# STC SA2386SW

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Avicon Development Corporation, United States
- Description: Installation of S.A.F.E., EGT, CHT Systems.
- Applied: February 14, 1976
- Status date: August 3, 1978
- Product: Aircraft, Large Airplane
- Certification basis: Part 21
- Data sheets: [TCDS A11WE](https://openairdocs.org/tcds/A11WE), [TCDS A17WE](https://openairdocs.org/tcds/A17WE), [TCDS 1A3](https://openairdocs.org/tcds/1A3), [TCDS A18CE](https://openairdocs.org/tcds/A18CE), [TCDS A17EU](https://openairdocs.org/tcds/A17EU), [TCDS A29EU](https://openairdocs.org/tcds/A29EU), [TCDS A1CE](https://openairdocs.org/tcds/A1CE), [TCDS 3A15](https://openairdocs.org/tcds/3A15), [TCDS A-777](https://openairdocs.org/tcds/A-777), [TCDS 5A3](https://openairdocs.org/tcds/5A3), [TCDS 5A4](https://openairdocs.org/tcds/5A4), [TCDS A12CE](https://openairdocs.org/tcds/A12CE), [TCDS 3A16](https://openairdocs.org/tcds/3A16), [TCDS H3SW](https://openairdocs.org/tcds/H3SW), [TCDS 3A19](https://openairdocs.org/tcds/3A19), [TCDS A-799](https://openairdocs.org/tcds/A-799), [TCDS 3A12](https://openairdocs.org/tcds/3A12), [TCDS 3A17](https://openairdocs.org/tcds/3A17), [TCDS A13CE](https://openairdocs.org/tcds/A13CE), [TCDS A20CE](https://openairdocs.org/tcds/A20CE) and 40 more
- Certificate PDF: https://openairdocs.org/files/sha256/f4/7e/f47e8f3c2f23c1019cf3acaf9c8ca839494cc3c94461117ae195f75b27876bc4
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/0E8ACB2995E8291386257D93005DBFAE.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2386SW

## ADs that name it (0)

None.

## Approved models (393, first 50)

- Aerostar Aircraft Corporation 360 ([TCDS A11WE](https://openairdocs.org/tcds/A11WE))
- Aerostar Aircraft Corporation 400 ([TCDS A11WE](https://openairdocs.org/tcds/A11WE))
- Aerostar Aircraft Corporation PA-60-600 (Aerostar 600) ([TCDS A17WE](https://openairdocs.org/tcds/A17WE))
- Aerostar Aircraft Corporation PA-60-601 (Aerostar 601) ([TCDS A17WE](https://openairdocs.org/tcds/A17WE))
- Alexandria Aircraft LLC 14-19 ([TCDS 1A3](https://openairdocs.org/tcds/1A3))
- Alexandria Aircraft LLC 14-19-2 ([TCDS 1A3](https://openairdocs.org/tcds/1A3))
- Alexandria Aircraft LLC 14-19-3 ([TCDS 1A3](https://openairdocs.org/tcds/1A3))
- Alexandria Aircraft LLC 14-19-3A ([TCDS 1A3](https://openairdocs.org/tcds/1A3))
- Alexandria Aircraft LLC 17-30 ([TCDS 1A3](https://openairdocs.org/tcds/1A3))
- Alexandria Aircraft LLC 17-30A ([TCDS A18CE](https://openairdocs.org/tcds/A18CE))
- Alexandria Aircraft LLC 17-31 ([TCDS 1A3](https://openairdocs.org/tcds/1A3))
- Alexandria Aircraft LLC 17-31A ([TCDS A18CE](https://openairdocs.org/tcds/A18CE))
- Alexandria Aircraft LLC 17-31ATC ([TCDS A18CE](https://openairdocs.org/tcds/A18CE))
- Alexandria Aircraft LLC 17-31TC ([TCDS 1A3](https://openairdocs.org/tcds/1A3))
- B-N Group Ltd. BN-2 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-2 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-20 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-21 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN2A MK. III ([TCDS A29EU](https://openairdocs.org/tcds/A29EU))
- Beechcraft Corporation 19A ([TCDS A1CE](https://openairdocs.org/tcds/A1CE))
- Beechcraft Corporation 23 ([TCDS A1CE](https://openairdocs.org/tcds/A1CE))
- Beechcraft Corporation 35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Beechcraft Corporation 35-33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation 35-A33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation 35-B33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation 35-C33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation 35-C33A ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation 35R ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Beechcraft Corporation 36 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation 45 (Military YT-34) ([TCDS 5A3](https://openairdocs.org/tcds/5A3))
- Beechcraft Corporation 50 ([TCDS 5A4](https://openairdocs.org/tcds/5A4))
- Beechcraft Corporation 60 ([TCDS A12CE](https://openairdocs.org/tcds/A12CE))
- Beechcraft Corporation 95-55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation 95-A55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation 95-B55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation 95-B55A ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation 95-B55B ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation 95-C55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation 95-C55A ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation A23 ([TCDS A1CE](https://openairdocs.org/tcds/A1CE))
- Beechcraft Corporation A23-19 ([TCDS A1CE](https://openairdocs.org/tcds/A1CE))
- Beechcraft Corporation A23A ([TCDS A1CE](https://openairdocs.org/tcds/A1CE))
- Beechcraft Corporation A35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Beechcraft Corporation A36 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation A45 (Military T-34A; B-45) ([TCDS 5A3](https://openairdocs.org/tcds/5A3))
- Beechcraft Corporation A60 ([TCDS A12CE](https://openairdocs.org/tcds/A12CE))
- Beechcraft Corporation B19 ([TCDS A1CE](https://openairdocs.org/tcds/A1CE))
- Beechcraft Corporation B35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Beechcraft Corporation B50 ([TCDS 5A4](https://openairdocs.org/tcds/5A4))

All 393: https://openairdocs.org/stc/SA2386SW/models.md

## 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.

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

•-fl6att£a£ifnd/.

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

!0-2(10-6S|

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

## Every issue (1)

- August 3, 1978: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/f4/7e/f47e8f3c2f23c1019cf3acaf9c8ca839494cc3c94461117ae195f75b27876bc4)

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