Date
Builder
Hours
Tasks
3-10-02
RRS
1.0
Began Construction.  Edge-shaped (and polished) the strengheners for the rear
 spar.
4-1-02
RRS
NA
Ordered tools from Avery and Cleveland. Parts were backordered, so all of the important tools were not received until 5-20-02.
5-21-02
RRS
0.5
Clecoed parts for rear stabilizer spar.
5-25-02
RRS/CMS
2.0
Officially began work on the plane.  Drilled and deburred rear stabilizer spar.
5-27-02
RRS/CMS
2.0
Riveted bearing support on rear spar.  Began drilling front spar.
5-29-02
RRS
1.0
Front spar on Horizontal Stabilizer.
5-30-02
RRS
2.0
Front spar work.
5-31-02
RRS
2.0
Front spar, rear spar.
6-1-02
RRS/CMS
4.0
Clecoed on skins, assembled tail
6-2-02
RRS/CMS
2.5/1.5
Horizontal Stabilizer final prep; clecoed the fin together.
6-3-02
RRS
2.0
Horizontal Stabilizer drilling; dulled bolts at Bob Miller's.
6-5-02
RRS/CMS
2.0 
Match-drilled 3/4 of Horizontal Stabilizer Skin.
6-9-02
RRS
0.5
Finished match-drilling HS.
6-10-02
RRS/CMS
2.5
Disassembled HS, began deburring and dimpling HS.
6-11-02
RRS
1.0
Dimpled right side of HS.
6-18-02
RRS/CMS
2.5
Deburred and dimpled HS.
6-19-02
RRS
1.0
Finished dimpling HS parts.
6-22-02
RRS/CMS
4.0
Prepared HS parts for priming (alodine)
6-23-02
RRS
1.0
Primed HS parts.
6-24-02
RRS
2.0
Began riveting the HS.
6-25-02
RRS/CMS
2.5
Finished riveting the HS spars.
6-26-02
RRS
3.0
Final assembly of HS.
6-27-02
RRS
0.5
Attached front spar.
6-28-02
RRS
2.5
Bucked spar rivets.
7-1-02
RRS
2.0
Final inspection before closing HS.  Replaced #4 rivet in tip connection.  
Began riveting the front spar in place.
7-2-02
RRS
3.0
Finished metal part of HS.  Torqued bolts and finished riveting spar.
Began work on VS.  Match-drilled rudder brackets; deburred and fluted ribs.
7-3-02
RRS/CMS
4.0
Match-drilled and deburred VS (inside skin.)
7-14-02
RRS
2.0
Finished deburring and dimpling vertical fin.
7-15-02
RRS
4.5
Prepared and primed VS.  Began riveting rear spar. (Uncle Mike and Mom put in 
rivets.
7-17-02
RRS/CMS
5.0
Riveted the VS, performed a visual inspection before closing VS with the rear spar.
All rivets looked uniform.  We also randomly checked rivets with a rivet guage.
7-18-02
RRS
2.0
Finished VS.  Trimmed stiffeners for rudder.
7-19-02
RRS/CMS
7.0/2.0
Continued work on rudder.  MAtch-drilled stiffeners and cut elevator stiffeners.
Worked on rudder frame, fabricated extra parts for rudder.  Deburred stiffeners and skin.
7-20-02
RRS
5.0
Finished elevator stiffeners.  Match-drilled elevators.
7-20-02
CMS
1.0
Dimpled stiffeners, helped to match-drill elevators.
7-21-02
RRS
2.0
Finished prepping the rudder and elevator stiffeners.
7-22-02
RRS
3.0
Deburred and dimpled the rudder and two elevator surfaces.
7-23-02
RRS
2.0
Deburred and sanded skins for rudder and elevator.
7-24-02
RRS
8.5
Prepped and primed control surfaces, elevator stiffeners.
7-25-02
RRS
2.0
Finished riveting the stiffeners; began deburring rudder parts.
7-26-02
RRS
2.5
Rudder frame fitting and match-drilling.
7-27-02
RRS/CMS
6.0/2.5
Rudder deburring and dimpling, final fitting of rudder parts.
7-28-02
RRS
5.0
Right elevator assembly, fitting and match-drilling.
8-3-02
RRS
3.0
Fitted left elevator together.
8-4-02
RRS
2.5
Match-drilled left elevator.  Began deburring.
8-9-02
RRS
2.0
Deburring and countersinking/dimpling left elevator.
8-11-02
RRS
6.0
Primed components for rudder and elevators.  Riveted in the trim tab cover
plate assembly.
8-12-02
RRS/CMS
3.5
Began riveting the rudder frame.
8-13-02
RRS
6.0
Continued riveting on rudder.  Started riveting left and right elevator
structures.  Had several "tools" made by Bob Miller: small bucking bar and
several squeeze shims.
8-14-02
RRS
1.5
Riveted left elevator frame together.
8-25-02
RRS/CMS
6.0
Completed left elevator tab folds, mixed RVT (tank sealant) and applied it to 
all stiffeners in the training edges; assembled the skeletons and skins, clecoed
them.
8-28-02
RRS
3.0
Riveted surfaces.
8-30-02
RRS
2.0
More riveting on surfaces.
8-31-02
RRS
4.0
Riveted elevators, rolled rudder front skins.
9-1-02
RRS
2.0
Closed rudder front skins, pop rivets.
9-2-02
RRS/CMS
6.0
Deburred trim tab surface, horns and spar; trimmed off excess on the hinge.
Riveted part of the trim tab spar to the skin, rolled both elevator edges.
9-11-02
RRS
1.5
Straightened the bends on teh left elevator.  Drilled out rivets in the elevator.
9-15-02
RRS/CMS
4.0
Drilled out and re-riveted some rivets on the elevator near the trim tab area
to get rid of a bubble in the sheet metal.  Further bending and final riveting
of elevator tabs near trim tab area.  RIveted the hinge to the trim tab.  Mounted
3 rod-ends into the rudder.
9-18-02
RRS/CMS
2.0
Attached rudder to fin.  Riveted curved edge of the right elevator.
10-7-02
RRS/CMS
2.0
Match-drilled control surface fiberglass tips using #30 bit, deburred and dimpled.
Sealed the vertical fin fiberglass cap with fiberglass resin (Bondo.)
10-12-02
RRS/CMS
6.0
Trimmed the stabilizer for the fiberglass tips (x4); trimmed off excess on 
fiberglass tips, match-drilled tips with horizontal stabilizer skins.  Made
styrofoam molds for tips.
10-18-02
RRS
4.0
Fiberglass tip work.  Closed ends of fin and stabilizer caps.  Riveted fin cap.
Riveted tips on stabilizer.  Match-drilled tops of rudder.
10-25-02
RRS/CMS
3.0
Deburred bottom of rudder (metal) and countersunk fiberglass cap for bottom
of rudder; pop-riveted fiberglass cap to rudder.
10-31-02
RRS
2.5
Riveted right elevator tip.  Epoxy on end and then resin.
11-02-01
RRS
 
Sanded tip (time recorded in 10-31-02.)
11-02-02
RRS/CMS
4.0
Used dremmel on fiberglass tip on left elevator tip, expoxy and resin.  Riveted
the front seam.  All parts of the tail assembly are now complete.
TOTAL MAN HOURS FOR EMPENNAGE: 244  
Next Log Section