STC SA3132NM

This Certificate issued to ROBERT W. MURRAY 24196 Zancon Mission Viejo, California 92692 Part 4b of the Civil Air Regulations. *certification basis set forth in Type Certificate A1SO Original Product Type Certificate Number :

A1SO

Lockheed

382, 382B, E, F, G Description of Type Design Change : Installation of a de-icing system on the Hamilton Standard P/N 554654 propeller spinner in accordance with Montgomery Systems Tech Drawings 465154, Revision B, dated December 23, 1985; 465125, Revision N/C, date d October 1, 1983; and 465126, Revision B, dated December 23, 1985, or later FAA approved revisions, as an alternate to the Hamilton Standard de-icing system currently approved.

Limitations and Conditions: This approval should not be extended to other specific airplanes of this model on which other previously appr oved modifications are incorporated, unless it is determined that the interrelationship between this cha nge and any of those other previ ously approved modifications will introduce no adverse effect on the airworthiness of tho se aircraft. If the holder agrees to permit another person to use this certificate to alter the product, th e holder shall give the other person written evidence of that permission.

Date of application : October 1, 1983

Date of issuance : February 24, 1986

Date reissued : August 31, 2006, December 20, 2011

Date amended : August 31, 2006

( Signature) Haifa Haj-Eid Supervisor, Technical and Administrative Support Staff Los Angeles Aircraft Certification Office ( Title)

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