STC SA6039SW-D

nited Stares of Sonica Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA60395W-D This certificate issued to: 11. S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, TX 76067 Certifies that the change in the type design for the following product with the limitations and conditions therefer as specified hereen meet's the airworthiness reguirements of Part 3 of the CiVil Air Hegulations Original Product - Type tientificate Numben: 1A10 Make: PIPER Model: PA-23-250 AND PA-E23-250 Description of Type Design Change:

Installation of S-TEC Manual Electric Trim System, Model ST-340, according to Bulletin No. 440, dated 9-18-85 and Master Drawing List No. 92350, dated 9-18-85 and/or later FAA Approved revisions of the above data (14 Volt System).

1. Only eligible on Piper Models PA-23-250 and PA-E23-250, S/N 27-2000 through S/N 27-7554172.

2. Also eligible on the above Models when equipped with Approved Turbocharged Engines (250 H.P.) and/or Wing Tip Tanks per STC SA1480WE.

(See Continuation Sheet, Page 2, a part of this STC.)

Date of Application: 9-23-85 Date Reissued:

Date of Issuance: 9-27-85 Date Amended:

FEDERAL AVIATION By Direction of the Administrator (Signature) COMINI STRATOR Harold W. Holdeman DAS Staff Coordinator, DAS 5 SW (Title)

47.

PAA FORM 8110-2 (10-68)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA60395W-D Limitations and Conditions: (con't) FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89635, dated 9-27-85 is required for Piper Models PA-23-250 and PA-E23-250, S/N 27-2000 through S/N 27-/5541/2 and the above Models when equipped with approved Turbocharged Engines (250 H.P.)

and/or Wing Tip Tanks per STC SA1480WE and/or later FAA Approved revisions of the above supplement.

4. Compatability of this modification with other previously approved modifications must be determined by the installer.

l irator of this certificate is punishable by a fine of not exceeding S1.000, or imprisonment not exceeding 3 years, or both

• i: /[PM 8110-2-1 (10-69) This certificate may be transferred in accordance with LAR 21.1?

nitro States of Sumerica Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number 5A60385W-D This cerlificale, issured 11. S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, TX 76067 Part 3 of the Civil Air Hegulatu-no.

Original Product - Type tiertificate Number: 3A13 Make: CESSNA Model: 102E, 182F, 182G, 182H, 1820, 182K, 102L, 182M AND 182N Description of Type Design Change:

Installation of S-TEC Manual Electric Trim System, Model ST-337, according to Bulletin No. 437, dated 9-03-85 and Master Drawing List No. 92348, dated 9-03-85 and/or later FAA Approved revisions of the above data (14 Volt System).

1. FAA Approved Supplemental Flight Manual, P/N 89625, dated 9-06-85 is required and/or later FAA Approved revisions of the above supplement.

2. Compatability of this modification with other previously approved modifications must be determined by the installer.

Date of Application: 9-05-85 Date Reissued:

Date of Issuance: . 9-06-85 Date Amended:

FEDERAL AVIATION By Direction of the Administrator (Signature) TOMINIST RATOR DAS Staff Coordinator, DAS 5 SW Harold W. Holdeman (Tille )

47.

FAA FORN 8110-2 (10-68)

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) _ (Address of transferee). (pant pa sequent) (City, Stake, and MIP code ) from (Name of grantor) (Print or type) (Address of grantor) (Number and sireel;

( City, Stale, and ZIP rode, Extent of Authority (if licensing agreement):

Signature of grantor (In ink): - 382-090