STC SR00565DE

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate $Q\DOWHUDWLRQRIWKLVFHUWLILFDWHLVSXQLVKDEOHE\DILQHRIQRWH[FHHGLQJRULPSULVRQPHQWQRWH[FHHGLQJ\HDUVRUERWK7KLVFHUWLILFDWHPD\EHWUDQVIHUUHGRUPDGH DYDLODEOHWRWKLUGSHUVRQVE\OLFHQVLQJDJUHHPHQWVLQDFFRUGDQFHZLWK&)53RVVHVVLRQRIWKLV6XSSOHPHQWDO7\SH&HUWLILFDWH 67& GRFXPHQWE\SHUVRQVRWKHUWKDQ WKH67&KROGHUGRHVQRWFRQVWLWXWHULJKWVWRWKHGHVLJQGDWDQRUWRDOWHUDQDLUFUDIWDLUFUDIWHQJLQHRUSURSHOOHU7KH67&¶VVXSSRUWLQJGRFXPHQWDWLRQ GUDZLQJVLQVWUXFWLRQV SURSHOOHUPXVWSURYLGHWKDWSHUVRQZLWKZULWWHQSHUPLVVLRQDFFHSWDEOHWRWKH)$$ 5HI&)5  )$$)RUP  683(56('(635(9,286(',7,21 3DJHRIBBB

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SR00565DE Air Comm Corporation 1575 West 124th Ave., Suite 210 Westminster, CO 80234 27 Federal Aviation Regulations Eurocopter H88EU EC135P2, EC135P2+, EC135T2, EC135T2+ Installation of Cabin Air Conditioning System in accordance with Air Comm Corporation Master Drawing List Report No.

DL-EC135, Revision A, dated October 19, 2004, FAA approved November 24, 20 04, or later FAA approved revision.

June 28, 2004 November 24, 2004 June 22, 2005; June 18, 2020

Todd Dixon Manager, Denver ACO Branch Compliance and Airworthiness Division 3 June 18, 2020

1. Instructions for Continued Airworthiness, Air Comm Corporation Repor t EC135-200M-1, Revision Original, dated August 25, 2004, FAA accepted November 24, 2004, or later FAA accepted revi sion is required for this installation.

(See Continuation Page 3) Digitally signed by TODD G DIXON Date: 2020.06.18 06:31:48 -06'00'

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate $Q\DOWHUDWLRQRIWKLVFHUWLILFDWHLVSXQLVKDEOHE\DILQHRIQRWH[FHHGLQJRULPSULVRQPHQWQRWH[FHHGLQJ\HDUVRUERWK7KLVFHUWLILFDWHPD\EHWUDQVIHUUHGRUPDGH DYDLODEOHWRWKLUGSHUVRQVE\OLFHQVLQJDJUHHPHQWVLQDFFRUGDQFHZLWK&)53RVVHVVLRQRIWKLV6XSSOHPHQWDO7\SH&HUWLILFDWH 67& GRFXPHQWE\SHUVRQVRWKHUWKDQ WKH67&KROGHUGRHVQRWFRQVWLWXWHULJKWVWRWKHGHVLJQGDWDQRUWRDOWHUDQDLUFUDIWDLUFUDIWHQJLQHRUSURSHOOHU7KH67&’s supporting documentation (drawings, instructions, SURSHOOHUPXVWSURYLGHWKDWSHUVRQZLWKZULWWHQSHUPLVVLRQDFFHSWDEOHWRWKH)$$ 5HI&)5  )$$)RUP  683(56('(635(9,286(',7,21 3DJHRIBBB

Date oI transfer:

SR00565DE SR00565DE 3

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate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

(Continuation Sheet) Number: SR00565DE 3 3 Limitations and Conditions Continued:

2. FAA Approved Flight Manual Supplement, Document No. EC135-1, Revision Original, approval date of November 24, 2004, or later approved revision is required.

3. Approval of this change in type design applies to the model of aircraft li sted above only.

4. Compatibility of this design change with previously approved alterati ons must be determines by the installer.

5. If the holder agrees to permit another person to use this certificate to a lter the product, the holder shall give the other person written evidence of that permission.

6. A copy of this certificate and the appropriate flight manual supplement as listed above must be maintained as a part of the permanent record for the altered aircraft.

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