# STC SE8776SW - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Continental Motors, Inc., United States - Description: Installation of coated cylinders and piston rings. - Applied: November 12, 1993 - Status date: October 31, 2016 - Product: Aircraft, Single-Engine - Certification basis: Part 21, Part 33 - Data sheets: [TCDS A-764](https://openairdocs.org/tcds/A-764), [TCDS ATC 31](https://openairdocs.org/tcds/ATC%2031), [TCDS E-216](https://openairdocs.org/tcds/E-216), [TCDS ATC 75](https://openairdocs.org/tcds/ATC%2075), [TCDS E-121](https://openairdocs.org/tcds/E-121), [TCDS E-195](https://openairdocs.org/tcds/E-195), [TCDS E-237](https://openairdocs.org/tcds/E-237), [TCDS E1SW](https://openairdocs.org/tcds/E1SW), [TCDS 5E-1](https://openairdocs.org/tcds/5E-1), [TCDS 5E-2](https://openairdocs.org/tcds/5E-2), [TCDS 5E-4](https://openairdocs.org/tcds/5E-4), [TCDS 5E-5](https://openairdocs.org/tcds/5E-5), [TCDS 5E-8](https://openairdocs.org/tcds/5E-8), [TCDS E-294](https://openairdocs.org/tcds/E-294), [TCDS E-310](https://openairdocs.org/tcds/E-310), [TCDS E11EU](https://openairdocs.org/tcds/E11EU), [TCDS E3IN](https://openairdocs.org/tcds/E3IN), [TCDS E4IN](https://openairdocs.org/tcds/E4IN), [TCDS 3E1](https://openairdocs.org/tcds/3E1), [TCDS 3E3](https://openairdocs.org/tcds/3E3) and 53 more - Certificate PDF: https://openairdocs.org/files/sha256/e3/29/e3292210e3926f9d75ae5092c2aa88deb084ee9fa91fd047645985998629351a - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/B901C6C779B104E7862580CE0074DB4B.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SE8776SW ## ADs that name it (0) None. ## Approved models (231, first 50) - Consolidated Vultee Aircraft Corporation Stinson Division L-5 ([TCDS A-764](https://openairdocs.org/tcds/A-764)) - Curtiss-Wright Corporation LA-1 ([TCDS ATC 31](https://openairdocs.org/tcds/ATC%2031)) - Fairchild Engine Division Fairchild Engine and Airplane Corp. 6-440 Series ([TCDS E-216](https://openairdocs.org/tcds/E-216)) - Jacobs Aircraft Engine Co. L-3 ([TCDS ATC 75](https://openairdocs.org/tcds/ATC%2075)) - Jacobs Aircraft Engine Co. L-4 Series ([TCDS E-121](https://openairdocs.org/tcds/E-121)) - Jacobs Aircraft Engine Co. L-6 Series ([TCDS E-195](https://openairdocs.org/tcds/E-195)) - Jacobs Service Company R-755A Series ([TCDS E-237](https://openairdocs.org/tcds/E-237)) - Jacobs Service Company R-755S ([TCDS E1SW](https://openairdocs.org/tcds/E1SW)) - Jacobs Service Company R-755SM ([TCDS E1SW](https://openairdocs.org/tcds/E1SW)) - Pratt & Whitney Division R-1340 Series ([TCDS 5E-2](https://openairdocs.org/tcds/5E-2)) - Pratt & Whitney Division R-1830 Series ([TCDS 5E-4](https://openairdocs.org/tcds/5E-4)) - Pratt & Whitney Division R-2000 Series ([TCDS 5E-5](https://openairdocs.org/tcds/5E-5)) - Pratt & Whitney Division R-2800 Series ([TCDS 5E-8](https://openairdocs.org/tcds/5E-8)) - Pratt & Whitney Division