|
| Span |
Area |
Empty Weight |
Payload |
Gross Weight |
Wing Load |
Water Ballast |
| m |
ft |
sq.m |
sq.ft |
kg |
lb. |
kg |
lb. |
kg |
lb. |
kg
/sq.m |
lb.
/sq.ft |
kg |
lb. |
| 13.11 |
43 |
19.51 |
210 |
213 |
470 |
195 |
430 |
408 |
900 |
20.91 |
4.8 |
0 |
0 |
| Aspect
ratio: |
8.81 |
| Airfoil: |
NACA 4301 2A |
| Structure: |
metal/ fabric 1-spar, constant chord, 1-strut braced wings; metal/ fabric tail; steel-tube/ fuselage |
| Engine: |
|
Comment:
The 2-22 was introduced in 1945 and became
(until superseded by the 2-23) the most used two-
place trainer in America. It was derived from
the SGU 1-7 and developed through A, B, C, D and
E models. The original 2-22 had a 204 kg/ 450
lb. Empty weight and 377 kg./ 830 lb gross with
no rear side windows and no doors. The A (3
built) was a redesign for the U.S. Air Force
Academy with lengthened nose, full canopy and
409 kg/ 900 lb gross weight. The B is the
original modified for 409 kg./ 900 lb gross
weight. The C incorporated the A and B changes
plus smaller ailerons; 103 built, including 28
kits (described as the 2-22CK). The D is the
orinal model with small ailerons. The E was the
last production model, with larger spoilers,
roomier cockpit, new canopy with wing root
changes to provide for a skylight.
Specifications are for the 2-22E. ATC |
|
