Europa-List Digest Archive

Sun 01/23/22


Total Messages Posted: 3



Today's Message Index:
----------------------
 
     1. 02:02 PM - Re: Stalls & spins - any test pilot pireps out there? (rparigoris)
     2. 05:03 PM - Re: Re: Stalls & spins - any test pilot pireps out there? (Bud Yerly)
     3. 06:15 PM - Re: Stalls & spins - any test pilot pireps out there? (budyerly@msn.com)
 
 
 


Message 1


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    Time: 02:02:09 PM PST US
    Subject: Re: Stalls & spins - any test pilot pireps out there?
    From: "rparigoris" <rparigor@hotmail.com>
    Hi Group When stalling Europa pulling some positive Gs, I believe the net effect of wing flexing upward at tips and design/geometry of aileron control has ailerons droop (less washout when pulling Gs). Nev had mentioned this to me and suggested to begin with 1/8" reflexed ailerons. Has anyone compared stalling when pulling Gs with reflexed ailerons compared with even ailerons? Results? I spoke with 1 owner that had at least 1/8" drooped ailerons and when I asked him about it, he said he was faster but it would spin like a maple leaf without not much coaxing. I think that was at 1G. Ron P. Read this topic online here: http://forums.matronics.com/viewtopic.php?p=505790#505790


    Message 2


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    Time: 05:03:46 PM PST US
    From: Bud Yerly <budyerly@msn.com>
    Subject: Re: Stalls & spins - any test pilot pireps out there?
    Ron, I have never noticed droopy ailerons. A laminar flow airfoil needs no reflexed up or down for reduced drag. The Europa is not a Cessna or Piper flat bottom airfoil. Let me be clear, there are aircraft that have interesting aileron rig. To name a few: Ailerons that have slop at the center position and the ailerons actually float. Ailerons that are not balanced and under G load droop because of poor geometry of the aileron quick disconnect. Poor QD geometry leading to interesting slippage and ailerons that have as much as 1/4 inch play up, OK at the center, and tight at the bottom. That is a build error or sloppy construction. Try this: Lock your aileron in the wing rack (since you are not flying this winter) and try to move your belcrank with your hand. If you can flex the mechanism look for loose screws. Build the plane like the book then test fly please. You are not going to do better than ELSA or the prototypes. Best Regards, Bud Yerly -----Original Message----- From: owner-europa-list-server@matronics.com <owner-europa-list-server@matronics.com> On Behalf Of rparigoris Sent: Sunday, January 23, 2022 5:02 PM Subject: Europa-List: Re: Stalls & spins - any test pilot pireps out there? Hi Group When stalling Europa pulling some positive Gs, I believe the net effect of wing flexing upward at tips and design/geometry of aileron control has ailerons droop (less washout when pulling Gs). Nev had mentioned this to me and suggested to begin with 1/8" reflexed ailerons. Has anyone compared stalling when pulling Gs with reflexed ailerons compared with even ailerons? Results? I spoke with 1 owner that had at least 1/8" drooped ailerons and when I asked him about it, he said he was faster but it would spin like a maple leaf without not much coaxing. I think that was at 1G. Ron P. Read this topic online here: https://na01.safelinks.protection.outlook.com/?url=http%3A%2F%2Fforums.matronics.com%2Fviewtopic.php%3Fp%3D505790%23505790&amp;data=04%7C01%7C%7C8bf681201c59485d6f4308d9debc9970%7C84df9e7fe9f640afb435aaaaaaaaaaaa%7C1%7C0%7C637785723895006432%7CUnknown%7CTWFpbGZsb3d8eyJWIjoiMC4wLjAwMDAiLCJQIjoiV2luMzIiLCJBTiI6Ik1haWwiLCJXVCI6Mn0%3D%7C3000&amp;sdata=y3l3RKyJlA37I3w0EzV%2FQxVoXv4%2FGrNzwnaj%2FqFUHg8%3D&amp;reserved=0


    Message 3


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    Time: 06:15:07 PM PST US
    Subject: Re: Stalls & spins - any test pilot pireps out there?
    From: "budyerly@msn.com" <budyerly@msn.com>
    David, I am perplexed. It is true that most of the used "deal of the century" aircraft that came through my shop for evaluation or repair took on an average of 350 man hours to bring them up to Annex E and flight standards. I have never had an aircraft from my shop display any charachteristic you describe. Even 139AB which had the right wing incidence at 3.1 degrees and the left at 2.6 degrees never rolled over and into a spin. Simply relaxation of back pressure broke the stall. Yes, the wing drop was entertaining, but only through complete disregard for normal flight stall techniques (i.e. adding aileron and leaving ones feet flat on the floor) and nearly full aft stick would the plane break into a severe un-commanded roll. (Fixing 139AB is a long story but 450 hours later and $20,000 it is a fine flying airplane.) If you know of another aircraft with such characteristics, I suggest you advise the owner to fix the darned thing. For everyone else, I don't intend to upset anyone. I've done a paper on my thoughts on stalls on the Europa expanding my techniques articles. I've omitted the glider wing stall spin as I found it benign and not worth talking about. In any case, spin entry had to be done with full aft stick and full rudder to gain entry. Proper spin recovery controls quickly broke the stall and rotation. The mass of the glider winged aircraft meant more rudder was used to quicken the stop of the rotation than on the short wing. I only did one turn in the glider as I didn't have a chute and the required safety gear to do spin testing here in the States for a full three turns. Attached is my synopsis of stalls in the Europa XS/Classic. I've also included a second hand buying paper Bottom line, if you find your Europa will stall straight ahead fine using my techniques for yaw control and it behaves differently in an accelerated stall, there is a control not operating properly which should have been identified on inspection. I have found that most scary Europa stall characteristics are build rig errors that have gone ignored and missed by inspectors, and most are pilot proficiency and training issues. Best Regards, Bud Yerly Read this topic online here: http://forums.matronics.com/viewtopic.php?p=505792#505792 Attachments: http://forums.matronics.com//files/buying_a_second_hand_experimental_161.docx http://forums.matronics.com//files/europa_stall_spin_evaluation_129.pdf




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