R-985 Series ([TCDS 5E-1](https://openairdocs.org/tcds/5E-1)) - Rolls-Royce Corporation Gipsy Queen 30 Mk.2 ([TCDS E-294](https://openairdocs.org/tcds/E-294)) - Rolls-Royce Corporation Gipsy Queen 70 MK2 ([TCDS E-310](https://openairdocs.org/tcds/E-310)) - Rolls-Royce Corporation Gipsy Queen 70 MK3 ([TCDS E-310](https://openairdocs.org/tcds/E-310)) - Rolls-Royce Corporation RR C90-12F ([TCDS E3IN](https://openairdocs.org/tcds/E3IN)) - Rolls-Royce Corporation RR C90-12FH ([TCDS E3IN](https://openairdocs.org/tcds/E3IN)) - Rolls-Royce Corporation RR C90-12FJ ([TCDS E3IN](https://openairdocs.org/tcds/E3IN)) - Rolls-Royce Corporation RR C90-12FP ([TCDS E3IN](https://openairdocs.org/tcds/E3IN)) - Rolls-Royce Corporation RR C90-14F ([TCDS E3IN](https://openairdocs.org/tcds/E3IN)) - Rolls-Royce Corporation RR C90-14FH ([TCDS E3IN](https://openairdocs.org/tcds/E3IN)) - Rolls-Royce Corporation RR C90-14FJ ([TCDS E3IN](https://openairdocs.org/tcds/E3IN)) - Rolls-Royce Corporation RR C90-16F ([TCDS E3IN](https://openairdocs.org/tcds/E3IN)) - Rolls-Royce Corporation RR C90-8F ([TCDS E3IN](https://openairdocs.org/tcds/E3IN)) - Rolls-Royce Corporation RR C90-8FJ ([TCDS E3IN](https://openairdocs.org/tcds/E3IN)) - Rolls-Royce Corporation RR O-200-A ([TCDS E3IN](https://openairdocs.org/tcds/E3IN)) - Rolls-Royce Corporation RR O-200-B ([TCDS E3IN](https://openairdocs.org/tcds/E3IN)) - Rolls-Royce Corporation RR O-200-C ([TCDS E3IN](https://openairdocs.org/tcds/E3IN)) - Rolls-Royce Corporation RR O-240-A ([TCDS E11EU](https://openairdocs.org/tcds/E11EU)) - Rolls-Royce Corporation RR O-300-A ([TCDS E4IN](https://openairdocs.org/tcds/E4IN)) - Rolls-Royce Corporation RR O-300-B ([TCDS E4IN](https://openairdocs.org/tcds/E4IN)) - Rolls-Royce Corporation RR O-300-C ([TCDS E4IN](https://openairdocs.org/tcds/E4IN)) - Rolls-Royce Corporation RR O-300-D ([TCDS E4IN](https://openairdocs.org/tcds/E4IN)) - Teledyne Continental Motors A-65 Series ([TCDS E-205](https://openairdocs.org/tcds/E-205)) - Teledyne Continental Motors C-125-1 ([TCDS E-236](https://openairdocs.org/tcds/E-236)) - Teledyne Continental Motors C-125-2 ([TCDS E-236](https://openairdocs.org/tcds/E-236)) - Teledyne Continental Motors C145 ([TCDS E-253](https://openairdocs.org/tcds/E-253)) - Teledyne Continental Motors C145-2 ([TCDS E-253](https://openairdocs.org/tcds/E-253)) - Teledyne Continental Motors C145-2HP ([TCDS E-253](https://openairdocs.org/tcds/E-253)) - Teledyne Continental Motors C75 Series ([TCDS E-233](https://openairdocs.org/tcds/E-233)) - Teledyne Continental Motors C90 Series ([TCDS E-252](https://openairdocs.org/tcds/E-252)) - Teledyne Continental Motors E165-2 ([TCDS E-246](https://openairdocs.org/tcds/E-246)) - Teledyne Continental Motors E165-3 ([TCDS E-246](https://openairdocs.org/tcds/E-246)) - Teledyne Continental Motors E165-4 ([TCDS E-246](https://openairdocs.org/tcds/E-246)) - Teledyne Continental