STC SE2340SW

FAA Form 8110-2 (5/14) Page 1 of 4

Number: SE2340SW

Part 13 of the Civil Air Regulations

Original Product – Type Certificate Number: * Make: * Model: * *See Limitations and Conditions

Installation of modified cylinder assemblies, barrels, pistons, and repaired crankcases in accordance with the drawings listed on the Continuation Sheet, or later FAA approved revisions Major repair/alteration of crankcases to be performed in accordance with Engine Components, Inc. Engineering Specification, Repair of Aircraft Reciprocating Engine Crankcases, ECI-EF4 Rev. 4, dated October 12, 1995, or later FAA approved revision. This specification is general except where specifically applied to a repair/alteration; the specification applies to all opposed aircraft reciprocating engine crankcases.

Date of Application: April 21, 1976 Date Reissued: 07/03/91; 03/21/08; 07/20/15; 01/25/16; 10/31/16 Date of Issuance: August 02, 1976 Date Amended: 09/01/76; 02/26/82; 07/08/82; 12/09/82; 07/09/85;

07/03/91/ 11/15/95 Revision 7

Signature

Title James A. Grigg Acting Manager, Fort Worth Aircraft Certification Office, Southwest Region Continental Motors Inc.

2039 S. Broad St.

Mobile, AL 36615

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

Transfer the ownership of Supplemental Type Certificate Number: SE2340SW

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: SE2340SW

FAA Form 8110-2 (5/14) Page 3 of 4

Date of Issuance: August 02, 1976 Date Amended: November 15, 1995 Date of Reissuance: October 31, 2016

The installer must determine whether this design change is compatible with previously approved modifications. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

*Cert Drawing No.

*Make *Model *TCDS Basis Eligibility Part Name Continental Motors Inc. IO-520-A, -B, -BA, E5CE CAR 13 AEC631475, Piston -BB, -C, -CB, -D, dated 01/27/76 -E, -F, -J, -K, -L, -M, -MB, -N, -NB

Continental Motors Inc. GTSIO-520-C, -D, E7CE CAR 13 AEC632585, Piston -H, -F, -K, -L, dated 01/28/76 -M, -N

Continental Motors Inc. TSIO-520-A, -B E8CE CAR 13 AEC632585, Piston -BA, -BB, -C, -CB, dated 01/28/76 -D, -E, -F, -J, -N, -NB, -BE

Continental Motors Inc. IO-520-A, -B, -BA, E5CE CAR 13 AEC34501, Barrel -BB, -C, -CB, -D, dated 10/13/75 -E, -F, -J, -K, -L, -M, -MB, -N, -NB AEC639272, Cylinder dated 10/16/75 Assy Mach.

Continental Motors Inc. GTSIO-520-C, -D, E7CE CAR 13 AEC634501, Barrel -H, -F, -K, -L, dated 10/13/75 -M, -N AEC639272, Cylinder dated 10/16/75 Assy Mach.

Continental Motors Inc. TSIO-520-A, -B, E8CE CAR 13 AEC634501, Barrel -BA, -BB, -C, -CB, dated 10/13/75 -D, -E, -F, -J, -N, -NB, -BE AEC639272, Cylinder dated 10/16/75 Assy Mach.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SE2340SW

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

Date of Issuance: August 02, 1976 Date Amended: November 15, 1995 Date of Reissuance: October 31, 2016

Continental Motors Inc. IO-346-A, -B E3CE CAR 13 AEC634501, Barrel dated 10/13/75

AEC639272, Cylinder dated 10/16/75 Assy Mach.

AEC631475 and AEC632585 pistons must be installed in complete sets due to weight differences, and must be installed such that they weigh within ½ ounce (14.17 grams) in opposite bays.

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