RV10-List Digest Archive

Sat 08/29/09


Total Messages Posted: 14



Today's Message Index:
----------------------
 
     1. 04:43 AM - Re: Page 15-4 Wing Rear Spar (John Trollinger)
     2. 06:42 AM - rudder stops (Sandra & Rick Lark)
     3. 07:43 AM - Re: rudder stops (Jesse Saint)
     4. 07:53 AM - Re: rudder stops (John Cox)
     5. 10:04 AM - Re: rudder stops (Tim Olson)
     6. 10:44 AM - another data point (David McNeill)
     7. 10:51 AM - Re: rudder stops (Jesse Saint)
     8. 01:36 PM - Tales from the dark OOPS I mean door side.... (Les Kearney)
     9. 03:39 PM - Rudder Trim Pushrod Help (BGS)
    10. 05:35 PM - Gaps between Weld-On 10 and Window (Jeff Carpenter)
    11. 05:37 PM - Re: another data point (Bill DeRouchey)
    12. 06:14 PM - Re: another data point (David McNeill)
    13. 09:12 PM - Re: Rudder Trim Pushrod Help (woxofswa)
    14. 09:55 PM - Re: Tales from the dark OOPS I mean door side.... (RV Builder (Michael Sausen))
 
 
 


Message 1


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    Time: 04:43:00 AM PST US
    Subject: Re: Page 15-4 Wing Rear Spar
    From: John Trollinger <john@trollingers.com>
    Thanks all.. its nice to not always have to wait for vans to be open to get your answer. back to the shop to drill some holes. Do Not Archive John


    Message 2


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    Time: 06:42:01 AM PST US
    From: "Sandra & Rick Lark" <jrlark@bmts.com>
    Subject: rudder stops
    Hi all. I'm just about to fasten the rudder stops(R-1007B's) to the lower rudder hinge bracket(VS-1010) and have decided to use bolts as opposed to the AN470AD4-6 rivets as Scott Schmidt and others have reported can work loose in high winds. In looking in the ACS catalogue I see structural machine screws (NAS600-603, page 93) which have a far greater tensile strength than the rivets. Unfortunately there is no rating for shear strength which I would think is more important. What type of screws have those who have replaced the rivets used?? Has anyone approached Vans w/regards to this substitute, as the prototype has them?? Thx, Rick #40956 Southampton, Ont.


    Message 3


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    Time: 07:43:50 AM PST US
    From: Jesse Saint <jesse@saintaviation.com>
    Subject: Re: rudder stops
    I have used standard #6 screws and nuts as used elsewhere in the kit. The steel screw with a bigger diameter should have a LOT higher sheer strength than the rivet, although I don't know in actual values. When I looked at Van's plane it appeared that this is what they were using. do not archive Jesse Saint Saint Aviation, Inc. jesse@saintaviation.com Cell: 352-427-0285 Fax: 815-377-3694 On Aug 29, 2009, at 9:26 AM, Sandra & Rick Lark wrote: > <jrlark@bmts.com> > > Hi all. > > I'm just about to fasten the rudder stops(R-1007B's) to the lower > rudder hinge bracket(VS-1010) and have decided to use bolts as > opposed to the > AN470AD4-6 rivets as Scott Schmidt and others have reported can work > loose in high winds. > > In looking in the ACS catalogue I see structural machine screws > (NAS600-603, page 93) which have a far greater tensile strength than > the rivets. Unfortunately there is no rating for shear strength > which I would think is more important. What type of screws have > those who have replaced the rivets used?? > > Has anyone approached Vans w/regards to this substitute, as the > prototype has them?? > > Thx, Rick > #40956 > Southampton, Ont. > >


    Message 4


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    Time: 07:53:59 AM PST US
    Subject: rudder stops
    From: John Cox <johnwcox@pacificnw.com>
    Consider Hi-Loks (HL18s) or Hi-Lites from Hi-Shear Corporation. John Cox #40600 From: Sandra & Rick Lark Sent: Sat 8/29/2009 6:26 AM Subject: RV10-List: rudder stops Hi all. I'm just about to fasten the rudder stops(R-1007B's) to the lower rudder hinge bracket(VS-1010) and have decided to use bolts as opposed to the AN470AD4-6 rivets as Scott Schmidt and others have reported can work loose in high winds. In looking in the ACS catalogue I see structural machine screws (NAS600-603 , page 93) which have a far greater tensile strength than the rivets. Unfortunately there is no rating for shear strength which I would think is more important. What type of screws have those who have replaced the rivet s used?? Has anyone approached Vans w/regards to this substitute, as the prototype has them?? Thx, Rick #40956 Southampton, Ont.


