STC SA2081WE

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA2081WE This certificate issued to: Madras AIr Service Port O3 & 3 of the Civil Air Fuyulationa: • (see applicable I. C. Data Sheets).

Original Product -Typobertificate Lumbar: A-777 3A15 Make: Beech Model: A35 Through G35 and 35-33, 35-A33. 35-B33, 35R 35-C33, 35-C33A, 333, Description of Type Design Change: P33, F33А, G33, H35, J35, K35, M35, N35, and P35.

Installation of Madras Air Service Part No. MAS 102 wing tips in accordance with Madras Air Service Installation Instructions dated 11-14-69 Revised 2-12-70.

Drawing needed to manufacture parts required for this modification is MAS 102.

See continuation sheets 3 and 4.

The approval of this change in type design applies basically to the above model aircraft only. This approval should not be extended to other aircraft 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 other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. Madras Air Service FAA Approved Airplane Flight Manual Supplement dated 12 February 1970, Revised October 16, 1987 is required.

February 4, 1969 April 5, 1974 Date of Application: Date Reissued:

December 24, 1969 February 18, 1970, December 7, 1987 Date of Issuance: . Date Amended:

FEDERAL AVIATION By Direction of the Administrator (Signature) Assistant Manager, Seattle Aircraft Certification Office (Title)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA2081WE Supplemental Type Certificate ADDENDUM NO. SA2081WE Limitations and Conditions: The conditions and limitations of Aircraft Specifications A-777 and 3A15 apply except as follows:

This STC Addendum, which is a part of Supplemental Type Certificate No. SA2081WE, prescribes conditions and limitations under wich the product for which the STC was issued meets the airworthiness requirements of the Civil Air Regulations.

A copy of this SIC Addendum is required to be maintained as a part of the modified aircrafts permanent records.

A. AIRCRAFT APPROVED BY TYPE CERTIFICATE NO. A-777 Models A35, B35, C35, D35, E35, G35, 35R, 4 PCLM (Normal Category), as modified by STC SA2081WE.

Approved for operation in Normal Category only.

Interior Equipment Item 404 of Aircraft Specification A-777.

NOTE 1. The following placard supersedes that of Note 2 on aircraft Specification A-777 and must be displayed in front of and in clear view of the pilot:

"NORMAL CATEGORY AIRPLANE. MADRAS AIR SERVICE AFM SUPPLEMENT DATED 12 FEBRUARY 1970 IS REQUIRED FOR OPERATION OF THIS AIRCRAFT. INTENTIONAL SPINS PROHIBITED. NO ACROBATIC MANEUVERS APPROVED."

NOTE 2. The wing tips are not approved for installation on aircraft equipped with a Lycoming GO-435-D1 engine in accordance with Aircraft Specification A-777, Note 4.

B. AIRCRAFT APPROVED BY TYPE CERTIFICATE NO. 3A15 I. Models 35-33, 35-A33, 35-B33, 35-C33, 35-C33A E33, F33, F33A, G33, H35, J35, K35, M35, N35, and P35. PCLM (Normal Category), as modified by STC SA2081WE.

FAA FORM 8110-2-1 (10-69) PAGE 3OF 4 PAGES

Approved for operation in Normal Category Interior Equipment Item 403 of Aircraft Specification 3A15.

Note 1. The following placard supersedes that of Note 2(a) of Aircraft Specification 3A15 and must be displayed in full view of the pilot:

"NORMAL CATEGORY AIRPLANE. MADRAS AIR SERVICE AFM SUPPLEMENT DATED 12 FEBRUARY 1970 IS REQUIRED FOR OPERATION OF THIS AIRCRAFT. INTENTIONAL SPINS PROHIBITED. NO ACROBATIC MANEUVERS APPROVED."