STC SA1778CE-D

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Page 1 of 3 FAA Form 8110-2 (5/14)

Number: SA1778CE-D This certificate issued to: Honeywell International Inc.

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

Original Product – Type Certificate Number: Make: Piper Model:

A25SO PA-46-310P, PA-46-350P

Install KAP100 single axis, KAP150 two axis or KFC150 two axis Flight Control System with optional third (yaw) axisand optional KAS297BVertical Speed and Altitude Selector.

This approval should not be extended to other specific airplanesof this model on which other previously approved modificationsare incorporated, unlessit isdetermined that the interrelationship between this change and any of those other previously approved modificationswill introduce no adverse effect upon the airworthinessof 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: 9-21-83 Date Reissued: 2-28-95; 2-28-00; 4-10-20

Date of Issuance: 10-26-83 Date Amended:

10-19-88

Signature

Title Richard B. Sleigh ODA Administrator, ODA-602216-NM

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Page 2 of 3 FAA Form 8110-2 (5/14)

To (Name and address of transferee)

From (Name and address of grantor)

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

(Continuation Sheet) Number: SA1778CE-D

Description of Type Design Change: (continued) REQUIRED DATA:

Model PA-46-310P KAP100 Single Axis Flight Control System

1. Master Drawing List 155-9296-00, dated 9-20-83.

2. Airplane Flight Manual Supplement 006-0428-00, dated 10-26-83.

KAP150 and KFC150 Two Axis Flight Control System 1a. Master Drawing List 155-9296-00, dated 9-20-83for Field Installation.

1b. Master Drawing List 155-9296-01, Rev. 1, dated 10-24-83for Piper Factory Installation.

2. Airplane Flight Manual Supplement 006-0428-01, dated 10-26-83.

Optional KAS297BVertical Speed and Altitude Selector 1a. Master Drawing List 155-9296-00, dated 9-20-83for Field Installation.

1b. Master Drawing List 155-9296-01, Rev. 1, dated 10-24-83for Piper Factory Installation.

2. Airplane Flight Manual Supplement 006-0428-092, dated 10-26-83.

Model PA-46-350P KAP100 Single Axis Flight Control System

1. Master Drawing List 155-9296-00, Rev. 2, dated 9-21-88.

2. Airplane Flight Manual Supplement 006-0428-00, Rev 1, dated 10-19-88.

KAP150 and KFC150 Two Axis Flight Control System 1a. Master Drawing List 155-9296-00, Rev. 2, dated 9-21-88for Field Installation.

1b. Master Drawing List 155-9296-01, Rev. 3, dated 10-19-88for Piper Factory Installation.

2. Airplane Flight Manual Supplement 006-0428-01, Rev. 1, dated 10-19-88.

Optional KAS297BVertical Speed and Altitude Selector 1a. Master Drawing List 155-9296-00, Rev. 2, dated 9-21-88for Field Installation.

1b. Master Drawing List 155-9296-01, Rev. 3, dated 10-19-88for Piper Factory Installation.

2. Airplane Flight Manual Supplement 006-0428-092, Rev. 1, dated 10-19-88.

Later FAA approved revisionsto above listed data are incorporated without further revision to the Supplemental Type Certificate.

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