    Message 5


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    Time: 10:04:21 AM PST US
    From: Tim Olson <Tim@MyRV10.com>
    Subject: Re: rudder stops
    I don't think you have to get too worried about the shear spec of the screws you use. You just need to get something that is more resistant than the aluminum rivets. So any steel screw will do. I'd try to put one that you can use the smooth upper part of the screw through the material, where the grip just starts as you get outside the rudder blocks. Put a washer or two on it to guarantee you get it tight and don't bottom on the shoulder. The fact is, if you beat the thing up so bad that a steel screw is going to shear, the rudder stop material itself is probably going to break anyway, and you'll break an ear off. So the screw themselves really aren't a big worry. Tim Olson - RV-10 N104CD Sandra & Rick Lark wrote: > > Hi all. > > I'm just about to fasten the rudder stops(R-1007B's) to the lower rudder > hinge bracket(VS-1010) and have decided to use bolts as opposed to the > AN470AD4-6 rivets as Scott Schmidt and others have reported can work > loose in high winds. > > In looking in the ACS catalogue I see structural machine screws > (NAS600-603, page 93) which have a far greater tensile strength than the > rivets. Unfortunately there is no rating for shear strength which I > would think is more important. What type of screws have those who have > replaced the rivets used?? > > Has anyone approached Vans w/regards to this substitute, as the > prototype has them?? > > Thx, Rick > #40956 > Southampton, Ont. >


    Message 6


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    Time: 10:44:23 AM PST US
    From: "David McNeill" <dlm46007@cox.net>
    Subject: another data point
    At 40G at 6000 MSL and 80 F and 2400 pounds. We landed Runway 19 and easily turned off at the 1700 ft insectiing runway/taxiway mark. On departure the ground run was about 1000 ft.


    Message 7


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    Time: 10:51:13 AM PST US
    From: Jesse Saint <jesse@saintaviation.com>
    Subject: Re: rudder stops
    Also, if the threaded part goes through the other bracket, even with nut between the brackets, you are working, at least partially, in double sheer. Jesse Saint Saint Aviation jesse@saintaviation.com 352-427-0285 Sent from my iPhone On Aug 29, 2009, at 12:59 PM, Tim Olson <Tim@MyRV10.com> wrote: > > I don't think you have to get too worried about the shear spec > of the screws you use. You just need to get something > that is more resistant than the aluminum rivets. So any steel > screw will do. I'd try to put one that you can use the > smooth upper part of the screw through the material, where > the grip just starts as you get outside the rudder blocks. > Put a washer or two on it to guarantee you get it tight > and don't bottom on the shoulder. > > The fact is, if you beat the thing up so bad that a steel > screw is going to shear, the rudder stop material itself > is probably going to break anyway, and you'll break an > ear off. So the screw themselves really aren't a big > worry. > > Tim Olson - RV-10 N104CD > > > Sandra & Rick Lark wrote: >> > >> Hi all. >> I'm just about to fasten the rudder stops(R-1007B's) to the lower >> rudder hinge bracket(VS-1010) and have decided to use bolts as >> opposed to the >> AN470AD4-6 rivets as Scott Schmidt and others have reported can >> work loose in high winds. >> In looking in the ACS catalogue I see structural machine screws >> (NAS600-603, page 93) which have a far greater tensile strength >> than the rivets. Unfortunately there is no rating for shear >> strength which I would think is more important. What type of >> screws have those who have replaced the rivets used?? >> Has anyone approached Vans w/regards to this substitute, as the >> prototype has them?? >> Thx, Rick >> #40956 >> Southampton, Ont. > >


