The Early BE2A had unequal span wings and a greater chord , lifting tailplane .
Later production ( From memory after May 1913?) BE2A ...The Wings Aerofoil section was changed from the earlier to an RAF 6 type ...In this , the main spars were positioned farther forward within the wing structure compared to the earlier unequal span wings .
Thus , with the fuselage to wing centre section struts in an unchanged position , the effect was to bring BACK the wing as a whole by some 5 " ( from memory ) ...
With the C/G of the body as unchanged , the lifting component and consequental Area required of the tailplane was therefor reduced .
The area of the stabalizer was where the reduction change was made , and employed a true radius curve to the leading edge . ( and this replaced the earlier multi radiused component .).
These same tailplane / elevator was continued into use on the BE2B , with only slight internal structural changes to the elevators .
With the wing moved back , a safer , pitching moment was obtained .
The relatively highly cambered Tailplane ribs are 3/16 birch ply webs with 5/8 x 5/32 thick cap strips of spruce .
The Spar is spruce and the tip ends crank down to meet the 1" dia steel tube LE/ tip , and is welded at its ends to the Rear spar , also a 1" dia. tube ..
The ribs and spar are attached at front and rear by wood screws and small clips sweated to the LE & Rear spar .tubes ,..
A central adjustable fixing is provided at the rear of the central rib , to adjust the T/Plane Incidence , it pivoting at the front , around the Leading edge tube and fixed either side to the body longerons .
Elevators have a LE of 7/8" steel tube and Trailing edge is 3/8" st tube ..All elevator ribs are of flanged steel sheet ,with greatest depth at appx 1/3 back from the LE....( Later these were strengthened with a double flange on the BE2B). All joints are welded .
Regards John McKenzie