Motors E185-1 ([TCDS E-246](https://openairdocs.org/tcds/E-246)) - Teledyne Continental Motors E185-10 ([TCDS E-246](https://openairdocs.org/tcds/E-246)) - Teledyne Continental Motors E185-11 ([TCDS E-246](https://openairdocs.org/tcds/E-246)) - Teledyne Continental Motors E185-2 ([TCDS E-246](https://openairdocs.org/tcds/E-246)) All 231: https://openairdocs.org/stc/SE8776SW/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. FAA Form 8110-2 (5/14) Page 1 of 14 Number: SE8776SW Part * of the * Regulations 1. Approval of piston rings AEC648005, revision IR, dated 2/17/94, and AEL252577M-1, revision IR, dated 4/12/94, or later FAA approved revision. 2. Approval of cylinder bore coating in accordance with Engineering Specifications 93-10-1, revision 2, dated 2/4/94, and EC66029, revision A, dated 1/31/94, or later FAA approved revisions. 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. Installation of coated cylinders and piston rings are limited to engines specified on continuation sheets (See continuation sheet 3 of 14) Date of Application: November 12, 1993 Date Reissued: 08/27/07; 07/20/15; 01/25/16; 10/31/16 Date of Issuance: April 26, 1994 Date Amended: February 06, 1996 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 14 Transfer the ownership of Supplemental Type Certificate Number: SE8776SW 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: SE8776SW FAA Form 8110-2 (5/14) Page 3 of 14 Date of Issuance: April 26, 1994 Date Amended: February 06, 1996 Date of Reissuance: October 31, 2016 Part Name and Make and Part No. Model *TCDS *Reg./Part Ring, Compression Continental Motors Inc. E5CE CAR 13 AEC648005 I.R. IO-520-A, B, BA, BB, C, CB, D, or later FAA Approved E, F, J, K, L, M, MB, N, NB Revision **TSIO-520A, AE, AF, B, BB, BE, E8CE CAR 13** C, CE, D, DB, E, EB, G, H, J, JB, K, KB, L, LB, M, N, NB, P, R, T, U, UB, VB, WB LTSIO-520-AE GTSIO-520-C, D, F, H, K, L, M, N E7CE CAR 13 IO-550-A, B, C, D, E, F, G, L E3SO PART 33 TSIO-550-A, B E5SO PART 33 TSIO-550L-A, B E4SO PART 33 Ring, Compression Lycoming Engines E274 CAR 13 AEL252577M-1 I.R. or O-320-A1A, A1B, A2A, A2B, A2C, later FAA Approved A2D, A3A, A3B, A3C, B1A, B1B, Revision B2A, B2B, B2C, B3A, B3B, B3C, C1A, C1B, C2A, C2B, C2C, C3A, C3B, C3C, D1A, D1B, D1C, D1D, D1F, D2A, D2B, D2C, D2F, D2G, D2H, D2J, D3G, E1A, E1B, E1C, D1F, E2A, E2B, E2C, E2D, E2E, E2F, E2G, E2H, E3D, E3H, H1AD, H1BD, H2AD, H2BD, H3AD, H3BD IO-320-A1A, A2A, B1A, B1B, B1C, 1E12-7 CAR 13 B1D, B1E, B2A, C1A, C1B, D1A, D1AD, D1B, D1C, E1A, E1B, E2A, E2B, F1A LIO-320-B1A, C1A AIO-320-A1A, A1B, A2A, A2B, B1B, C1B O-340-A1A, A2A, B1A E277-5 CAR 13 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SE8776SW FAA Form 8110-2 (5/14) Page 4 of 14 Date of Issuance: April 26, 1994 Date Amended: February 06, 1996 Date of Reissuance: October 31, 2016 Part Name and Make and Part No. Model *TCDS *Reg./Part Ring, Compression