# STC SA1151SW

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: George D. Merrell
- Description: Installation of Lycoming IO-360-C1C engine (200 hp) with Hartzell HC-C2YK-2/ C7666A-4 propeller.
- Status date: November 22, 1998
- Data sheets: A1EA, A1EA
- Certificate PDF: https://openairdocs.org/files/sha256/96/d2/96d2851a1e36c429f2c35e74cd7c2ef725935286d73f292f6106000e24baa8c8
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/724164AD9F91425386257D41005A2135.0001
- Page: https://openairdocs.org/stc/SA1151SW

## ADs that name it

None.

## Approved models (2)

- Piper Aircraft Inc. PA-30 (TCDS A1EA)
- Piper Aircraft Inc. PA-39 (TCDS A1EA)

## 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.

^tetea ®f of tEranspm-iation - Jlfrtteral ^titatinn ^Ahmhttslrjitinn upplettmttal (Certificate SA11S1SW George D. Merrell, an Individual DBA George Merrell Co.

Hwy 1431 West at Pacific Loop Kingsland, TX 78639 w& 3 Civil Air A1EA Piper PA-30, PA-39 Installation of Lycoraing IO-360-C1C engine (200 HP) with Hartzell Propeller Model HC-C2VK-2/C7666A-4 according to Drawing List 24,000 dated May 11, 1970, revised December 22, 1970, for Models PA-30 and PA-39; or installation of Lycoming IO-360-C1C, or -GIF engine, (200 HP) with Hartzell Propeller Model HOC2YK-2/C7666A-4 in accordance with Drawing List 24,000 revised May 6, 1977, and Drawing 2400, Sheet 3 revised 7/29/77, to Revision B; or later FAA approved revision.

(See continuation sheet 3 of 3) dtr-fa til .'March 03, 1970 June Q'l, 1970 November 22, 1998 7/24/70; 2/11/71;

10/2/73; 8/15/77; 3/14/63 Rev. 5 S. Frances Cox Manager, Special Certification Office, Southwest Region (Title) Any Alteration of this ctrtlflcatf ij punishable by d flnf of not •Jfcseding Sl.QOQ, Gr iopflsonifent not exceeding 3 years, or both.

I NS I Rl (.1 I M>!\\S I h«- li Jiisfer cndorsrmnu Ivlnw may hr used lo riolih (fn Hi |>[>i upr ialc FA A }' cgional Oflifr of ihr rrarnlf r »! [his .SLipjjIcnirnl-il Typr Crriiht ;>if I h<- [• A A "ill rihisMi< [hr i;rn the ;nc in thf namr ol ihr irdiisferee antl lor ward u iu him.

TRANSFER ENDORSEMENT Transfer the ow-nership of Supplemental Type Certificate Number ._.._ to (JVatnf of transferee) (Address of transferee) _.. .

' and street) (Cay, Stall, and £1? cad,) from (Name ufgmntnr) (Print or type) „ (Address oj grantor) (Nimbi* and i idly. Stilt, and ZIP autt] Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

^tates < ^Department of Iftranspcrtnttcit - ^cheral J\iitatton J\bmmtslratt0tt (Certificate (dlotttmuatton Date of Issuance: June 07, 1970 Date of Reissuance: November 22, 1998 (Continued):

1. The following FAA Approved Airplane Flight Manual Supplements are required:

a. Supplement dated June 7, 1970, revised October 2, 1973, for Piper Model PA-30 with IO-360-C1C engine; OR

b. Supplement dated June 7, 1970, revised October 2, 1973, revised June 3, 1977, for Piper Model PA-30 with IO-360-C1C, or -GIF engine;

OR

c. Supplement dated February 11, 1971, for Piper Models PA-30 and PA-39 with IO-360-C1C engine.

2. This STC SAIISISW may not be used without the installation of STC SA1112SW dorsal fin, and STC SA1154SW rudder aileron interconnect system.

3. Loading instructions for individual aircraft is required.

4. Compatibility of this modification with other previously approved modifications must be determined by the installer.

-END- A/iy alteration of this certificate Is punishably by a fine of not exceeding $1,000, pr imprfsonasnt not ext7ee4ing 3 years, or both.

FAA Form 6110-2-1(10-69) Page 3 of 3 This certificate (iMy be transferred In tfctordance with FM 21.47.

## Every issue (1)

- November 22, 1998: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/96/d2/96d2851a1e36c429f2c35e74cd7c2ef725935286d73f292f6106000e24baa8c8)

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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.