    Message 8


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    Time: 01:36:41 PM PST US
    From: "Les Kearney" <kearney@shaw.ca>
    Subject: Tales from the dark OOPS I mean door side....
    Hi Over the past few weeks I have been working on my canopy and doors. I have experienced a wide range of emotions when dealing with the doors ' mostly frustration! The doors seemed to be designed to test the will to build and our ability to persevere. As part of the process I have studied the usual websites to see what others have done and trolled the archives for any hints and tips that might be useful. Here are some of the things that I did (or wish I had done the first time through) to get to doors that actually work. When reading this, note that I used the Rivethead door blocks and the McMaster Carr door seals which mount on the canopy opening and not on the door. I also installed Steve DeNieri=92s flush handles and locks. What I did 1. Trimmed the door halves oversize prior to bonding. The index holes didn=92t match so bonding alignment was a concern. So was having enough material to allow clamping to the canopy while curing. 2. When bonding the door halves I followed the plans to a T. It turns out that most of the door edges get removed so it is important to have lots close in to the inside edge of the flanges. I ended up with several areas of delamination. I found that it was possible to inject epoxy into delaminated areas using a large bore hypo. The entire bottom edge of one door delaminated which strangely enough made repair easier. 3. The rear index holes didn=92t match so door alignment relative to the door sill was a problem. It was possible that the inner door half could sit too low in the openings and not have reasonable clearance from the sills. Without correction, this might result in the doors sitting on the bottom of the door sill. To ensure consistent spacing between the door and the door sill, I taped stacks of popsicle sticks (3 in each) onto the bottom of the door sill. The inner door sat on these during the bonding process. 4. The popsicle stick spacers also remained in place when during the initial door trim especially on the door top. I didn=92t want to inadvertently trim the door to short buy taking too much off the top. The doors were left a little long until the hinges were installed. 5. The initial fit objective was to get the doors flush in the opening with only a tiny gap all the way round. 6. The Rivethead door blocks were installed on the canopy fibreglass door posts 7. After the hinges and door blocks were installed considerable time was spent getting the doors pins open / close easily. After door seals were installed, I got to do this all over again. 8. Using washers as shims between the hinge and the canopy can change the gap between the canopy door post and the door. I used washers on an aft door hinges to slightly raise the height of the aft side of the door which in turn increased the forward gap between the door post and the door. 9. During latching the doors move fore / aft depending on which door pin contacts the door first and which has more friction. This in turn moves the door in the frame and changes the fore / aft gaps between the door and he canopy. A shim in the door opening between the canopy and the door prevents this shift during fitting. Uncorrected, this was going to be a problem. 10. The door seals caused the bottom of the doors to be pushed out which in turn resulted in the considerable pressure being required (on the outside of the door) to close the door enough for the door pins to engage. 11. I found the once the door seals were more than =BD compressed, the resistive force on the doors increased significantly. By removing more material from the outside of the canopy opening, I was able to reduce the seal compression and get an easier to close door. This was especially true of the canopy door posts. 12. What made a *huge* difference in getting the doors to close easily was pushing the canopy door sill inboard by about 1/8=94 This moved the seal that contacts the bottom of the door inboard and took most of outward pressure off the bottom of the door. 13. I floxed the nylon guide blocks on the fire/aft edges of the doors so that they were flush with the inner door perimeter. Consequently they interfered with the previously installed Rivethead door blocks. To correct, the canopy door posts were notched to allow the Rivethead blocks to mount directly on the aluminum door posts and thereby provide clearance for the door. I shimmed the Rivethead blocks so that there was minimal clearance between the doors and the blocks. This ensures that the doors remain correctly aligned within the door opening. See #9. 14. Once the door pins engaged the Rivethead door block, it still took some effort to fully engage the pins. There were several factors that added to the effort: * There is a lot of internal friction the Van=92s ratchet mechanism. Application of white grease made operation *much* easier * White grease on the door pins reduced the effort required to latch the doors. * There is a slight bow on the door. The long door pin should have a slight curve to ensure it does not bind against the in side of the door * The further the door pins go into the door blocks, the greater the closing effort required. I reduced mine so that the only extend about =BC=94 through the aluminum door posts. * The more pressure required to push the door in place so the pins can engage, the more effort required to close the door * If the door perimeter contacts the canopy anywhere, the effort required to close the door will increase. What I would do differently * When bonding the door halves, use considerable more epoxy & flox on the door perimeter especially close to the inner edge of the flanges to be bonded. * Pay more attention to the curves on the door pins (especially the long ones). One of the pins was binding on the door interior thus increasing the effort required to latch the door. * Grease the ratcheting mechanism before starting the door fit. A lot of the door stiffness comes from the door mechanisms. When trying to adjust the fit, it would have beneficial to have the stiffness out of the equation as it was sometime difficult to know what was causing the fit problems. * Install the door seals prior to doing the initial door fit. * Pay more attention to where the door seals are being compressed too much when closing the door PRIOR to trimming the inside of the canopy flange. (In some places, I had to build up the inside of the canopy flange as I had to take more off the outside of the flange. To reduce door compression. * Flox the fore and aft door pin guides when building the doors * Install the Rivethead door blocks directly on the aluminum door posts rather than first fitting on the canopy. * Shim the Rivethead door blocks to ensure door alignment when fitting the doors Then end result of this is I can now close and latch both doors with only one finger of pressure on the inside door handle with only one finger of pressure on the outside of the bottom of the door. Cheers Les #40643 ' Living in a f/g world


