Pulsar-List Digest Archive

Mon 09/26/11


Total Messages Posted: 9



Today's Message Index:
----------------------
 
     1. 07:43 AM - Re: EXTERNAL: Aborted Trip and Safe Return after Repair (Cowan, Michael)
     2. 12:09 PM - Parting out my Pulsar3 (Max)
     3. 12:35 PM - Fw: FW: Galloping Ghost Crash---The Latest Theory!!! (Bob Heiser)
     4. 12:53 PM - Re: Parting out my Pulsar3 (otto souta)
     5. 01:16 PM - Home Safely (Dennis Adams)
     6. 01:46 PM - Re: Parting out my Pulsar3 (Larry Wheat)
     7. 05:43 PM - Re: Parting out my Pulsar3 (Max)
     8. 05:59 PM - Re: Parting out my Pulsar3 (Bill S)
     9. 07:24 PM - Fw: Galloping Ghost total loss cooling system. (Alex Kozloff)
 
 
 


Message 1


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    Time: 07:43:56 AM PST US
    From: "Cowan, Michael" <michael.cowan@lmco.com>
    Subject: Aborted Trip and Safe Return after Repair
    Alex, Glad to hear you're back in SP and all is OK. Sorry you had to miss the reunion. Sounds like we missed a good one. Hopefully next year I'll have mine flying and we can organize a group to make the trip back east. Anytime you take a notion to visit the AV, let us know. Maybe we could convince Bob to fly down from Big Bear. Great airport restaurant at WJF. Best, Mike & Becky Cowan -----Original Message----- From: owner-pulsar-list-server@matronics.com [mailto:owner-pulsar-list-server@matronics.com] On Behalf Of Alex Kozloff Sent: Saturday, September 24, 2011 4:37 PM Subject: EXTERNAL: Pulsar-List: Aborted Trip and Safe Return after Repair Hey Gang: Sorry couldn't make it to LWC from my first stop at IFP (Bullhead City, AZ). It took four (4) days to sort out the problem, Order Parts, Install them, and fly home. The problem was that the snap ring that retains the spring retract boss for the Bendix sheared off. This allowed the starter motor gear to move further forward than normal and jam against the crank shaft gear. With the engine running and the Bendix gear unretracted, the starter acted as a generator instead of a motor. This generated an unregulated back EMF that fried the started motor. We couldn't find any parts of the snap ring, and were worried that some bits may have entered the generator section. Thank goodness there is a hole in the bottom of the generator case that may have been put there to preclude such an event. Bottom line, once new starter was installed, engine ran like a top all the way back to SZP. The temperature at IFP was 106 to 112 degrees during my stay there; and it could have been a very uncomfortable working environment. It so happens that Reg Pridmore, one of my SZP neighbors, had a hangar there that allowed the work to be done out of the sun. That fact, plus superb support from Scott Harms, who built the hangars and the personnel at Landmark FBO made it all possible. As it turned out, across the Colorado River from Bullhead City (Named after an outcropping in the river shaped like a Bull's head)lies Laughlin, NV. Gambling towns such as Laughlin, offer reasonable room rates and excellent dining venues for their customers, as well as free shuttle service from the airport. So, if you are planning to have a breakdown in your plane, arrange it to happen at IFP, You won't be sorry, -- Alex Kozloff Pulsar I N190AK Santa Paula, CA 93061 (949) 400-6364 Cell (805) 525-1415 Office _!_ 'O-O-(_)-O-O'


    Message 2


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    Time: 12:09:21 PM PST US
    From: "Max" <max@spro.net>
    Subject: Parting out my Pulsar3
    Pulsar Builders, I am parting out my Pulsar3 purchased from Skystar Aviation in 1998. It has a Rotax 914 (which has been sold), a night VFR panel complete, Cleveland dual brake system, axles, wheels and tires, Whelen Nav lights and strobes, and an in-flight adjustable Ivoprop hub and controls for a 2 or 3 blade configuration. If you have interest in something, let me know, and I will provide more specific Info. Max Boesiger Coldwell Banker (208) 250-6234


    Message 3


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    Time: 12:35:24 PM PST US
    From: Bob Heiser <w7ikt@fly-web.us>
    Subject: Fwd: FW: Galloping Ghost Crash---The Latest Theory!!!


    Message 4


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    Time: 12:53:37 PM PST US
    From: otto souta <otto@otamat.com>
    Subject: Re: Parting out my Pulsar3
    Hi Max, please advise details of the Ivoprop hub and controls. Regards Otto On 26/09/2011 20:09, Max wrote: > --> Pulsar-List message posted by: "Max"<max@spro.net> > > Pulsar Builders, > I am parting out my Pulsar3 purchased from Skystar Aviation in 1998. It > has a Rotax 914 (which has been sold), a night VFR panel complete, Cleveland > dual brake system, axles, wheels and tires, Whelen Nav lights and strobes, > and an in-flight adjustable Ivoprop hub and controls for a 2 or 3 blade > configuration. If you have interest in something, let me know, and I will > provide more specific Info. > > > Max Boesiger > Coldwell Banker > (208) 250-6234 > >


