VansAirForceForums  
Home > VansAirForceForums

- POSTING RULES
- Donate yearly (please).
- Advertise in here!

- Today's Posts | Insert Pics


Go Back   VAF Forums > Model Specific > RV-12/RV-12iS
Register FAQ Members List Calendar Today's Posts

Reply
 
Thread Tools Search this Thread Display Modes
  #61  
Old 07-17-2018, 06:01 AM
joedallas's Avatar
joedallas joedallas is offline
 
Join Date: May 2010
Location: Spring Hill Fl
Posts: 734
Default Sorry for the confusion

Sorry for the confusion

I posted the photos that Bob Lindell sent me with his permission.

This page is posted to help notify builders of the seriousness of SB 18-07-05

I added a few notes to the page

http://joesrv12.com/Builder%20Lo..._Bullitens.htm

Joe Dallas
__________________
Joe Dallas
Kit-#12400
www.joesrv12.com
www.EAA1298.com

Last edited by joedallas : 07-17-2018 at 06:21 AM.
Reply With Quote
  #62  
Old 07-17-2018, 11:39 AM
Hotscam Hotscam is offline
 
Join Date: Mar 2011
Location: Bosschenhoofd, Netherlands
Posts: 151
Default

We inspected the hubs of both our RV12?s and found no cracks, but a very time consuming job to set the correct pitch again to get the specified rpm value at WOT.
As we are not keen at all to do this every 50 hours we ordered new design hub plates at Sensenich.
They charge $ 195 per unit. 😡
__________________
Jack Netherlands

PH-SEP and PH-SES

RV12 #120519 and #120790
Hobbs 700+ hours and 400+ hours
Dual SV1000 Skyview 15, Pocket FMS and Powerflarm 6.0 (ADSB)

RV10 PH-USN Hobbs 350 hours
Reply With Quote
  #63  
Old 07-17-2018, 02:02 PM
Piper J3's Avatar
Piper J3 Piper J3 is online now
 
Join Date: Nov 2014
Location: Hinckley, Ohio
Posts: 2,056
Default

Quote:
Originally Posted by Hotscam View Post
We inspected the hubs of both our RV12?s and found no cracks, but a very time consuming job to set the correct pitch again to get the specified rpm value at WOT.
As we are not keen at all to do this every 50 hours we ordered new design hub plates at Sensenich.
They charge $ 195 per unit. 😡
You replaced just the front plate or entire hub? I believe the hub is machined as a matched assembly with matching serial numbers...
__________________
-
Jim Stricker
EAA #499867
PPL/ASEL 1970 - Sport Pilot since 2007
80 hrs Flying Aeronca Chief 11AC N86203
1130 hrs Flying 46 Piper J-3 Cub N6841H
Bought Flying RV-12 #120058 Oct 2015 with 48TT - Hobbs now 618

LSRM-A Certificate 2016 for RV-12 N633CM
Special Thanks... EJ Trucks - USN Crew Chief A-4 Skyhawk
MJ Stricker (Father & CFI) - USAAF 1st Lt. Captain B-17H
Reply With Quote
  #64  
Old 07-17-2018, 03:40 PM
Hotscam Hotscam is offline
 
Join Date: Mar 2011
Location: Bosschenhoofd, Netherlands
Posts: 151
Default

They asked for the serial numbers of the hubs and quoted all the parts required including fasteners, so I may assume it is correct.
I will pick them up at Oskosh so will see what we get
__________________
Jack Netherlands

PH-SEP and PH-SES

RV12 #120519 and #120790
Hobbs 700+ hours and 400+ hours
Dual SV1000 Skyview 15, Pocket FMS and Powerflarm 6.0 (ADSB)

RV10 PH-USN Hobbs 350 hours
Reply With Quote
  #65  
Old 07-17-2018, 03:47 PM
Hotscam Hotscam is offline
 
Join Date: Mar 2011
Location: Bosschenhoofd, Netherlands
Posts: 151
Default

I re-read their mail and it clearly says top half and fasteners
__________________
Jack Netherlands

