G2EA 2
Production basis Production Certificate No. 101
Equipment: The basic equipment as prescribed in the applicable airworthiness regulations (See
certification basis) must be installed in the aircraft for certification.
NOTE 1. Suitable placards to cover the various pilot and passenger weights must be installed in full view of the pilot
as determined from the manufacturer's weight and balance report.
NOTE 2. The following placards must be installed in full view of the pilot:
(a) "Solo front seat only."
(b) "Max. glide or dive 98 m.p.h.
Max. aero tow 98 m.p.h.
Max. auto-winch tow 69 m.p.h.
NOTE 3. Approved safety belt and shoulder harness required for each occupant.
NOTE 4. Each Model SGS 2-33A glider assembled from a kit is designated Model SGS-2-33AK. These K models
will be eligible for an airworthiness certificate when accompanied by an affidavit certifying that the glider is
constructed in exact accordance with the approved drawings and manual, and that the parts and materials
furnished by the manufacturer in the kit have been used; and further when the following inspections have
been satisfactorily passed:
(a) An inspection for workmanship, materials, and conformity before any covering is applied. (All
woodwork may be sealed.)
(b) A final inspection of the completed glider.
(c) Check of flight characteristics.
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