    Message 5


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    Time: 01:16:05 PM PST US
    Subject: Home Safely
    From: Dennis Adams <ghf4986@gmail.com>
    All, I got home safely. Had lost of headwinds right on the nose, 25 and 30 mph all the way. Attached is a photo of the Wind River Range in Wyoming that I managed to take between buffets. Not a good idea to cross mountains late in the day! Greg thanks so much for all you and Donna do for us. You really keep it alive. Best, Dennis Adams N375CM


    Message 6


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    Time: 01:46:24 PM PST US
    Subject: Re: Parting out my Pulsar3
    From: Larry Wheat <lwheat2083@gmail.com>
    Max: I am in the process of building a Pulsar III. What parts of the fuselage and wings, wheel pants etc do you have. Was the airplane damaged? To what extent. I am located in MOses Lake, Washington and was thinking about spares. Thanks in advance. Cheers On Mon, Sep 26, 2011 at 12:09 PM, Max <max@spro.net> wrote: > > Pulsar Builders, > I am parting out my Pulsar3 purchased from Skystar Aviation in 1998. It > has a Rotax 914 (which has been sold), a night VFR panel complete, > Cleveland > dual brake system, axles, wheels and tires, Whelen Nav lights and strobes, > and an in-flight adjustable Ivoprop hub and controls for a 2 or 3 blade > configuration. If you have interest in something, let me know, and I will > provide more specific Info. > > > Max Boesiger > Coldwell Banker > (208) 250-6234 > > -- Larry Wheat


    Message 7


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    Time: 05:43:33 PM PST US
    From: "Max" <max@spro.net>
    Subject: Parting out my Pulsar3
    Larry, I'm afraid there isn't much left of the fuselage and wings. All was damaged enough that they aren't worth the effort (and weight) to fix. I do have the upper cowl piece. I have a complete panel that was designed and assembled by Gulf Coast Avionics. Are you interested in any of that? Max Boesiger (208) 250-6234 From: owner-pulsar-list-server@matronics.com [mailto:owner-pulsar-list-server@matronics.com] On Behalf Of Larry Wheat Sent: Monday, September 26, 2011 2:45 PM Subject: Re: Pulsar-List: Parting out my Pulsar3 Max: I am in the process of building a Pulsar III. What parts of the fuselage and wings, wheel pants etc do you have. Was the airplane damaged? To what extent. I am located in MOses Lake, Washington and was thinking about spares. Thanks in advance. Cheers On Mon, Sep 26, 2011 at 12:09 PM, Max <max@spro.net> wrote: Pulsar Builders, I am parting out my Pulsar3 purchased from Skystar Aviation in 1998. It has a Rotax 914 (which has been sold), a night VFR panel complete, Cleveland dual brake system, axles, wheels and tires, Whelen Nav lights and strobes, and an in-flight adjustable Ivoprop hub and controls for a 2 or 3 blade configuration. If you have interest in something, let me know, and I will provide more specific Info. Max Boesiger Coldwell Banker (208) 250-6234 <tel:%28208%29%20250-6234> s.com/Navigator?Pulsar-List" target="_blank">http://www.matronics.com/Navigator?Pulsar-List ronics.com/" target="_blank">http://forums.matronics.com Matt Dralle, List Admin. ==== -- Larry Wheat


    Message 8


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    Time: 05:59:56 PM PST US
    From: "Bill S" <docyukon@ptcnet.net>
    Subject: Re: Parting out my Pulsar3
    Max Do you have the four wing spar mounting bolts? Bill S . Pulsar lll Kit #17 ----- Original Message ----- From: Max To: pulsar-list@matronics.com Sent: Monday, September 26, 2011 7:41 PM Subject: RE: Pulsar-List: Parting out my Pulsar3 Larry, I'm afraid there isn't much left of the fuselage and wings. All was damaged enough that they aren't worth the effort (and weight) to fix. I do have the upper cowl piece. I have a complete panel that was designed and assembled by Gulf Coast Avionics. Are you interested in any of that? Max Boesiger (208) 250-6234 From: owner-pulsar-list-server@matronics.com [mailto:owner-pulsar-list-server@matronics.com] On Behalf Of Larry Wheat Sent: Monday, September 26, 2011 2:45 PM To: pulsar-list@matronics.com Subject: Re: Pulsar-List: Parting out my Pulsar3 Max: I am in the process of building a Pulsar III. What parts of the fuselage and wings, wheel pants etc do you have. Was the airplane damaged? To what extent. I am located in MOses Lake, Washington and was thinking about spares. Thanks in advance. Cheers On Mon, Sep 26, 2011 at 12:09 PM, Max <max@spro.net> wrote: Pulsar Builders, I am parting out my Pulsar3 purchased from Skystar Aviation in 1998. It has a Rotax 914 (which has been sold), a night VFR panel complete, Cleveland dual brake system, axles, wheels and tires, Whelen Nav lights and strobes, and an in-flight adjustable Ivoprop hub and controls for a 2 or 3 blade configuration. If you have interest in something, let me know, and I will provide more specific Info. Max Boesiger Coldwell Banker (208) 250-6234 s.com/Navigator?Pulsar-List" target="_blank">http://www.matronics.com/Navigator?Pulsar-List ronics.com/" target="_blank">http://forums.matronics.com Matt Dralle, List Admin. ==== -- Larry Wheat http://www.matronics.com/Navigator?Pulsar-Listhttp://forums.matronics.com http://www.matronics.com/contribution


