|
|
|
|
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 |
|