puget Sound area. Amazing
that the pilot of the 170 was able to fly his plane at all: This is the second NTSB report I've read where pilots were able to maintain control of an engine-less plane. How is this possible? Without an engine up front, the CG would pitch so far aft that the plane should fall like a maple leaf -- yet these two guys were able to nose the plane over and maintain flight. How can this be? -- Jay Honeck Iowa City, IA Pathfinder N56993 www.AlexisParkInn.com "Your Aviation Destination" |
#7
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Jay Honeck wrote:
How can this be? Just goes to show: "Never stop flying the airplane." ![]() -- John T http://tknowlogy.com/TknoFlyer http://pocketgear.com/products_searc...veloperid=4415 ____________________ |
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The only "successful" flights I have seen after an engine departs, involved
VERY steep bank angles until VERY near the ground. Both a/c (A T6 at Reno, and a Swift in Idaho) came to rest close to the engine that had departed. I assume the engine didn't glide very well. Al Gerharter "Jay Honeck" wrote in message news:eAFxc.19854$HG.16770@attbi_s53... Both pilots are well known and respected in the Puget Sound area. Amazing that the pilot of the 170 was able to fly his plane at all: This is the second NTSB report I've read where pilots were able to maintain control of an engine-less plane. How is this possible? Without an engine up front, the CG would pitch so far aft that the plane should fall like a maple leaf -- yet these two guys were able to nose the plane over and maintain flight. How can this be? -- Jay Honeck Iowa City, IA Pathfinder N56993 www.AlexisParkInn.com "Your Aviation Destination" |
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Jay Honeck opined
Both pilots are well known and respected in the Puget Sound area. Amazing that the pilot of the 170 was able to fly his plane at all: This is the second NTSB report I've read where pilots were able to maintain control of an engine-less plane. How is this possible? Without an engine up front, the CG would pitch so far aft that the plane should fall like a maple leaf -- yet these two guys were able to nose the plane over and maintain flight. How can this be? AIrspeed. Given enough airsped a tail (or nose) heavy aircraft can fly. But the feedback becomes positive instead of negative. If you slow down the tail drops. More down elevator is needed increasing drag. Get too slow and you cannot recover. Computers can handle the problem better than people. See late model jet aircraft with relaxed stability. -ash Cthulhu for President! Why vote for a lesser evil? |
#10
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In article eAFxc.19854$HG.16770@attbi_s53, Jay Honeck wrote:
How is this possible? Without an engine up front, the CG would pitch so far aft that the plane should fall like a maple leaf -- yet these two guys were able to nose the plane over and maintain flight. I suspect at nearly full forward elevator, the tail is producing upforce (rather than the usual downforce) - it becomes a lifting surface. I should imagine the aircraft would become extremely twitchy in pitch though. The tail on most light taildraggers can hold the aft fuselage up on the ground with virtually no airspeed (many can do it whilst stationary given sufficient propwash over the tail). Even our little C140 could keep the tail up at low airspeed with two fat buggers in the cabin (who are behind the main wheels), so the tail will generate a reasonable amount of lift. -- Dylan Smith, Castletown, Isle of Man Flying: http://www.dylansmith.net Frontier Elite Universe: http://www.alioth.net "Maintain thine airspeed, lest the ground come up and smite thee" |
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