PH-SEP and PH-SES

RV12 #120519 and #120790
Hobbs 700+ hours and 400+ hours
Dual SV1000 Skyview 15, Pocket FMS and Powerflarm 6.0 (ADSB)

RV10 PH-USN Hobbs 350 hours
Reply With Quote
  #66  
Old 07-17-2018, 04:47 PM
DonFromTX's Avatar
DonFromTX DonFromTX is offline
 
Join Date: Oct 2010
Location: La Feria Texas
Posts: 3,822
Default

That must be a change. When I upgraded mine a year or so ago, I had to buy the entire hub and send my blades to them for whatever they done.

Quote:
Originally Posted by Hotscam View Post
I re-read their mail and it clearly says top half and fasteners
__________________
A&P, PP-SEL, Pathological Flier, EAA Technical Counselor
EAA Chapter 595 President,http://www.595.eaachapter.org/index.htm
Retired US Army Officer
Reply With Quote
  #67  
Old 07-17-2018, 09:57 PM
rvbuilder2002's Avatar
rvbuilder2002 rvbuilder2002 is offline
 
Join Date: Jul 2005
Location: Hubbard Oregon
Posts: 9,026
Default

Quote:
Originally Posted by Hotscam View Post
We inspected the hubs of both our RV12?s and found no cracks, but a very time consuming job to set the correct pitch again to get the specified rpm value at WOT.
As we are not keen at all to do this every 50 hours we ordered new design hub plates at Sensenich.
They charge $ 195 per unit. 😡
Assuming you were happy with performance before removing the propeller, returning to a specific pitch/performance value is a rather simple process.
If the set pitch value is recorded in the log book or you measure it before removing the propeller.
As long as you have that number, getting setting back to that pitch will give you the same performance you had before.
__________________
Opinions, information and comments are my own unless stated otherwise. They do not necessarily represent the direction/opinions of my employer.

Scott McDaniels
Van's Aircraft Engineering Prototype Shop Manager
Hubbard, Oregon
RV-6A (aka "Junkyard Special ")
Reply With Quote
  #68  
Old 07-18-2018, 12:45 AM
Hotscam Hotscam is offline
 
Join Date: Mar 2011
Location: Bosschenhoofd, Netherlands
Posts: 151
Default

Thats what I did but the plane needs to be exactly level and the angle tends to change a little when you tighten the bolts.
I took the spark plugs out to move the prop without disturbing the level of the plane.
After two iterations I got it within 100 rpm of the original WOT rpm.
It took me 4 hours for two 12?s
__________________
Jack Netherlands

PH-SEP and PH-SES

RV12 #120519 and #120790
Hobbs 700+ hours and 400+ hours
Dual SV1000 Skyview 15, Pocket FMS and Powerflarm 6.0 (ADSB)

RV10 PH-USN Hobbs 350 hours
Reply With Quote
  #69  
Old 07-18-2018, 03:51 AM
Piper J3's Avatar
Piper J3 Piper J3 is online now
 
Join Date: Nov 2014
Location: Hinckley, Ohio
Posts: 2,056
Default

Quote:
Originally Posted by Hotscam View Post
Thats what I did but the plane needs to be exactly level
Not so… Refer to Page 07 of Section 47 Construction Drawings. The plane does not need to be level at all and can even change angle between measurements.

The prop pitch angle is relative to the canopy longeron regardless of aircraft level. Each time the prop is moved recheck the digital level on the longeron before measuring the blade pitch. If the aircraft “level” has been disturbed while moving the prop simply re-zero the digital level on the canopy longeron before continuing to measure blade pitch.

It is not necessary to remove spark plugs or even upper cowling.

Tools required include a good quality bubble level and two wooden spacer blocks to level prop hub. Mark blocks L-R, forward and top-side so they are placed same exact position on hub each time. Likewise, mark bubble level so it is not “reversed” for each use.

