Top Flite Red Box Zero

Wing Construction Log

For Wayne Degeorge, West Seneca, NY

Schwing RC 2003 all commercial rights reserved.

 

This Zero wing will include functioning split flaps and B&D mechanical retract installation.

 

PHASE ONE Jaunary 28,2003

 

Step One- Layout and Parts Modifications for Retractable Landing Gear Installation.

Modifications to ribs 3,4,5,and 6 required. The retract unit location was determined by the fixed gear strut position and length from the wing plan’s front view. Hardwood mounting rails will extend from rib 4 to rib 6. Rib 3 must be modified also to accommodate the retracted wheels.

 

Step Two- Plywood Rib Doublers Required

The unit located over the plan top view. Ribs must be modified to accept 1/2x1/4 hardwood mounting rails from r4-r6. These 3 load-bearing ribs are double with plywood. The R3 rib is also doubled since so much of it has to be cut out for the wheel well. Relief cuts for the servo pushrod,(or hoses for pneumatics) have to be made also.

Retract modified ribs ready to install are shown below. Note right and left method required when fabricating these ribs. Arch shaped cuts in the load bearing ribs are large enough to pass the pushrods required for mechanical retracts, not to mention scale struts. R3 doubler parts were trimmed and used for doubling R4’s, and new 1/8 lite-ply doublers were made for R3 and R6 ribs.

 

 

Once the ribs have been modified wing construction can proceed as described.

 

Phase 2- Build and Join the Wing Frames

Note W7 ribs are slightly undersized in both chord and thickness, 1/16 shims were required to fill the gap at the trailing edge joint. A cap-strip will have to be added to the top aft section of ribs W7 also, before final sanding of the wing frames for sheeting.

 

Basic frames complete. Rib notches behind the main-spars are for routing of bellcrank pushrods. In this case they’ll be the wiring route for aileron servos.

Plane the top taper to airfoil shape on the 7/16 trailing edge before adding 3/8 leading edge of the fixed flap section.

 

The flaps on the Zero are the “split” type, top section in this area is fixed. To make the ribs 3/32x3/8 balsa is cut to length and than each piece split diagonally with a razor saw, providing 2 sets of ribs.

 

Spars trimmed to proper dihedral angle.

 

Plywood joiners in place at the leading edge, mainspar and trailing edge. Trailing edge filler block has to be installed first.

With the right wing half still pinned over the plan, height under the left tip at the mains-par should be 6-5/8”. Blocks placed under W7 with jig tabs in prevent unintentional warping.

 

January 29, 2003 

 

Phase 3- Prep for retract installation.

Phase 4- Sheet the Wing Top

The Zero’s wing was sheeted with pre-joined 3/32 sheets from the original kit. Skins were joined with Elmer’s carpenter’s glue (aliphatic resin) to insure a uniform surface after sanding. If CA is used the seams will be more resistant to sanding than the rest of the wood skins, leaving hard ridges.

The oversize skins were fixed permanently to the frames with Everbond epoxy. A very thin film was spread with a squeegee across the inside surface of the balsa skin and each rib top was painted with epoxy. Jig tabs on the rib bottoms maintain warp-free alignment while the epoxy sets under weight overnight.

 

Magazine stacks work well for this job. By adding a trailing edge stock wedge between the stack and skin over the leading edge area, good contact is maintained while the epoxy cures for accurate airfoil shape.

February 3, 2003

Retract Installation

Split flap prep work must be completed before the bottom of the wing is skinned.

 

      WING DIRECTORY      Retract Directory

 

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