VansAirForceForums  
Home > VansAirForceForums

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

- Today's Posts | Insert Pics

  #1  
Old 01-13-2020, 02:52 PM
FlyGuy65 FlyGuy65 is offline
 
Join Date: Oct 2015
Location: Houston (Kingwood), TX
Posts: 58
Default Basic pitot tube hole RV-7

Basic, per plans pitot tube installation. Plans seem to call for a hole to be drilled between two rivets joining the leading edge skin to the spar, just above an access plate nutplate. It would seem to make more sense to just enlarge one of the two predrilled rivet holes, rather than drilling an entirely new hole in the spar and trying to jam it between 2 rivets. Nothing on the wing has been riveted together yet, so I would not be drilling out a pre-existing rivet.

And am I wasting time on this to begin with - all of the search results seem to bring up folks using upgraded, heated pitot systems.

Thanks!

RV-7 Glacially slow build
Reply With Quote
  #2  
Old 01-13-2020, 07:58 PM
Charles in SC Charles in SC is offline
 
Join Date: Aug 2006
Posts: 703
Default

I am not sure that will give you enough room for the bulkhead type fitting that goes in the hole. I will look at mine tomorrow.
__________________
RV 7
Reply With Quote
  #3  
Old 01-13-2020, 08:20 PM
Robin8er Robin8er is offline
 
Join Date: Sep 2015
Location: Socal
Posts: 452
Default

Drilling the spar is what alot of people do. It's what the plans call for. No issues as long as you debur it and prime it.

I chose to drill just behind the spar and install a double in the skin.
__________________
RV-8 N695RA flying
Working on an RV-4

Born to fly, forced to work
Reply With Quote
  #4  
Old 01-14-2020, 07:21 AM
BillL BillL is offline
 
Join Date: Sep 2007
Location: Central IL
Posts: 5,514
Default

Quote:
Originally Posted by FlyGuy65 View Post
Basic, per plans pitot tube installation. Plans seem to call for a hole to be drilled between two rivets joining the leading edge skin to the spar, just above an access plate nutplate. It would seem to make more sense to just enlarge one of the two predrilled rivet holes, rather than drilling an entirely new hole in the spar and trying to jam it between 2 rivets. Nothing on the wing has been riveted together yet, so I would not be drilling out a pre-existing rivet.

And am I wasting time on this to begin with - all of the search results seem to bring up folks using upgraded, heated pitot systems.

Thanks!

RV-7 Glacially slow build
Ask Vans - - likely they want those rivets to carry load.
__________________
Bill

RV-7
Lord Kelvin:
“I often say that when you can measure what you are speaking about,
and express it in numbers, you know something about it; but when you
cannot measure it, when you cannot express it in numbers, your knowledge
is of a meager and unsatisfactory kind.”
Reply With Quote
  #5  
Old 01-22-2020, 12:53 PM
gmcjetpilot's Avatar
gmcjetpilot gmcjetpilot is offline
 
Join Date: Jan 2005
Posts: 4,283
Default

Yep the rivets are structural. The idea of putting it in the skin with doubler a variation... Great question but if you drill out rivet for pitot, I doubt the loss of one rivet would affect strength. The AN tube fitting of course is not structural but it will take something. In general stick with the plans.
__________________
George
Raleigh, NC Area
RV-4, RV-7, ATP, CFII, MEI, 737/757/767

2020 Dues Paid

Last edited by gmcjetpilot : 01-29-2020 at 07:22 AM.
Reply With Quote
Reply


Thread Tools Search this Thread
Search this Thread:

Advanced Search
Display Modes

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 02:13 PM.


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.