STC SA1147CE

FAA Form 8110-2 (5/14) Page 1 of 3 Number: SA1147CE This certificate issued to: Honeywell International Inc.

21111 N 19th Ave Phoenix, Arizona 85027 Part 23 of the Federal Aviation Regulations.

Make: Piper A7SO Model: PA 34-200T, PA 34-220T Description of Type Design Change:

Installation of King Model KFC 200 2 axis (3 optional) Flight Control System, Autopilot only or Autopilot with Flight Director.

This approval should not be extended to other specific airplanes of this model on which other previously approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those previously approved modifications will introduce no adverse effect upon the airworthiness of that airplane.

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.

Date of Application: 6-20-75 Date Reissued: 1-31-95; 2-28-00; 4-6-20 Date of Issuance: 7-24-75 Date Amended: 1-7-76; 1-27-76; 9-13-77; 1-19-81; 6-27-83 By Direction of the Administrator Signature Richard B. Sleigh Title ODA Administrator, ODA-602216-NM

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

To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement):

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA1147CE

FAA Form 8110-2 (5/14) Page 3 of 3 Description of Type Design Change: (continued)

1. For PA-34-200T equipped with KCS 55 (or KCS 55A)/Kl 255, Master Drawing List 155-9033, Rev. 2. dated 7-21-75 thru Rev.

11, dated 6-2-78.

1b. For PA-34-200T equipped with KCS 55 (or KCS 55A)/Kl 255 (or KI 256 or KG 258), Master Drawing List 155-9033-00, Rev.8, dated 7-1-77 thru Rev. 11, dated 6-2-78.

1c. For PA-34-200T equipped with KCS 55A/Kl 256 or KG 258. Master Drawing List 155-9033-00, Rev. 8, dated 7-1-77 or later FAA Approved revision.

1d. For PA-34-200T incorporating fail safe trim with visual/aural alerting, Master Drawing List 155-9033-00, Rev. 11, dated 6-2-78 or later FAA Approved revision.

1e. For PA-34-200T incorporating aural autopilot disconnected alerting and non-coupling go-around, Master Drawing List 155- 9033-00, Rev. 12, dated 7-2-79 or later FAA Approved revision.

1f. For PA-34-220T, Master Drawing List 155-9033-00, Rev. 13, dated 1-5-81 or later FAA Approved revision.

1g. For PA-34-200T/PA-34-220T incorporating optional yaw damper system, Master Drawing List 155-9033-00, Rev.14, dated 5- 5-83 or later FAA Approved revision.

2a. For PA-34-200T equipped with KCS 55 (or KCS 55A)/KI 255, Airplane Flight Manual Supplement 006-0302-00, Rev. a, dated 7-24-75 thru Rev. 6. dated 6-2-78.

2b. For PA-34-200T equipped with KCS 55 (or KCS 55A)/Kl 255 (or KI 256 or KG 258). Airplane Flight Manual Supplement 006- 0302-00. Rev. 3, dated 7-1-77 thru Rev. 6, dated 6-2-78.

2c. For PA-34-200T equipped with KCS 55A/KI 256 or KG 258, Airplane Flight Manual Supplement 006-0302-00, Rev. 3, dated 7-1-77; or, for airplane incorporating KG 258 without flight director, 006-0302-01, Rev. 0. dated 9-13-77; or later FAA Approved revision.

2d. For PA-34-200T incorporating fail safe trim with visual/aural alerting, Airplane Flight Manual Supplement 006-0302-00, Rev.

6, dated 6-2-78; or, for airplane incorporating KG 258 without flight director, 006-0302-01, Rev. 3. dated 6-2-78; or later FAA Approved revisions.

2e. For PA-34-200T incorporating aural autopilot disconnect alerting and non-coupled go-around, Airplane Flight Manual Supplement 006-0302-00, Rev. 7, dated 7-2-79: or. for airplanes incorporating KG 258 without flight director, 006-0302-01, Rev. 4. dated 7-2-79; or later FAA Approved revisions.

2f. For PA-34-220T, Airplane Flight Manual Supplement 006-0391 -00, Rev. 0. dated 1-7-81: or. for airplanes incorporating KG 258 without flight director. 006-0391-01, Rev. 0, dated 1-7-81: or later FAA Approved revisions.

2g. For PA-34-200T incorporating optional yaw damper system, Airplane Flight Manual Supplement 006-0302-00, Rev. 8, dated 6-27-83; or. for airplanes incorporating g KG 258 without flight director, 006-0302-01, Rev. 5, dated 6-27-83; or later FAA Approved revisions.

2h. For PA-34-220T incorporating optional yaw damper system, Airplane Flight Manual Supplement 006-0391-00. Rev. 2. dated 6-27-83: or, for airplanes incorporating KG 258 without flight director, 006-0391 -01, Rev. 2, dated 6-27-83; or later FAA Approved revisions ---------------------------------------------------------------------------END--------------------------------------------------------------------------