# STC SA09618SC

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: CenTex Aerospace Inc.
- Description: Installation of Teledyne Continental Motors TSIO-520-WB engine and increase maximum takeoff and landing weights to 6200 pounds.
- Status date: October 20, 2000
- Data sheets: A23CE, A23CE
- Certificate PDF: https://openairdocs.org/files/sha256/9e/e4/9ee4b9e8e4dbef66f6ebc5d80a7a6d4fbce18f94c5dd9ed21c086d4876811897
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/ACACA0FC8135089785256CC1007F3B56.0001
- Page: https://openairdocs.org/stc/SA09618SC

## ADs that name it

None.

## Approved models (2)

- Beechcraft Corporation 58P (TCDS A23CE)
- Beechcraft Corporation 58TC (TCDS A23CE)

## 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.

;lttt!iref> ( OSf of <£rim6jj0riaitrm - Jfcberal .A&tatinn upplmtetttal CcnTex Aerospace, Inc.

7805 Airport Drive P. O. Box 5803 Waco, TX 76708 ate*/-* (EertifttateProject No. ST61B4SC-A (RDK) SA09618SC Jft Mf 23 at*/ Federal Aviation A23CE Beech 58P; 58TC f~- Installation of Teledync Continental Motors TSIO-520-WB engine and increase maximum takeoff and landing weighls to 6200 pounds in accordance with CenTcx Aerospace. Inc. Drawing Number CTA58-1001. dated January 12. 2000, or later FAA approved revision. FAA approved Airplane Flight Manual Supplement Number AFMS 1000, dated September 7. 2000, or later FAA approved revision is required.

Compatibility of this design change with previously approved modifications must be determined by the installer. If the holder agrees to permit another person to use this certificalc lo alter the producl. the holder sliall give the other person written evidence of that permission.

frwft*n*rS'r<w.S'r<w. trtrSr /j ft 1 ffyf' Me . January 12, 2000 October 20, 2000 (Signature) S. Frances Cox Manager, Special Certification Office Southwest Region (Title) Any of this certificate Is Cy a fine ff not ln^ $1,QQQ, or imprisonment not exceeding 3 years, of FAA Forir 8110-2 {10-&8) Page 1 of certificate puy i* tian$feri<*t! Jn Accordance with FAR 21.47.

IIVS I Rl. (., I IO[\S. I lit iranslcr rndorsrmciil below may br used lo nuriK ilir appropriate FA A K rgional Office ( Mr- [iMnsIrr u! [his Siifjplrnif nfal Typr Crrlifu dl<L 1'ht' I A A vull roissur tin* rrnihraic m llif nacnr o! ihs iransfcrte and lor\%ard n (o hitn.

TRANSFER ENDORSEMENT Transfer the ouncrship of Supplemental Type Certificate Number ___„ to (Name o) transferee) (Address of transferee)._.

Vumbt' andsmtl) t, Slate, and £1P todl) from (Name of grantor) (Print or typr) (Address oj granlvr) (tfvmbtt and stretl) (City, SlaU, nil! £!P codr) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

## Every issue (1)

- October 20, 2000: Issued, Current. [certificate](https://openairdocs.org/files/sha256/9e/e4/9ee4b9e8e4dbef66f6ebc5d80a7a6d4fbce18f94c5dd9ed21c086d4876811897)

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.