What it approves
Installation of a Max-Viz, Inc. Enhanced Vision System (EVS) Model 1500
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.
FAA Form 8110-2 (5/14) Page 1 of This certificate issued to:
Part of the Original Product – Type Certificate Number: Make:
By Direction of the Administrator Signature Title SR02751NY Aviation Completion Innovations, Inc.
3 Caesar Place Moonachie, New Jersey 07074 Federal Aviation Regulations.
29 Configuration 1: Installation of a Max-Viz, Inc. Enhanced Vision System (EVS) Model 1500 in accordance with Air Concepts International, Inc., Installation Drawing List No. 31101-804-INS, Revision B, dated August 1, 2009 (Retractable Mount).
Configuration 2: Installation of a Max-Viz, Inc. Enhanced Vision System (EVS) Model 1500 in accordance with Air Concepts International, Inc., Installation Report No. 41016-804-INS, Revision IR, dated May 2, 2008 (Fixed Mount).
Configuration 3: Installation of a FLIR System Inc. Enhanced Vision System Model EVS 3 IR camera in accordance with Air Concepts International, Inc., Installation Drawing List No. 41016-804-INS, Revision A, dated November 5, 2010.
1. Instructions for Continued Airworthiness Configuration 1: Modified aircraft for the Retractable Mount EVS are to be maintained in accordance with Air Concepts International, Inc. Instructions for Continued Airworthiness Report No. IC00139.05, Revision IR, Dated November 18, 2009, FAA accepted March 10, 2010.
(See Limitations and Conditions continued on Page 3 of 3) Anthony E. Gallo Manager New York ACO Branch Agusta S.p.A AB139, AW139
January 31, 2019 December 20, 2010, July 12, 2011 November 30, 2007 March 19, 2010 R00002RD 3
FAA Form 8110-2 (5/14) Page 2 of
To (Name and address of transferee)
From (Name and address of grantor)
3 SR02751NY
FAA Form 8110-2 (5/14) Page 3 of 3 Date Reissued: January 31, 2019
Configuration 2: Modified aircraft for the Fixed Mount EVS are to be maintained in accordance with Air Concepts International, Inc. Instructions for Continued Airworthiness Report No. IC00139.05-1, Revision IR, Dated November 15, 2009, FAA accepted March 10, 2010.
Configuration 3: Modified aircraft for the Fixed Mount EVS3 are to be maintained in accordance with Air Concepts International, Inc. Instructions for Continued Airworthiness Report No. IC00139.05-2, Revision IR, Dated April 12, 2010, FAA accepted December 20, 2010.
2. Rotorcraft Flight Manual Supplements Configuration 1: Modified aircraft for the Retractable Mount EVS are to be operated in accordance with Air Concepts International Rotorcraft Flight Manual Supplement No. 00139.05, Revision A, FAA approved July 12, 2011.
Configuration 2: Modified aircraft for the Fixed Mount EVS are to be operated in accordance with Air Concepts International Rotorcraft Flight Manual Supplement No. 00139.05-1, Revision A, FAA approved July 12, 2011.
Configuration 3: Modified aircraft for the Fixed Mount EVS3 are to be operated in accordance with Air Concepts International Rotorcraft Flight Manual Supplement No. 00139.05-2, Revision A, FAA approved July 12, 2011.
3. The installer must determine whether this design change is compatible with previously approved modifications.
4. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.
....…End…....
SR02751NY
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.