O-360-A1A, A1AD, A1C, A1D, A1F, E286 CAR 13 AEL252577M-1 I.R. or A1F6, A1F6D, A1G, A1G6, A1G6D, later FAA Approved A1H, A1H6, A1J, A1LD, A2A, A2D, Revision A2E, A2F, A2G, A2H, A3A, A3AD, A3D, A4A, A4AD, A4D, A4G, A4J, A4JD, A4K, A4M, A4N, A5AD, B1A, B1B, B2A, B2B, C1A, C1C, C1E, C1F, C1G, C2A, C2B, C2C, C2D, C2E, D1A, D2A, D2B, E1A6AD, F1A6, G1A6 LO-360-A1G6D, A1H6, E1A6D HO-360-A1A, B1A, B1B TO-360-A1A6D, C1A6D, E1A6D, E26EA PART 33 F1A6D Ring, Compression Lycoming Engines E26EA PART 33 AEL252577M-1 I.R. or LTO-360-A1A6D, E1A6D later FAA Approved IO-360-A1A, A1B, A1B6, A1B6D, 1E10 CAR 13 Revision A1C, A1C6, A1D, A1D6, A1D6D, A2A, A2B, A2C, A3B6D, A3D6D, B1A, B1B, B1BD, B1C, B1D, B1E, B1F, B1F6, B2E, B2F, B2F6, B4A, C1A, C1B, C1C, C1CD, C1D6, C1E6, C1E6D, C1F, D1A, E1A, F1A, J1A6D, J1AD, K2D AEIO-360-A1A, A1B, A1B6, A1C, A1D, A1E, A2A, A2B, A2C, A2E, B1B, B1D, B1F, B1F6, G1G6, B2F, B4A, H1A AIO-360-A1A, A1B, A2A, A2B, B1B HIO-360-A1A, B1A, B1B, C1A, C1B, D1A, E1AD, E1BD, F1AD LHIO-360-C1A, C1B, F1AD (T)IO-360-A3B6D, C1F, F1A LIO-360-C1E, C1E6, C1E6D TIO-360-A1A, A1B, A3B6, C1A6D E16EA PART 33 VO-360-A1A, A1B, B1A 1E1 CAR 13 IVO-360-A1A United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SE8776SW FAA Form 8110-2 (5/14) Page 5 of 14 Date of Issuance: April 26, 1994 Date Amended: February 06, 1996 Date of Reissuance: October 31, 2016 Part Name and Make and Part No. Model *TCDS *Reg./Part Ring, Compression GO-480-A1A, B, B1, B1A6, B1B, E275 CAR 13 AEL252577M-1 I.R. or B1C, B1D, C1B6, C1D6, C2D6, later FAA Approved C2E6, D1A, E1A6, F1A6, F2A6, Revision F2D6, F3A6, F3B6, F4A6, F4B6, F6, G1A6, G1B6, G1D6, G1E6, G1F6, G1G6, G1H6, G1J6, G2D6, G2F6 IGO-480-A1A6, A1B6 GSO-480-A 1A6, A1C6, A2A6, B1A6, E284 CAR 13 B1B3, B1B6, B1C6, B1E6, B1F6, B1G6, B1J6, B2C6, B2D6, B2G6, B2H6 IGSO-480-A1A6, A1B6, A1C6, A1D6, A1E6, A1F6, A1G6 O-480-3 O-540-A1A, A1A5, A1B5, A1C5, E295 CAR 13 A1D, A1D5, A2B, A3D5, A4A5, A4B5, A4C5, A4D5, B2B5, B2C5, B2C5D, B4A5, B4B5, B4B5D, D1A5, E1A, E4A5, E4B5, D1A5, E1A, E4A5, E4B5, E4C5, F1A5, F1B5, G1A5, G2A5, J1A5D, J1B5D, J1C5D, J1D5D, J2A5D, J2B5D, J2C5D, J2D5D, J3A5, J3A5D, J3C5D, L3C5D VO-540-A1A, A2A, B1A, B1B, B1B3, E304 CAR 13 B1C, B1D, B1E, B1F, B1G, B1H3, B2A, B2C, B2D, B2E, B2G, C1A, C1B, C1C3, C2A, C2B, C2C United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SE8776SW FAA Form 8110-2 (5/14) Page 6 of 14 Date of Issuance: April 26, 1994 Date Amended: February 06, 1996 Date of Reissuance: October 31, 2016 Part Name and Make and Part No. Model *TCDS *Reg./Part Ring, Compression Lycoming Engines 1E4 CAR 13 AEL252577M-1 I.R. or IO-540-A1A5, B1A5, B1B5, B1C5, later FAA Approved C1B5, C1C5, C2C, C4A5, C4B5, Revision C4B5D, C4C5, C4D5D, D4A5, D4B5, D4C5, E1A5, E1B5, E1C5, G1A5, G1B5, G1C5, G1D5, G1E5, G1F5, J4A5, K1A5, K1A5D, K1B5, K1B5D, K1C5, K1D5, K1E5, K1E5D, K1F5, K1F5D, K1G5, K1G5D, K1H5, K1J5, K1J5D, K1K5, L1A5, L1A5D, L1B5D, L1C5, M1A5, M1A5D, M1B5, M1B5D, M2A5D, N1A5, N1A5D, P1A5, R1A5, S1A5, T4A5, T4A5D, T4B5D, T4C5D, U1A5D, U1B5D, V4A5D, W1A5D, W3A5D