# STC SA1901SW - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Swick Aircraft Corp - Description: Clipped wings, revised control system and added aileron and elevator servo tabs. - Status date: March 29, 1977 - Data sheets: A-696 - Certificate PDF: https://openairdocs.org/files/sha256/4b/c1/4bc1c25115877b01a8ea35b93d54e37c1a271bd1aee62c068d69e3ec54e22652 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/9E4E6810D748FD0186257D7A00535B62.0001 - Page: https://openairdocs.org/stc/SA1901SW ## ADs that name it None. ## Approved models (1) - Taylorcraft 2000 LLC BC12-D (TCDS A-696) ## What the certificate says Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record. 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