Chapter Project
In Final Building Stages
Shared Ownership Opportunity

EAA Chapter 282 has for a period of time been manufacturing an AcroDuster Too as a Chapter project. As you may know, acroduster too photoan EAA Chapter is prohibited by EAA National rules from operating a flying aircraft. Therefore, as soon as the project is completed it will be sold. As we are making careful but steady progress, the project is taking shape nicely and will be completed relatively soon. The wings and control surfaces are completed with the exception of final paint. The firewall forward is currently being assembled to position equipment and controls.

Afterwards the engine will be assembled utilizing a hollow crank, new cylinders, computer controlled digital pulse fuel injection and solid state ignition system. The airframe plumbing and wiring are nearing completion. Next, the structure and fitting of the canopy will be completed followed by covering of the fuselage and paint. The completion is now well in sight.

The Clearwater Flying Club, Inc. (CFC) has executed a purchase agreement to take ownership of the project at its completion with the intention of basing it at Clearwater Air Park and used exclusively by members of the club. The CFC has openings for membership and a share of the ownership of the AcroDuster. Priority for membership is offered to current members of EAA Chapter 282.

Contact CFC president Jim McCarthy or any of the individuals below for additional information regarding application to join and take advantage of this offer of a high performance, newly built, high technology engine, fully aerobatic two seat aircraft.

Jim McCarthy727-772-7052
Peter Hunt727-447-6409
Jim Porter727-481-7255

Acroduster Too

Yes, Acroduster Too not Two, II, 2 or The Sequel.

This hearty aerobatic biplane will pull 9 Gs. She is a Plans Build which means we at the EAA Chapter 282 are building her from scratch working from design proven plans and diagrams.


Acroduster Too Specs
Dimensions SPAN LENGTH HEIGHT WING AREA INCIDENCE SWEEP BACK
21' 5" 18' 6" 6' 10" 130 SQ FT 0° Both Wings 6° Top Wing
Weights ENGINE FUEL MAX EMPTY WT USEFUL LD GROSS WT AEROBATIC WT
200 HP LYCOMING 38 GALS 1050 LBS 750 LBS 1800 LBS 1630 LBS
Loads LIMIT LD ULTIMATE LD WING LD POWER LD I I
6g Pos/Neg 9g Pos/Neg 12.7 PSF 8.15 LBS/HP I I
Speeds TOP CRUISE STALL CLIMB RATE VNE I
160 MPH 150 MPH 60 MPH 2100 FPM 200 MPH I