AEIO-540-D4A5, D4B5, D4C5, K1A5D, K1B5, K1D5, K1F5D, K1G5, K1G5D, K1H5, K1J5, K1J5D, L1B5, L1B5D HIO-540-A1A (T)IO-540-E1B5 IVO-540-A1A E11EA CAR 13 TVO-540-A1A 1E14 CAR 13 TIO-540-A1A, A1B, A1C, A2A, A2B, E14EA CAR 13 A2C, AA1AD, AB1AD, AE2A, AF1A, C1A, C1AD, E1A, E1B5, F2B5, G1A, H1A, J2B, J2BD, K1AD, N2BD, R2AD, S1AD, T2AD, U2A, V2AD, W2A LTIO-540-F2BD, J2B, J2BD, K1AD, N2BD, R2AD, U2A, V2AD, W2A TVO-540-A1A 1E14 CAR 13 TIVO-540-A2A IGO-540-A1A, A1B, A1C, B1A, 1E11 CAR 13 B1B, B1C IGSO-540-A1A, A1C, A1D, A1E, 1E7 CAR 13 A1F, A1H, B1A, B1C TIO-541-A1A, E1A4, E1B4, E1C4, E10A6 CAR 13 E1D4 TIGO-541-D1A, D1B, E1A, G1AD E19EA FAR 33 IO-720-A1A, A1B, A1BD, B1A, 1E15 CAR 13 B1B, B1BD, C1B, C1BD, D1B, D1BD, D1C, D1CD United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SE8776SW FAA Form 8110-2 (5/14) Page 7 of 14 Date of Issuance: April 26, 1994 Date Amended: February 06, 1996 Date of Reissuance: October 31, 2016 The following is the engine eligibility for the major repairs accomplished according to EC Spec. 93-10-1 and EC66029: *Make *Model *TCDS *Reg./Part CONTINENTAL A- 65- 1, 3, 6, 6J, 7, 8, 8F, 8FJ, 8J, E-205 CAR 13 MOTORS INC. 9, 9F, 9FJ, 9J, 12, 12F, 12FJ, 12J, 14, 14F, 14FJ, 14J **A- 75- 3, 6, 6J, 8, 8F, 8FJ, 8J, 9, 9J E-213 CAR 13** C- 75- 8, 8F, 8FH, 8FHJ, 8FJ, 8J, 12 E-233 CAR 13 12B, 12BF, 12BFH, 12F, 12FH, 12FHJ, 15, 15F, FJ, J C- 85- 8, 8F, 8FHJ, 8FJ, 8J, 12, 12F, 12FH, 12FHJ, 12FJ, 12J, 14F, 15, 15F C- 90- 8F, 8FJ, 12F, 12FH, 12FJ, 12FP, E-252 CAR 13 14F, 14FH, 14FJ, 14FP, 16F O- 200- A, B, C **C- 125- 1, 2 E-236 CAR 13** **C- 145- 2, 2H, 2HP E-253 CAR 13 O- 300- A, B, C, D, E** **GO- 300- A, B, C, D, E, F E-298 CAR 13** **IO- 346- A, B E3CE CAR 13** **IO- 360- A, AB, B, C, CB, D, DB, E, F, E1CE CAR 13** G, GB, H, HB, J **TSIO- 360- B, C, CB, D, DB, E, EB, F, FB, E9CE PART 33** G, GB, H, HB, JB, KB, LB, MB **LTSIO- 360- E, EB, KB E9CE PART 33** **E- 165- 2, 3, 4 E-246 CAR 13 E- 185- 1, 2, 3, 9, 10, 11** United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SE8776SW FAA Form 8110-2 (5/14) Page 8 of 14 Date of Issuance: April 26, 1994 Date Amended: February 06, 1996 Date of Reissuance: October 31, 2016 The following is the engine eligibility for the major repairs accomplished according to EC Spec. 93-10-1 and EC66029: *Make *Model *TCDS *Reg./Part CONTINENTAL E- -225 2, 4, 8, 9 E-267 CAR 13 MOTORS INC. **O- 470- 2, 4, 7, 7A, 7B, 11, 11B, 11BC1, E-269 CAR 13 11C1, 13, 13A, 15** O- 470- A, B, B-C1, E, G, G-C1, H, J, K, E-273 CAR 13 K-C1, L, L-C1, M, M-C1, P, R, S, U IO- 470- A, C **IO- 470- D, E, F, G, H, I, J, L, LO, M, 3E1 CAR 13** N, P, R, S, T, U, V, VO **LIO- 470- A, B, C, D 3E1 CAR 13** **TSIO- 470- B, C, D 3E3 CAR 13** **IO- 520- A, B, BA, BB, C, CB, D, E, F, E5CE CAR 13** J, K, L, M, MB, N, NB **TSIO- 520- A, AE, AF, B, BB, BE, C, CE, D, E8CE CAR 13** DB, E, EB, G, H, J, JB, K, KB, L, LB, M, N, NB, P, R, T, U, **UB, VB, WB LTSIO- 520- AE** **GTSIO- 520- C, D, F, H, K. L, M, N E7CE CAR 13** **IO- 550- IO-550A, B, C, D, E, F, G, L E3SO PART 33** **TSIO- 550- A, B E5SO PART 33** **TSIO- 550L- A, B E4SO PART 33** **W 670- 6A, 6M, -16, -K, -M, -23, -24 E162 CAR 13** United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SE8776SW FAA Form 8110-2 (5/14) Page 9 of 14 Date of Issuance: April 26, 1994 Date Amended: February 06, 1996 Date of Reissuance: October 31, 2016 The following is the engine eligibility for the major repairs accomplished according to EC Spec. 93-10-1 and EC66029: *Make *Model *TCDS *Reg./Part LYCOMING O- 235- C1, C1B, C1C, C2A, C2B, C2C, E223-17 CAR 13 ENGINES E1, E1B, E2A, E2B, H2C, F1, F1B, F2A, F2B, G1, G1A, G1B, G2A, G2B,, J2A, J2B, K2A, K2B, K2C, L2A, L2C, M1, M2C, M3C, K2A, K2B, K2C, L2A, L2C, M1, M2C, M3C, N2A, N2C, P1, P2A, P2C, P3C **O- 290- 11, D, D2, D2A, D2B, D2C E229-13 CAR 13** O- 320- A1A, A1B, A2A, A2B, A2C, A2D, E274 CAR 13 A3A, A3B, A3C, B1A, B1B, B2A, B2B, B2C, B3A, B3B, B3C, C1A, C1B, C2A, C2B, C2C, C3A, C3B, C3C, D1A, D1B, D1C, D1D, D1F, D2A, D2B, D2C, D2F, D2G, D2H, D2J, D3G, E1A, E1B, E1C, D1F, E2A, E2B, E2C, E2D, E2E, E2F, E2G, E2H, E3D, E3H, H1AD, H1BD, H2AD, H2BD, H3AD, H3BD LIO- 320- B1A, C1A AIO- 320- A1A, A1B, A2A, A2B, B1B, C1B **AEIO- 320- E1A, E1B, E2A, E2B, D1B, D2B E274 CAR 13** **O- 340- A1A, A2A, B1A E277-5 CAR 13** O- 360- A1A, A1AD, A1C, A1D, A1F, A1D, E286 CAR 13 A1F, A1F6, A1F6D, A1G, A1G6, A1G6D, A1H, A1H6, A1J, A1LD, A2A, A2D, A2E, A2F, A2G, A2H, A3A, A3AD, A3D, A4A, A4AD, A4D, A4G, A4J, A4JD, A4K, A4M, A4N, A5AD, B1A, B1B, B2A, B2B, C1A, C1C, C1E, C1F, C1G, C2A, C2B, C2C, C2D, C2E, D1A, D2A, D2B, E1A6D, F1A6, G1A6 LO- 360- A1G6D, A1H6, E1A6D HO- 360- A1A, B1A, B1B United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SE8776SW FAA Form 8110-2 (5/14) Page 10 of 14 Date of Issuance: April 26, 1994 Date Amended: February 06, 1996 Date of Reissuance: October 31, 2016 The following is the engine eligibility for the major repairs accomplished according to EC Spec. 93-10-1 and EC66029: *Make *Model *TCDS *Reg./Part LYCOMING TO- 360- A1A6D, C1A6D, E1A6D, F1A6D E26EA PART 33 ENGINES LTO- 360- A1A6D, E1A6D IO- 360- A1A, A1B, A1B6, A1B6D, A1C, 1E10 CAR 13 A1C6, A1D, A1D6, A1D6D, A2A, A2B, A2C, A3B6D, A3D6D, B1A, B1B, B1BD, B1C, B1D, B1E, B1F, B1F6, B2E, B2F, B2F6, B4A, C1A, C1B, C1C, C1CD, C1D6, C1E6, C1E6D, C1F, D1A, E1A, F1A, J1A6D, J1AD, K2D AEIO- 360- A1A, A1B, A1B6, A1C, A1D, A1E, A2A, A2B, A2C, A2E, B1B, B1D, B1F, B1F6, G1G6, B2F, B4A, H1A AIO- 360- A1A, A1B, A2A, A2B, B1B HIO- 360- A1A, B1A, B1B, C1A, C1B, D1A, E1AD, E1BD, F1AD LHIO- 360- C1A, C1B, F1AD (T)IO- 360- A3B6D, C1F, F1A LIO- 360- C1E, C1E6, C1E6D **TIO- 360- A1A, A1B, A3B6, C1A6D E16EA PART 33** **VO- 360- A1A, A1B, B1A 1E1 CAR 