Project: N18TA   -  
            Listing for Category : fuselage
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Builder Name:DeWitt Whittington   -  
Project:   Glasair - Sportsman 2+2   -   VIEW REPORTS
Total Hours:3544.2
Start/Last Date:Nov 22, 2003 - Sep 30, 2021
Engine:Lycoming O-360-A1A 180hp
Propeller:Hartzell Constant Speed 72"
Panel:GRT HX (3), GTN650, GTR200, VP200, Trio Pro Pilot,
 
Friendly URL: https://eaabuilderslog.org?s=N18TA

Home or Last Project Picture

Sep 17, 2014     Floor boards up front - (35 hours)       Category: Fuselage
Cutting and fitting the front floorboards was a pain. One small device made it a bit easier. Namely "locating" pin, pointed on one end and cylindrical on the other. Those pins fitted in the holes where clip nuts would fit. That allowed us to mark the "blind" side in order to drill the holes for the hold-down screws accurately


 
Oct 28, 2008     Tail cone fairing and very back end of fuselage - (10 hours)       Category: Fuselage
The tail cone which we fitted to the aft end of the Sportsman fuselage. The elevator pushrod extends into this area and attached to the elevator horn.


 
Nov 17, 2007     Fuselage recesses for flap inner corners when wings are folded - (10 hours)       Category: Fuselage
Our earlier version of the Sportsman kit required we cut holes in the top of the fuselage in the rear of the cabin to accommodate the inner edge of the flaps when the wings are folded. Covers for these two oval holes must be removed before the folding process. The wing dihedral was slightly increased in later serial numbered kits so these holes are not required.


 
Jan 18, 2005     Fuselage to cage attachment - lots of fitting and shimming - (100 hours)       Category: Fuselage
One of the first multi-part job we attacked when we moved from the tail kit to the fuselage kit, was finishing the attachment of the welded CrMo tubing cage to the two halves of the fiberglass shell. The shell halves were pre-attached to each other, one of the features of a Quick Build kit. But that attachment was only at a few places. You'll see in the following photos that we fabricated aluminum parts, and used vinyl ester resin mixed with glass fiber, flox and microbeads mixtures to seat, and shim the attachments to the fuselage.


 
Aug 08, 2004     Elevator area of the fuselage - (80 hours)       Category: Fuselage
The fuselage tapers down greatly to the very aft end where the horizontal stabilizer if attached. It order to hold the stabilizer in position rigidly, we laid up fiberglass angles to which we attached a rather thick aluminum plate which we trimmed to fit. Then we drilled a dozen holes for AN3 bolts. On the four fiberglass angles, we mounted 12 nutplates for the bolts. This torque plate greatly stiffens the fuselage so it resists the loads on the elevator.


 


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