    Message 9


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    Time: 03:39:41 PM PST US
    Subject: Rudder Trim Pushrod Help
    From: "BGS" <Brian.Steeves@Parkenna.com>
    I am modifying my rudder for rudder trim with a trim tab fit into the rudder. Not that everything is in and mounted, I am having some clearance problems with the push rod hitting the outer skin and flare. As it sits now, the servo can travel a little over half an inch but the actual travel is 7/8 for the T2-7A Servo. When the push rod is pushed it ends up hitting the outer rudder skin, when it is pulled it hits the flare. I am attaching a couple of pictures to help better understand my rambling and horrible description. So my question is, can anybody give me some ideas on how get full travel of the servo without the push rod hitting the skin or flare (hopefully with out boring the hole out to much). For more detailed pictures you can see them on my builders log at http://www.briansrv10.com/Rudder_Trim.php Appreciate any help you can give. Read this topic online here: http://forums.matronics.com/viewtopic.php?p=260401#260401 Attachments: http://forums.matronics.com//files/rudder_trim_help_002_545.jpg http://forums.matronics.com//files/rudder_trim_help_001_294.jpg


    Message 10


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    Time: 05:35:40 PM PST US
    From: Jeff Carpenter <jeff@westcottpress.com>
    Subject: Gaps between Weld-On 10 and Window
    I took the plunge yesterday and bonded the window in to the left side door. I peeled the tape off today and found significant gaps between the weld-on and the window... particularly along the curved vertical edges. In hindsight, it was obviously too hot to be doing this work yesterday... my shop is at the base of the mountains near JPL where the fires have been raging for the past few days and, though it is air conditioned, was probably about 85% inside. The weld-on just set up too quickly. I'm thinking of drilling a few small holes and injecting epoxy in to fill the gaps. Has anyone gone down this road before? Is there a better way to fix this, shy of replacing the whole thing? Jeff Carpenter 40304 Singin those Weld-on 10 blues...


    Message 11


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    Time: 05:37:36 PM PST US
    From: Bill DeRouchey <billderou@yahoo.com>
    Subject: Re: another data point
    David- Sorry I missed you. We had four RV's from Prescott at the Valle fly-in. Bill --- On Sat, 8/29/09, David McNeill <dlm46007@cox.net> wrote: From: David McNeill <dlm46007@cox.net> Subject: RV10-List: another data point At 40G at 6000 MSL and 80 F and 2400 pounds. We landed Runway 19 and easily turned off at the 1700 ft insectiing runway/taxiway mark. On departure the ground run was about 1000 ft.