13 IVO- 360- A1A** O- 435- A, A2, 17, 23, 23A, 23B, 23C, E228 CAR 13 25, 4, 6, 6A GO- 435- C1B1, C2, C2A, C2A2, C2B, C2B1, C2B2, C2B2-6, C2E, (C2)11 **GSO- 435- B, B2 E276 CAR 13** **VO- 435- A1A(21), A1B, A1C, A1D, A1E, E279 CAR 13 A1F, B1A** **TVO- 435- 17, A1A, B1A, B1B, C1A, D1A, 1E13 CAR 13 D1B, E1A, F1A, G1A, G1B** United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SE8776SW FAA Form 8110-2 (5/14) Page 11 of 14 Date of Issuance: April 26, 1994 Date Amended: February 06, 1996 Date of Reissuance: October 31, 2016 The following is the engine eligibility for the major repairs accomplished according to EC Spec. 93-10-1 and EC66029: *Make *Model *TCDS *Reg./Part LYCOMING GO- 480- A1A, B, B1, B1A6, B1B, B1C, B1D, E275 CAR 13 ENGINES C1B6, C1D6, C2D6, C2E6, D1A, E1A6, F1A6, F2A6, F2D6, F3A6, F3B6, F4A6, F4B6, F6, G1A6, G1B6, G1D6, G1E6, G1F6, G1G6, G1H6, G1J6, G2D6, G2F6 IGO- 480- A1A6, A1B6 GSO- 480- A 1A6, A1C6, A2A6, B1A6, B1B3, E284 CAR 13 B1B6, B1C6, B1E6, B1F6, B1G6, B1J6, B2C6, B2D6, B2G6, B2H6 IGSO- 480- A1A6, A1B6, A1C6, A1D6, A1E6, A1F6, A1G6 O- 480- 3 O- 540- A1A, A1A5, A1B5, A1C5, A1D, E295 CAR 13 A1D5, A2B, A3D5, A4A5, A4B5, A4C5, A4D5, B2B5, B2C5, B2C5D, B4A5, B4B5, B4B5D, D1A5, E1A, E4A5, E4B5, D1A5, E1A, E4A5, E4B5, E4C5, F1A5, F1B5, G1A5, G2A5, J1A5D, J1B5D, J1C5D, J1D5D, J2A5D, J2B5D, J2C5D, J2D5D, J3A5, J3A5D, J3C5D, L3C5D VO- 540- A1A, A2A, B1A, B1B, B1B3, B1C, E304 CAR 13 B1D, B1E, B1F, B1G, B1H3, B2A, B2C, B2D, B2E, B2G, C1A, C1B, C1C3, C2A, C2B, C2C United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SE8776SW FAA Form 8110-2 (5/14) Page 12 of 14 Date of Issuance: April 26, 1994 Date Amended: February 06, 1996 Date of Reissuance: October 31, 2016 The following is the engine eligibility for the major repairs accomplished according to EC Spec. 93-10-1 and EC66029: *Make *Model *TCDS *Reg./Part LYCOMING IO- 540- A1A5, B1A5, B1B5, B1C5, C1B5, 1E4 CAR 13 ENGINES C1C5, C2C, C4A5, C4B5, C4B5D, C4C5, C4D5D, D4A5, D4B5, D4C5, E1A5, E1B5, E1C5, G1A5, G1B5, G1C5, G1D5, G1E5, G1F5, J4A5, K1A5, K1A5D, K1B5, B1B5D, K1C5, K1D5, K1E5, K1E5D, K1F5, K1F5D, K1G5, K1G5D, K1H5, K1J5, K1J5D, K1K5, L1A5, L1A5D, L1B5D, L1C5, M1A5, M1A5D, M1B5, M1B5D, M2A5D, N1A5, N1A5D, P1A5, R1A5, S1A5, T4A5, T4A5D, T4B5D, T4C5D, U1A5D, U1B5D, V4A5D, W1A5D, W3A5D AEIO- 540- D4A5, D4B5, D4C5, K1A5D, K1B5, 1E4 CAR 13 K1D5, K1F5D, K1G5, K1G5D, K1H5, K1J5, K1J5D, L1B5, L1B5D HIO- 540- A1A (T)IO- 540- E1B5 **IVO- 540- A1A E11EA CAR 13** **TVO- 540- A1A 1E14 CAR 13** TIO- 540- A1A, A1B, A1C, A2A, A2B, A2C, E14EA CAR 13 AA1AD, AB1AD, AE2A, AF1A, C1A, C1AD, E1A, E1B5, F2B5, G1A, H1A, J2B, J2BD, K1AD, N2BD, R2AD, S1AD, T2AD, U2A, V2AD, W2A LTIO- 540- F2BD, J2B, J2BD, K1AD, N2BD, R2AD, U2A, V2AD, W2A **TVO- 540- A1A 1E14 CAR 13 TIVO- 540- A2A** **IGO- 540- A1A, A1B, A1C, B1A, B1B, B1C 1E11 CAR 13** United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SE8776SW FAA