STC SE3330NM

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate This certificate may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21. 47.

FAA Form 8110-2 (5/14) Page 1 of 7

Number: SE3330NM

This certificate issued to: Real Gaskets Tennessee 2506 Stateline Road Elizabethton, TN 37643

Part * of the Civil Air Regulations.

Original Product – Type Certificate Number: * (see pages 3 through 7) Make: Continental Model: (see pages 3 through 7)

Continental valve cover gasket, part number (P/N) 530162, 532451, 534857, 632310, and 632459 for the engine models listed on page 3 through 7 of this Supplemental Type Certificate (STC) is replaced by the gasket P/N RG-530162, RG-532451, RG-534857, RG-632310, and RG-632459 manufactured in accordance with drawing Nos. 04, 05, 06, 07, and 08, dated January 31, 1986, or later FAA approved revisions. Installation is accomplished in accordance with Real Gaskets Tennessee document No. RG- 530162, RG-532451, RG-5324857, RG-632310 or RG-632459, or Revision: III, dated 5/30/2014, or later FAA approved revisions.

Approval of this change in type design applies to the engine models listed on Pages 3 through 7 of this STC only. The installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the engine.

(Limitations and Conditions continued on pages 3 through 7)

Date of Application: December 30, 1985 Date Reissued: 7/13/2001; 11/15/2011; 11/20/2014; 02/27/2015 Date of Issuance: April 21, 1986 Date Amended: 7/13/2001

Signature

Title Melvin D. Taylor, Manager, Atlanta Aircraft Certification Office

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate This certificate may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21. 47.

FAA Form 8110-2 (5/14) Page 2 of 7

To (Name and address of transferee)

From (Name and address of grantor)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SE3330NM

This certificate may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21. 47.

FAA Form 8110-2 (5/14) Page 3 of 7

Instructions for Continued Airworthiness (ICA), Real Gaskets Tennessee Document No. RG-530162, RG-532451, RG-534857, RG- 632310 or RG-632459 Rev. III, dated 5/30/2014, or later FAA accepted revisions, as applicable, must be made available to the operator at the time of installation.

APPLICABILITY OF THE TYPE DESIGN CHANGE FOR P/N 530162 ENGINE MODEL TYPE CERT.

NUMBER REGULATION

CERTIFICATION BASIS

EFFECTIVE DATE AMENDMENTS

C75,C85 E-233 CAR 13

C90, 0-200 E-252 CAR 13 8-1-41

A-65 E-205 CAR 13

A-75 E-213 CAR 13 8-1-41

C-125-2 E-236 CAR 13 8-1-41

C-145-2 E-253 CAR 13 8-1-41 -2H

O-300-A E-253 CAR 13 -B -C -D

GO-300-A E-298 CAR 13 6-15-56 13-1 -B -C -D

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SE3330NM

This certificate may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21. 47.

FAA Form 8110-2 (5/14) Page 4 of 7

APPLICABILITY OF THE TYPE DESIGN CHANGE FOR P/N 532451 ENGINE MODEL TYPE CERT.

NUMBER REGULATION

CERTIFICATION BASIS

EFFECTIVE DATE AMENDMENTS

O-470-A E-273 CAR 13 12-4-52 -E -J

IO-470-J 3E1 CAR 13 6-15-56 13-1 -K

E-165-2 E-246 CAR 13 8-01-41

E-185-1 E-246 CAR 13 8-01-41 -3 -8 -9 -11

E-225-4 E-267 CAR 13 8-01-49 -8

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SE3330NM

This certificate may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21. 47.

FAA Form 8110-2 (5/14) Page 5 of 7

APPLICABILITY OF THE TYPE DESIGN CHANGE FOR P/N 534857 ENGINE MODEL TYPE CERT.

NUMBER REGULATION

CERTIFICATION BASIS

EFFECTIVE DATE AMENDMENTS

O-470-B E-273 CAR 13 12-4-52

IO-470-D 3E1 CAR 13 6-15-56 13-1

IO-520- A E5CE CAR 13 6-15-56 13-1 THROUGH 13-5

BA, C, D, E, F

TSIO-520- B E8CE CAR 13 6-15-56 13-1 THROUGH 13-5

T, U, VB, WB

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SE3330NM

This certificate may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21. 47.

FAA Form 8110-2 (5/14) Page 6 of 7

APPLICABILITY OF THE TYPE DESIGN CHANGE FOR P/N 632310 ENGINE MODEL TYPE CERT.

NUMBER REGULATION

CERTIFICATION BASIS

EFFECTIVE DATE AMENDMENTS

IO-360-A E1CE CAR 13 6-15-56 13-1 THROUGH 13-3

TSIO-360-A E9CE 14 CFR 33 02-01-65 33-1

LTSIO-360-E E9CE 14 CFR 33 02-01-65 33-1

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SE3330NM

This certificate may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21. 47.

FAA Form 8110-2 (5/14) Page 7 of 7

APPLICABILITY OF THE TYPE DESIGN CHANGE FOR P/N 632459 ENGINE MODEL TYPE CERT.

NUMBER REGULATION

CERTIFICATION BASIS

EFFECTIVE DATE AMENDMENTS

GTSIO-520-C E7CE CAR 13 6-15-56 13-1 THROUGH 13-4