F1 Rocket Hangar

Speed...Speed and Looks...Looks and Speed!

  • The Airplane Builder
  • F1 Rocket Info
    • F1 Rocket Specs
    • F1 Rocket Build Tips
  • F1 Build Log
  • About
    • Disclosure
  • Stewart 51 Hangar
  • Resources
  • Ask Mike | Contact

Fuel Tank Rib Layout

May 26, 2024 by admin Leave a Comment

Today I’m working on the fuel tank rib layout for all the various holes that need to be added to the ribs. These are fuel transfer holes, venting hole, and holes for the fuel vent line.

There are significant differences here between the RV-4 plans and the HRII Sport Wing plans. In particular, the fuel vent holes on the upper side of each rib are enlarged to a 1-inch diameter size hole, vs the 1/4-inch size vent hole on the RV-4 drawings. The other 2 larger vent holes remain the same at the 1 1/2-inch size. Additionally, the fuel vent line hole goes just aft of the forward 1-inch fuel vent hole.

Another difference between the various plans are for the vent hole located in the center of the aft round rib stiffener stamping. The HRII plans call for the hole to be located 3 7/8-inch up from the bottom of the rib, and 3-inches forward of the aft flange (see the green circle in the image below). The RV-4 rib layout calls for this hole to be located in the center of that stamping. The location dimensions for this location are 4-inches up and 3 5/8-inch forward (red circle). I then split the difference and added the blue circle (just disregard that one, I didn’t use it).

After looking at pictures of several other F1 Rockets, I decided to stick with the hole location as shown in the RV-4 plans to keep this vent hole centered on the stamped area, which is what many other builders have done. As this is a venting hole and just allows fuel to transfer from one tank bay to the other, I don’t see significant difference between the two locations. If anyone knows of any reason for the change between the RV-4 and HRII drawings, please comment below to let me know.

Here are the close up details for the 1-inch vent hole at the forward end of the rib, along with the fuel line vent hole which is 7/16-inch diameter to accept the SB437-4 plastic bushing. You can also see that the vent hole is located at 11-inches forward of the aft flange. The HRII plans leave much to be desired in detailing the location of the fuel vent line hole location, as it’s not even specified on the drawings. The additional instructions provided on Vince’s Rocket website, just state that this hole needs to be located just aft of the 1-inch vent hole. As you can see below, it works out pretty well if you locate that vent line hole with the center of the stamped hole.

Well, that’s all I have for today.  Please comment. I love to hear from my readers.  Thanks again for coming along for this ride, you make my work worthwhile.

Filed Under: Fuel Tanks Tagged With: Fuel Tank, Wings

Leave a Reply Cancel reply

Your email address will not be published. Required fields are marked *

This site uses Akismet to reduce spam. Learn how your comment data is processed.

Profile Photo 1 Hello - My name is Mike and I'm a true believer that if you can imagine something, it's just a matter of bringing it into reality.

Categories

  • Empennage
    • Elevators
      • Left Elevator
        • Trim Tab
      • Right Elevator
    • Horizontal Stabilizer
    • Rudder
    • Vertical Fin
  • In My Travels
  • Primer
  • Tools
  • Uncategorized
  • Wings
    • Ailerons
    • F-404 Bulkhead
    • Flaps
    • Fuel Tanks
    • Leading Edge
    • Left Wing
    • Rear Wing Spar
    • Right Wing
  • Workshop

Tags

Ailerons Anti-Hang Up Guide Countersink Dimpling Doubler E-606-PP Elevator Empennage F-404 Bulkhead Flaps Fuel Sender Fuel Tank Hinge Horizontal Stabilizer HS-3101 HS-3201 Jigs Leading Edge Main Squeeze Mods Oshkosh priming rear spar Rib spacing Riveting Rudder Rudder Brace Horn Screw-ups Spar spreader bars Stiffener Tools Trap Door TrimTab Vertical Fin VS-001 VS-002 VS-803PP VS-808PP W-407B W-407C W-407D Wing Wings Workshop

Copyright © 2025 · Beautiful Pro Theme on Genesis Framework · WordPress · Log in