Form 8110-2 (5/14) Page 13 of 14 Date of Issuance: April 26, 1994 Date Amended: February 06, 1996 Date of Reissuance: October 31, 2016 The following is the engine eligibility for the major repairs accomplished according to EC Spec. 93-10-1 and EC66029: *Make *Model *TCDS *Reg./Part LYCOMING IGSO- 540- A1A, A1C, A1D, A1E, A1F, A1H, 1E7 CAR 13 ENGINES B1A, B1C **TIO- 541- A1A, E1A4, E1B4, E1C4, E1D4 E10A6 CAR 13** **TIGO- 541- D1A, D1B, E1A, G1AD E19EA FAR 33** **IO- 720- A1A, A1B, A1BD, B1A, B1B, B1BD, 1E15 CAR 13 C1B, C1BD, D1B, D1BD, D1C, D1CD** FRANKLIN 6A4- 145- A3 E238 CAR 13 6A4- 150- B3, B4, B31 6A4- 165- B3, B4, B6, B6F 6AG4- 185- B12 6A4- 200- C6 6V4- 178- B3, B31, B32, B33 E244 CAR 13 6V4- 200- C32, C33 6A- 335- A, B, B1, B1A, D 6V- 335- A, B 6AS- 335- A, B E5EA CAR 13 4A- 235- B, B2, B3, B4, B6 E6EA CAR 13 6A- 350- C1, C1A, C2, C2A, D, D1, D1A, E9EA CAR 13 D1B 6V- 350- A, B 6AS- 350- A, A1 E18EA FAR 33 2A- 120- A, B, C, D E24EA FAR 33 6VS- 335- A, A1, B, B1 1E2 6V- 335- A1A, A1B JACOBS LA 1 ATC31 PAGE 28 CAR 13 L- 3 ATC75 PAGE 28 L- 4 (R-755-9) 121 PAGE 29 L- 5 195 PAGE 31 L- 6 (R-915) R- 755 A1, A2, A2M, A2M1, B1, B2, B2M, E237 CAR 13 E **JACOBS- R- 755 S, SM E1SW FAR 33 PAGE** United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SE8776SW FAA Form 8110-2 (5/14) Page 14 of 14 Date of Issuance: April 26, 1994 Date Amended: February 06, 1996 Date of Reissuance: October 31, 2016 The following is the engine eligibility for the major repairs accomplished according to EC Spec. 93-10-1 and EC66029: *Make *Model *TCDS *Reg./Part PRATT & R 985 SB, -2, -3, T1B2, T1B3, B-4, B-5 E123 CAR 13 WHITNEY R 1340 S1H1, S1H1-G, S1H2, S1H4, E129 CAR 13 S1H5-G, S3H2, -61 R 1340 S3H1-G, -59 E142 CAR 13 R 1340 S3H1 E143 CAR 13 R 1830 SC-G, SC3-G, S1C-G, S1C3-G, E186 CAR 13 S3C4-G, S4C4-G R 2000 2SD-G, 2SG1-G, D-4, 2SD13-G, E230 CAR 13 D-3, D-5, D14, D7 R 2000 E1 E257 CAR 13 R 2800 CA15, CA3, CA17, CA5, CA18, E231 CAR 13 CA19 R 2800 CB3, CB16, CB17, CB4 E264 CAR 13 R 4360 TSR3-G, B6, B6, B7, B13, B14, E247 CAR 13 CB2 **RANGER 6- 440- C2, C3, C4, C5 E216 CAR 13** **ROLLS GIPSY 6L1A 30 MK.2 E294 CAR 10** ROYCE QUEEN GIPSY 6L1A 70-4, 70 MK.2, 70 MK.3 E310 CAR 10 QUEEN C 90- 8F, 8FJ, 12F, 12FH, 12FJ, 12FP, E31N CAR 10 14F, 14FH, 14FJ, 16F O 200- A, B, C O 300- A, B, C, D E41N CAR 10 O 240- A E11EU FAR 21.29 (FAR 33) WRIGHT R 2600 742C14BB1, 2, 3 E248 CAR 13 R 1300 957C7BA1 E261 CAR 13 R 1300 990C7BA1 E289 CAR 13 R 3350 956C18CA1, 957C18CB1 E270 CAR 13 R 3350 34, 91, 972TC18DA1, 972TC18DA2, E272 CAR 13 972TC18DA3, 972TC18DA5 R 3350 981TC18EA1, 988TC18EA1, 2, 3, 4, E287 CAR 13 5, 6 -END- ## Every issue (1) - October 31, 2016: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/e3/29/e3292210e3926f9d75ae5092c2aa88deb084ee9fa91fd047645985998629351a) --- From OpenAirDocs.org, an independent open copy of FAA and NTSB data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.