    Message 12


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    Time: 06:14:27 PM PST US
    From: "David McNeill" <dlm46007@cox.net>
    Subject: another data point
    we departed about 0900; arrived about 0640. We left FFZ about 0556 , running LOP about 55% power and caught a friend's 172 in the pattern at 40G after he departed FFZ at 0530. The APRS track worked until about 1500 AGL in the 40G area. The last hit was at 7300 MSL _____ From: owner-rv10-list-server@matronics.com [mailto:owner-rv10-list-server@matronics.com] On Behalf Of Bill DeRouchey Sent: Saturday, August 29, 2009 5:30 PM Subject: Re: RV10-List: another data point David- Sorry I missed you. We had four RV's from Prescott at the Valle fly-in. Bill --- On Sat, 8/29/09, David McNeill <dlm46007@cox.net> wrote: From: David McNeill <dlm46007@cox.net> Subject: RV10-List: another data point At 40G at 6000 MSL and 80 F and 2400 pounds. We landed Runway 19 and easily turned off at the 1700 ft insectiing runway/taxiway mark. On departure the ground run was about 1000 ft.


    Message 13


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    Time: 09:12:58 PM PST US
    Subject: Re: Rudder Trim Pushrod Help
    From: "woxofswa" <woxof@aol.com>
    >From an old modeler, if you move the clevis down closer to the airfoil you will have more clearance and need less throw for the same deflection. -------- Myron Nelson Mesa, AZ Emp completed, legacy build fuse in progress Read this topic online here: http://forums.matronics.com/viewtopic.php?p=260436#260436


