STC SA1901SW

r / *- •**" '* ' '"', Hnittd of amtrica Bepartment of ^Transportation —federal SDiation administration mpplementalCertificate SA1901SW Sviclt Aircraft Corp.

Rt. 1, Box 163B Lewigville, Texas 75074 04 Civil Air 696 : lay lore raft BC12D : Clipped wings, revised control aysten and added

•Heron and elevator servo tabe according to Swick Clip-Wing Taylorcraft Modification Drawing Liat dated 10/16/76 or subsequent FAA approved revision.

See Continuation Sheet, page 2, a part of this STC.

May 10, 1973 AUKUSt 20 1974 A^ 'U'.Jne' S 4/7/75; 10/20/76; 3/29/77 Revision 3 £gDon P. Uataon Chief, Engineering and Manufacturing Branch _ alteration of this certificate is punishable by a fine of not exceeding SI ,000, or imprisonment tint exceeding 3years, or both.

This certiftiate may tie transferred in accordance with FAR 21.47, FAA FOIM 8110-2 (10-63)

United £tatu of America Bepattmcnt of Transportation— Jptdtral atriation administration Supplemental ICgpe Certificate(Continuation £heet) SA19QISW Revision 3 Limitations and Conditions :

1. C.G. fwd 14.2 aft 19.5

2. Control Surface Travels (Tolerances + 2°) Aileron tabs + 20° Aileron tabs ± 8° (Controlled by aileron position) Elevator tabs relative to elevator 12° nose up 7° down Additional travel controlled fay elevator position 5, Ltmllng means - top of horizontal stabilizer with 1.00" block on rear sp&r tube.

4. FAA Approved installation of Continental C-85 engine is required, or eligibile with STC SA1905SW installed. The drawings required for STC SA1905SU are shown in the drawing list.

FAA FORM BUQ-2-1 <io-69) This certificatt may bi transferred in accordant! with FAR 21.47.

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