STC SA2016NM

This Certificate issued to ROBERT W. MURRAY 24196 Zancon Mission Viejo, California 92692 Part * of the Civil Air Regulations. *see page 3 Original Product Type Certificate Number :

* see page 3 * * Description of Type Design Change : Installation of a de-icing system on the Rolls Royce P/N RK29954A engine inlet cowl in accordance with Montgomery Systems Tech Drawings 46584, Revision N/C; 46585, Revision N/C; and 46586, Revision N/C, all dated March 16, 1981, or later approved revisions, as an alternate to the Dunlop 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 15, 1982

Date of issuance : November 2, 1983

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

Date amended : October 11, 1989, August 31, 2006

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

NOTE:

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Number SA2016NM

Original Product — Continued

*Aircraft Make/Model

Mfg. or TC Holder Type Certificate No.

Certification Basis F-27A, F-27F, F-27G, F-27J, F-27M Fairchild 7A1 CAR part 4b

FH-227, FH-227B, FH-227C, FH-227B, FH-227C, FH-227D, FH-227E Fairchild Hiller 7A1 CAR part 4b

G-159 Gulfstream American Corporation 1A17 CAR part 4b

Viscount 810 Vickers-Armstrong A-814 CAR part 10

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