    Message 14


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    Time: 09:55:26 PM PST US
    From: "RV Builder (Michael Sausen)" <rvbuilder@sausen.net>
    Subject: Tales from the dark OOPS I mean door side....
    Yes the doors are tons of fun. I have about 80 hours in mine at this poi nt and probably about another 15 to go but they are very nice. For me the weather seal caused interference in the first third of the frame from the t op. No problem on the bottom. The McMaster Carr weather stripping is nice but it does add a considerable amount of work to the doors in order to get it to fit well on the frame. I had to build up the inside of the frame a fair amount with flox before I could take the lip down to an acceptable amo unt and make the weather strip fit right. I also cut the little lip that i s on the inside of the trim out. I also picked up some of the same trim wi th =BC" instead of the 3/16" that everyone has been getting. It tends to f it much better in the bulky areas of the cabin top but it does make for an extra 1/16" to account for. Which actually brings me to another thing. Before deciding to go with th e door frame weather stripping method I picked up some of the door weather stripping from Alex D. This is the stuff that conforms to the door better than the stock stuff from Van. I don't need it now so if anyone is going w ith the stock method and wants to use this instead, I'll save you a couple bucks and sell you mine for $60 shipped. Just drop me an email. You can s ee them here: http://www.aviationtechproducts.com/html/products_pics.html#DoorSeal Michael From: owner-rv10-list-server@matronics.com [mailto:owner-rv10-list-server@m atronics.com] On Behalf Of Les Kearney Sent: Saturday, August 29, 2009 1:28 PM Subject: RV10-List: Tales from the dark OOPS I mean door side.... Hi Over the past few weeks I have been working on my canopy and doors. I have experienced a wide range of emotions when dealing with the doors - m ostly frustration! The doors seemed to be designed to test the will to buil d and our ability to persevere. As part of the process I have studied the usual websites to see what others have done and trolled the archives for any hints and tips that might be us eful. Here are some of the things that I did (or wish I had done the first time through) to get to doors that actually work. When reading this, note that I used the Rivethead door blocks and the McMas ter Carr door seals which mount on the canopy opening and not on the door. I also installed Steve DeNieri's flush handles and locks. What I did 1. Trimmed the door halves oversize prior to bonding. The index holes didn't match so bonding alignment was a concern. So was having enough mater ial to allow clamping to the canopy while curing. 2. When bonding the door halves I followed the plans to a T. It turns out that most of the door edges get removed so it is important to have lots close in to the inside edge of the flanges. I ended up with several areas of delamination. I found that it was possible to inject epoxy into delamina ted areas using a large bore hypo. The entire bottom edge of one door delam inated which strangely enough made repair easier. 3. The rear index holes didn't match so door alignment relative to the door sill was a problem. It was possible that the inner door half could si t too low in the openings and not have reasonable clearance from the sills. Without correction, this might result in the doors sitting on the bottom o f the door sill. To ensure consistent spacing between the door and the door sill, I taped stacks of popsicle sticks (3 in each) onto the bottom of the door sill. The inner door sat on these during the bonding process. 4. The popsicle stick spacers also remained in place when during the i nitial door trim especially on the door top. I didn't want to inadvertently trim the door to short buy taking too much off the top. The doors were lef t a little long until the hinges were installed. 5. The initial fit objective was to get the doors flush in the opening with only a tiny gap all the way round. 6. The Rivethead door blocks were installed on the canopy fibreglass d oor posts 7. After the hinges and door blocks were installed considerable time w as spent getting the doors pins open / close easily. After door seals were installed, I got to do this all over again. 8. Using washers as shims between the hinge and the canopy can change the gap between the canopy door post and the door. I used washers on an aft door hinges to slightly raise the height of the aft side of the door which in turn increased the forward gap between the door post and the door. 9. During latching the doors move fore / aft depending on which door p in contacts the door first and which has more friction. This in turn moves the door in the frame and changes the fore / aft gaps between the door and he canopy. A shim in the door opening between the canopy and the door preve nts this shift during fitting. Uncorrected, this was going to be a problem. 10. The door seals caused the bottom of the doors to be pushed out which i n turn resulted in the considerable pressure being required (on the outside of the door) to close the door enough for the door pins to engage. 11. I found the once the door seals were more than =BD compressed, the res istive force on the doors increased significantly. By removing more materia l from the outside of the canopy opening, I was able to reduce the seal com pression and get an easier to close door. This was especially true of the c anopy door posts. 12. What made a *huge* difference in getting the doors to close easily was pushing the canopy door sill inboard by about 1/8" This moved the seal tha t contacts the bottom of the door inboard and took most of outward pressure off the bottom of the door. 13. I floxed the nylon guide blocks on the fire/aft edges of the doors so that they were flush with the inner door perimeter. Consequently they inter fered with the previously installed Rivethead door blocks. To correct, the canopy door posts were notched to allow the Rivethead blocks to mount dire ctly on the aluminum door posts and thereby provide clearance for the door. I shimmed the Rivethead blocks so that there was minimal clearance between the doors and the blocks. This ensures that the doors remain correctly ali gned within the door opening. See #9. 14. Once the door pins engaged the Rivethead door block, it still took som e effort to fully engage the pins. There were several factors that added to the effort: =B7 There is a lot of internal friction the Van's ratchet mechanism . Application of white grease made operation *much* easier =B7 White grease on the door pins reduced the effort required to la tch the doors. =B7 There is a slight bow on the door. The long door pin should hav e a slight curve to ensure it does not bind against the in side of the door =B7 The further the door pins go into the door blocks, the greater the closing effort required. I reduced mine so that the only extend about =BC" through the aluminum door posts. =B7 The more pressure required to push the door in place so the pin s can engage, the more effort required to close the door =B7 If the door perimeter contacts the canopy anywhere, the effort required to close the door will increase. What I would do differently =B7 When bonding the door halves, use considerable more epoxy & flo x on the door perimeter especially close to the inner edge of the flanges t o be bonded. =B7 Pay more attention to the curves on the door pins (especially t he long ones). One of the pins was binding on the door interior thus increa sing the effort required to latch the door. =B7 Grease the ratcheting mechanism before starting the door fit. A lot of the door stiffness comes from the door mechanisms. When trying to a djust the fit, it would have beneficial to have the stiffness out of the eq uation as it was sometime difficult to know what was causing the fit proble ms. =B7 Install the door seals prior to doing the initial door fit. =B7 Pay more attention to where the door seals are being compressed too much when closing the door PRIOR to trimming the inside of the canopy flange. (In some places, I had to build up the inside of the canopy flange as I had to take more off the outside of the flange. To reduce door compres sion. =B7 Flox the fore and aft door pin guides when building the doors =B7 Install the Rivethead door blocks directly on the aluminum door posts rather than first fitting on the canopy. =B7 Shim the Rivethead door blocks to ensure door alignment when fi tting the doors Then end result of this is I can now close and latch both doors with only o ne finger of pressure on the inside door handle with only one finger of pre ssure on the outside of the bottom of the door. Cheers Les #40643 - Living in a f/g world




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