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John Galban wrote:
Dave wrote: The plot thickens! ![]() I mn finding the same. (note links posted above) from several sources. This 14 knts had to come from SOMEWHERE... I'm thinking that "Prior 77 stall = 58" might have come from the point where Piper shifted from using MPH to Knots for their performance figures. 58 mph is right where the dirty stall should be on most 150 - 180 hp PA28s. Where the "44" came from is anybody's guess. 58 mph converted to knots is around 50-51 kts. Perhaps the missing 6 kts might come from a measurement in indicated airspeed rather than calibrated airspeed. One thing I can tell you is that they all stall at around the same speed. There were no drastic changes that changed the stall characteristics from '76 to 77. If you're seriously considering buying one, this is not something you should spend a lot of time worrying about. John Galban=====N4BQ (PA28-180) The stall speed is 44 kts. Speed on final should be 1.3 times that: 44*1.3 = 57. |
#2
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I agree... not worried at all...
![]() I just could not come to terms with the numbers, 1 yr apart.. Here are two of the sources that got me wondering.. Look here .. http://www.pilotfriend.com/Piper%20aircraft.htm and http://www.premi-air.co.nz/singlespe...iper+PA-28-151 All #'s are in knts.... Dave On 3 Jun 2005 16:48:18 -0700, "John Galban" wrote: Dave wrote: The plot thickens! ![]() I mn finding the same. (note links posted above) from several sources. This 14 knts had to come from SOMEWHERE... I'm thinking that "Prior 77 stall = 58" might have come from the point where Piper shifted from using MPH to Knots for their performance figures. 58 mph is right where the dirty stall should be on most 150 - 180 hp PA28s. Where the "44" came from is anybody's guess. 58 mph converted to knots is around 50-51 kts. Perhaps the missing 6 kts might come from a measurement in indicated airspeed rather than calibrated airspeed. One thing I can tell you is that they all stall at around the same speed. There were no drastic changes that changed the stall characteristics from '76 to 77. If you're seriously considering buying one, this is not something you should spend a lot of time worrying about. John Galban=====N4BQ (PA28-180) |
#3
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Dave wrote:
Hi All! OK... Piper Warrior...PA28-151 Considering purchase... It's is a 1976 Model.. Specs, (published) say stall, dirty ( Full Flaps ) for a 1976 built is 58 knts. Knots or MPH? I was once accused by a very inexperienced flight instructor of flying too fast on an engine out approach in a Lance because the airspeed indicator was in MPH instead of knots. I flew the proper speed for MPH. He'd apparently never flown an airplane with its airspeed indicator showing anything but knots. 58 knots seems pretty hot for a dirty stall speed. -- Mortimer Schnerd, RN VE |
#4
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![]() "Dave" wrote in message ... Hi All! OK... Piper Warrior...PA28-151 Considering purchase... It's is a 1976 Model.. Specs, (published) say stall, dirty ( Full Flaps ) for a 1976 built is 58 knts. ...1977 and later is 44 knts! WHAT changes were made to bring the stall speed down by 14 knts! I have looked at both, I cannot (untrained eye) see what is different.. Owner of the '76 says 52 knts(w/flaps) , 58 knts "clean" (????) Tis a huge difference... is this correct? Why? Can the 76 be modified to get the stall speed lower? Can any one help here? What is the story? Thanks in advance! Dave The earlier 151s have frise ailerons as opposed to the cheaper piano hinges on the later ones. Give much smoother handling. with the piano hinged ailerons the aileron it self has ridges to try and retain the airflow over the ailerons. |
#5
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The earlier 151s have frise ailerons as opposed to the cheaper piano
hinges on the later ones. Give much smoother handling. with the piano hinged ailerons the aileron it self has ridges to try and retain the airflow over the ailerons. No offense, and maybe I'm just an insensitive clod at the controls, but I've got over 800 hours in Cherokees of all flavors, my '75 had the Frise ailerons -- and to say that the piano hinge versions provide "much smoother handling" just ain't true. In fact, the handling differences are so slight as to be inconsequential. (Which, of course, is why Piper switched back to the easier-to-build piano hinged versions...) If I were blindfolded and told to fly either version, there is no way I would be able to tell you which is which in flight. (On the ground they DO feel different, IMO -- but who cares on the ground?) -- Jay Honeck Iowa City, IA Pathfinder N56993 www.AlexisParkInn.com "Your Aviation Destination" |
#6
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![]() "Jay Honeck" wrote in message news:cOhoe.17175$nG6.3465@attbi_s22... The earlier 151s have frise ailerons as opposed to the cheaper piano hinges on the later ones. Give much smoother handling. with the piano hinged ailerons the aileron it self has ridges to try and retain the airflow over the ailerons. No offense, and maybe I'm just an insensitive clod at the controls, but I've got over 800 hours in Cherokees of all flavors, my '75 had the Frise ailerons -- and to say that the piano hinge versions provide "much smoother handling" just ain't true. In fact, the handling differences are so slight as to be inconsequential. (Which, of course, is why Piper switched back to the easier-to-build piano hinged versions...) If I were blindfolded and told to fly either version, there is no way I would be able to tell you which is which in flight. (On the ground they DO feel different, IMO -- but who cares on the ground?) I did not say the piano hinge ailerons were smoother than the frise, quite the contrary but I would say the do feel different in the air and that's my experience. |
#7
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On 2005-06-03 23:43, Dave wrote:
Hi All! OK... Piper Warrior...PA28-151 Considering purchase... It's is a 1976 Model.. Specs, (published) say stall, dirty ( Full Flaps ) for a 1976 built is 58 knts. ...1977 and later is 44 knts! WHAT changes were made to bring the stall speed down by 14 knts! I have looked at both, I cannot (untrained eye) see what is different.. Owner of the '76 says 52 knts(w/flaps) , 58 knts "clean" (????) Tis a huge difference... is this correct? Why? Can the 76 be modified to get the stall speed lower? Can any one help here? What is the story? Thanks in advance! Dave I haven't gone beyond a websearch, so I can't verify this, but there may be a reason in the wing profile change around that time. According to a paragraph in: http://www.whittsflying.com/Page5.66Piper.htm quote When Piper went from the Hershey-bar wing to the tapered wing there was a dramatic shift in the critical approach airspeed. The short wing required that the pilot never allow the approach speed get slow. Arrive in ground effect too slow and you would fall right through it. Result was numerous fuel leaks since tanks were adjacent to landing gear. The tapered wing gave the opposite problem. Any approach speed that was slightly fast would cause excessive float. Short runways were the scenes of numerous overruns. end quote This was said to have happened in -78, so maybe it's unrelated. Otherwise I understood that: Short wing (Hershey-bar) = model# ends in 0 Long wing= model# ends in 1 Maybe your -76 151 still has a short wing? confusing. /Rolf |
#8
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On 2005-06-07 17:19, Rolf Blom wrote:
-snip- never mind; I see it was solved in a later post. /Rolf |
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