Page No. 1 2
Rev. No. 2 2
DEPARTMENT OF TRANSPORTATION
FEDERAL AVIATION ADMINISTRATION
G2EA
SCHWEIZER
Revision 2
SGS 2-33
SGS 2-33A
SGS 2-33AK
August 1, 1973
GLIDER DATA SHEET NO. G2EA
This data sheet which is a part of type certificate No. G2EA prescribes conditions and limitations under which the product for
which the type certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations.
Type Certificate Holder Schweizer Aircraft Corporation
County Airport
Elmira, New York 14902
I - Model SGS 2-33, 2 PCLM, Approved February 10, 1967; Model SGS 2-33A, 2 PCLM, Approved March 7, 1968;
Model SGS 2-33AK, 2 PCLM, Approved April 19, 1973. Model SGS 2-33A same as SGS 2-33 except for larger rudder with
aerodynamic balance; Model SGS 2-33AK is same as Model SGS 2-33A constructed from a kit (see Note 4 for eligibility
requirements)
Type Class II, Utility
Airspeed limits
(CAS) Vne-Glide or dive 98 m.p.h.
Vta-Airplane tow 98 m.p.h.
Vtaw-Auto-winch tow 69 m.p.h.
C.G. range (+11.9) to (+19.8) (Fuselage Sta. 78.2 to 86.1)
Maximum weight 1040 lb.
No. seats 2 (1 at -23) (1 at +8)
Baggage None
Control surface movements Limits
Elevator Up 23° Down 23° + 2°
Rudder Left 30° Right 30° + 2°
Aileron Up 38° Down 18° + 2°
Dive Brakes Top Up 85° Bot. Down 75° + 5°
Serial nos. eligible 1 and up
Specifications Pertinent to All Models
Datum Wing leading edge at root (Fuselage Sta. 66.3)
M.A.C. 53.54 in. (L.E. of M.A.C. 2.35 in. aft of wing leading edge at root)
Leveling means Top of upper longeron aft of wing.
Certification basis FAR 21 and Basic Glider Criteria Handbook, 1962.
Date of Application for Type Certificate April 1, 1966.
Type Certificate No. G2EA issued February 10, 1967.
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