I use Vans sheet metal TOOL-00002 Prop Pitch Bracket and same Craftsman Multifunction Digital Torpedo Level # 48295 as shown in construction drawings. For each measurement of blade pitch first place digital level on longeron and verify zero and re-zero if necessary. Next place the magnetic base of the digital level on the Prop Pitch Bracket (PPB) and finally place digital level/PPB onto the prop. Use gentle finger pressure to seat the PPB against the front edge of the prop.

I have not found tightening of the front prop hub to influence final blade angle. I snug only outer bolts and leave center bolts loose while adjusting blade pitch. When one blade pitch is correct, snug outer bolts even further before setting second blade.

Total time for above procedure is approximately 30 minutes and will attain relative pitch between both blades to within 0.1° angle.
__________________
-
Jim Stricker
EAA #499867
PPL/ASEL 1970 - Sport Pilot since 2007
80 hrs Flying Aeronca Chief 11AC N86203
1130 hrs Flying 46 Piper J-3 Cub N6841H
Bought Flying RV-12 #120058 Oct 2015 with 48TT - Hobbs now 618

LSRM-A Certificate 2016 for RV-12 N633CM
Special Thanks... EJ Trucks - USN Crew Chief A-4 Skyhawk
MJ Stricker (Father & CFI) - USAAF 1st Lt. Captain B-17H

Last edited by Piper J3 : 07-18-2018 at 03:55 AM.
Reply With Quote
  #70  
Old 07-18-2018, 05:52 AM
joedallas's Avatar
joedallas joedallas is offline
 
Join Date: May 2010
Location: Spring Hill Fl
Posts: 734
Default Not With my Inclinometer

SPI

0.10 dg Resolution Digital Combination Protractor and Inclinometer

SPI Tronic Price $243.97


0.10 dg Resolution Digital Combination Protractor and Inclinometer
Accuracy (Degrees) 0.1 (Level 10 ); 0.1 (Plumb 10 ); 0.2 (Maximum Error)

.1 Degree = 6 minute arc . 2 Degree = 12 Minute arc


With four moves of level and the built in error of .2 in the level how is this possible ?

Keeping the aircraft level makes this more possible ?

MY view


Joe Dallas


Quote:
Originally Posted by Piper J3 View Post
Not so… Refer to Page 07 of Section 47 Construction Drawings. The plane does not need to be level at all and can even change angle between measurements.

The prop pitch angle is relative to the canopy longeron regardless of aircraft level. Each time the prop is moved recheck the digital level on the longeron before measuring the blade pitch. If the aircraft “level” has been disturbed while moving the prop simply re-zero the digital level on the canopy longeron before continuing to measure blade pitch.

It is not necessary to remove spark plugs or even upper cowling.

Tools required include a good quality bubble level and two wooden spacer blocks to level prop hub. Mark blocks L-R, forward and top-side so they are placed same exact position on hub each time. Likewise, mark bubble level so it is not “reversed” for each use.

I use Vans sheet metal TOOL-00002 Prop Pitch Bracket and same Craftsman Multifunction Digital Torpedo Level # 48295 as shown in construction drawings. For each measurement of blade pitch first place digital level on longeron and verify zero and re-zero if necessary. Next place the magnetic base of the digital level on the Prop Pitch Bracket (PPB) and finally place digital level/PPB onto the prop. Use gentle finger pressure to seat the PPB against the front edge of the prop.

I have not found tightening of the front prop hub to influence final blade angle. I snug only outer bolts and leave center bolts loose while adjusting blade pitch. When one blade pitch is correct, snug outer bolts even further before setting second blade.

Total time for above procedure is approximately 30 minutes and will attain relative pitch between both blades to within 0.1° angle.
__________________
Joe Dallas
Kit-#12400
www.joesrv12.com
www.EAA1298.com

Last edited by joedallas : 07-18-2018 at 08:23 AM.
Reply With Quote
Reply



Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

vB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Forum Jump


All times are GMT -6. The time now is 11:06 AM.


The VAFForums come to you courtesy Delta Romeo, LLC. By viewing and participating in them you agree to build your plane using standardized methods and practices and to fly it safely and in accordance with the laws governing the country you are located in.