STC SA2386SW

United States of America Bepartmcnt of Transportation— federal aoiation administration supplemental t:uje Certificate SA2386SW Avicon Development Corp.

701 North Central Expressway Richardson, Texas 78050

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twfw^ 3 C 1 vi 1 Air See Limitations and Conditions See Limitations and Conditions see Limitation* and Conditions installation of S.A.P.E., EOT and CRT Systems according to Installation Drawing 900130. Revision B, dated 1/18/77, or later PAA Approved revision.

Thlt modification IB eligible on aircraft listed on Eligibility List, Sheets 1,2,3 attached to this STC, or later FAA approved list.

Thia installation is not eligible to replace on existing required system on the airplanes.

Compatibility of this modification with other previously approved modifications Mist be determined by the Installer.

^ina'.tta/a' tv/u'e/t/.ti, £wJx JefTni#Tji&t^ February 14, 1976 January 25, 1977 August 3, 1978 Revision 1 (Signature) Don P. Watson Chief, Engineering and Manufacturing Branch

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Attacttnent : - SA2386SW TWIN I'NC.INi; AIRCRAFT - STC APPROVED Sheet 1 BEECH

BRITTEN CESSNA PIPER TCJ-JIIMHhR 5A4 A12CE 3A16 A17EIJ A29EU 3A10 3A25 3A11 A2CE A6CE A7CE A IF: A A8EA A3SO .r.O Thru .150 60, A60, B60 U95A Thru 1-95, 95-55 thru 95-C55A HM-2. 2A, 2A-2 thru 21 HN-2A Mk. Ill 310, MOA thru 310R, 1:310 (All Series) T310 fAll Series

320. 320-1, 320A thru 320F, 340, 340A

321. OF.-2 336 337, 337A, H, C; M/T337A thru G 401, 4DlA,li; 402, 402A.B; 411. 411A, 414, 121, 421A thru C.

PA-30, ]'A-3f), PA-40 PA-31, PA-31-300 PA-32-260, -32-300, -32S-300, -32R-30fo A7SO PA-34-200. PA-31-200T

ROCKWELL INTERNATIONAL 6A1 2A4 SMITH. TF.n (AEROSTAR) A11WE A17WK APPLICABLI; SYSTEM:

Fr,T KIT AT5 ( ) or AT3 ( ) 50(1, 5C.O, 560A, 5f,OE, 500-A, ^OOB, 5000,

r.oor.SfiO-l;, hiitl, 6801:, 720, 680F, 6SOFT,, 685 3f»0, -100 600, (.01 ^T2 ( ) nr AI t ( ) FEDEittL AVIATION ADMIillSTtlATlOH GOUTHV/S3T REGiCN FLlGliT STANDARDS DIVISION

ENGLIJEEBINS APPROVED

SUCJSCTTO INSPECTION Kits eligible only on basic engines covered by T.C. numbers shown above.

Attachmenc - SA2386S¥

SINGLE ENGINE AIRCRAFT - STC APPROVED Sheet 2 BEECH BELL

BELLANCA CESSNA

LNSTROM GRUMAN AMI-RIC^N I It LI 0 HYNES

INTERCEPTOR

TC NUMBER ~~ATE!r—111 3A15 5A3 ILSSW H2CE 1A3 A18CE 3 AID 709 3A12 3A17 13CK A 2 OCR 5A6 3A13 3A24 A9CE A4CC A16CI:

3A21 5A5 3A14 MICE;

A11EA A!()[-: A US H3SW 3AJ8 MOIMil, 23, A2^ rliru A2.^-I!', 10A, B19 35, ASf, thru G35, And 35R 35-33 thru 3fj-C33A, 033-033. H3S-V35B, 36, A36.

•IS, A45, B4S, T34. T34A, T34B nii-i.iii on- 131:

14-1!) (all seriesl 17-30, 31, 31TC 17-10A, 17-31A. I7-3IATT 150 thru A150M 170 172, 172A thru 172N 175 thru R172J 177, 177A.B.C 177Ri;

180 thru 180J 182, 1K2A thru 1H2Q - IS.'., ISf.A thru 1BSI-, AlSr.H.F.

18S. 1H8A.B. A1SH. A188A.H 206, II2H6 (all series), P2fl6(all series TIL'iK.t fall s.-riesl, rP20(,(all series).

207/T207, 207A7T207A 2in, 1'liH thru 210!., T210F thru T210I,, 210-S, f>A 3 Of, A 30Sf(, 30511, To-lit or To-lP 1-28, l:2«A tliru C, 2HO(all series) AA-I , -1A, -lit SA, H-250, M-2:'r., irr-j!is 2d!lA thru 2H01) iZt.^L ." . "' •! ADf«S;;il5TRAT!OrJ '"•; -.- ^:^~!QN FL™;!,-,-' "^tNLi.Vc.,.. !

U3JECT -• -. '_ ;fc !Kits eligible only on basic engines covered by T.C. ^numbers shown above.

Attachment - SA2386SW Sheet 3 SINGLE I-NGINI: (CON"T)

CONSOLIDATE AtRONAUTICS PlPBR

TC NHMM-K 1A13 1A4 \\h 1A10 1A15 ROCKWELL INTERNATIONAL Al ISO A12SO M')IH:i. Dl-SIfl.

c-i, -.:, I.A -i, -u. -IP, -jnn I'A-Jd, -205, fall series) PA-22(A11 series) I'A. 23(;ill scrios) PA-152S PA-24 (all series) 111

11..', 114, 11 2 K SCNWKIZI'R A15I-A M.MILE ONliY ,1 AVION

MORAVAN NATIONAL

CORPORATION 3A23 2 A3

•\fiSW 782 A301-U '!-.l(Ml scries) MJO, Ml'llA thru M20G M22 n-H(All Scries) ZMN 52f»l.

APPLICAHLE SYSH.M:

tGT KIT

ATI ( ) rrnyniT KIT AT.? ( ) "i M'-t ( ) Note: Kits eligibile only on basic engines covered by T.C. numbers shown above, GC'.JTHV.-;;JT REGION FUG:-:F t'i* BOARDS DIVISION . ri;:'.!-cT TO INSPECTION