STC SA02930NY

FAA Form 8110-2 (8/13) Page 1

Part of the Civil Air)HGHUDO$YLDWLRQ Regulations Original Product – Type Certificate Number: MDNH:

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IMPORT SA02930NY Insight Instrument Corporation 599 Industrial Drive Fort Erie, Ontario Canada L2A 5M1 * * * * See attached FAA Approved Model List dated 8/7/2014 or later FAA approved revisions for the list of approved airplane models.

1. Installation of Insight Instrument Corporation Graphic Engine Monitor (GEM 610C) models G3, G2, and G1 and 1200C model G4 as primary Cylinder Head Temperature (CHT), Exhaust Gas Temperature (EGT), and Turbine Inlet Temperature (TIT) Instruments in accordance with Insight Instrument Corporation Master Document List MDL 610C-000 Rev. 10 and Installation Manual Document No. 070906 as specified in AML SA02930NY or later Transport Canada approved revisions..

2. Operation must be in accordance with Flight Manual Supplements 610C-FMS Issue 3 (models G3, G2, G1) and G4-FMS Issue 1 (model G4) as specified in AML SA02930NY or later Transport Canada approved revisions.

(See Description of Type Design Change continued on Page 3 of 3)

1. The installer must determine whether this design change is compatible with previously approved modifications.

2. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.

December 7, 2010 June 12, 2012, January 16, 2013 March 1, 2011 August 7, 2014 Gaetano Sciortino Manager New York Aircraft Certification Office

FAA Form 8110-2 (8/13) Page 2

To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement):

SA02930NY

FAA Form 8110-2 (8/13) Page 3

SA02930NY Date amended: August 7, 2014

Description of Type Design Change (continued):

3. Maintenance must be in accordance with Insight Instrument Corporation Instructions for Continued Airworthiness - Document No. 610C-ICA Issue 4 (models G3, G2, G1) and G4-ICA Issue 1 (model G4) or later Transport Canada approved revisions. Compliance with Chapter 4.0, “Airworthiness Limitations” of this Instruction for Continued Airworthiness is mandatory.

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