    Message 9


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    Time: 07:24:40 PM PST US
    Subject: Fwd: Galloping Ghost total loss cooling system.
    From: "Alex Kozloff" <avkozloff@roadrunner.com>
    Hey Pulsar Gang: This is the most complete story of the GG I've seen that I just received from my SZP neighbor who is a Rotary Engine expert. -- Alex Kozloff Pulsar I N190AK Santa Paula, CA 93061 (949) 400-6364 Cell (805) 525-1415 Office _!_ ------- Forwarded message ------- From: "Rotary Engine" <rotaryeng@earthlink.net> Cc: Subject: Galloping Ghost total loss cooling system. Paul, I don't keep up with these racing planes, but what happened to the radiator on this Mustang? How is the engine cooled? And I thought that the Mustang's radiator ductwork was designed so that it actually yielded positive thrust? If so, why remove it? Csaba Csera ================================================================================== From a pilot friend. Galloping Ghost crash Ok... here's the skinny on the accident.... A P-51 normally has two trim tabs. One on each elevator... This one had one and other one was fixed in place. He was warned about all the forces being put on that one tab. It failed. He had at least a 10G load when the plane pitched up from the loss of the trim tab and he went "nighty night" and probably never woke up. Here's the "theory" of the crash from experienced racers. In 1989 this type of thing happened to another pilot but he lived to tell the story. When flying a P-51 at 450+mph you need to have full nose down trim to keep the plane level. The elevator trim tab broke off and the aircraft immediately went in to a 10G climb, confirmed by the G-meter. The pilot came to, from the sudden blackout and realized he had slipped through the shoulder harness and was looking at the floor of the airplane. He was able to reach the throttle and pull it back to slow down and was able to recover and land. Fast forward to 2011 Photo one is the airplane taxiing, note the pilots head in the canopy. Photo two is typical oil canning as a result of the tremendous torque these engines put out at high power. [The oil canning could be due to several things. One is the down force on the tail to counter the effect of a CG ahead ahead of the lift. Another is the helical shape of the slip stream affecting the vertical fin and horizontal stabilizer causing a torque on the fuselage. Another could be caused by the violent snap roll the aircraft experienced. Obviously the skin thickness was reduced when the aircraft was rebuilt to reduce weight. The history of that is interesting as it was changed on late model production P51's as well. PL] Photo three is a photo of GG upside down with a missing elevator trim tab. Note all you see is the back of the pilots head indicating he is being forced down in the cockpit. Photo four is a view of the left side nose down with the tail wheel extended and no view of the pilot. The tail wheel is held up by hydraulics only with no mechanical uplock, thus indicating a high G-force causing it to extend. Photos five and six are from the left side prior to impact, note no view of the pilot and the tail wheel extended. Photo seven is the debris just after the crash. To the right of center above the crowd it appears to be the wing with the leading edge down. The people were mostly hit by chunks of concrete, asphalt and aircraft debris. They were also hurt by the trampling of people getting out of the way. Peter =========================================================================== Its a myth the thrust from the P51 cooling system completely over came the drag from the cooling system. It was still more drag than no cooling system at all. One must add in the frontal area of the duct and scoop. One reason the rotary adds less cooling system drag as the engine is so compact the entire cooling system can be placed in the cowl without adding frontal area. However that is not to say the rotary has no cooling drag. The cooling scoop acts more or less as a perpendicular flat plate extending down from the cowl surface. The porosity of this plate plate controls the cooling drag. If there is no rad in the duct the air going in the scoop will go out the exit only with a bit of skin friction drag. The key to low cooling drag is come up with a rad or rad configuration that achieves the cooling with a minimum of drag. The P51 rad and rad configuration was not optimum. Later work on heat exchangers improved the situation. That is a long story and best told by my book "How to Cool Your Wankel" and other books such as "Compact Heat Exchangers" and "The Aerodynamics of Propulsion". http://www2.leewardairranch.com/racing "She [GG] now represents the leading edge of air racing technology with a 3,600 hp racing engine, state-of-the-art boil-off cooling system, streamlined aerodynamics and a real-time data acquisition and management system." Of course the amount of cooling required is directly proportional to the amount of HP being generated. That is not the same as saying directly proportional to speed as you have more mass of air to work with at higher speeds. The total loss boil off cooling system adds weight and will only work for short periods of time as found in Reno air races. The weight has a small affect on drag. Probably the largest effect is a change in CG location that must be trimmed by the horizontal trim tab. Paul Lamar




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