STC SR00489SE

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate SR00489SENumber:

This certificate issued to: Paravion Technology, Inc.

2001 Airway Avenue Fort Collins, CO 80524 BB__.

Make:Original Product BellH2SW7\SH&HUWLILFDWH1XPEHU Model: 407 Description of Type Design Change:

1. Installation of tailrotor drive shaft driven Air Conditioning System in accordance with FAA approved Paravion Technology, Inc. Master Drawing List No. DL-407AC-110, Revision Q, dated August 4, 2021.

2. Instructions for Continued Airworthiness (ICA), Document No. PR-407AC-120M, Revision 9, dated April 6, 2021, or later FAA accepted revision is required for this installation.

3. Operation must be in accordance with Rotorcraft Flight Manual Supplement, document number PR-407AC-110M, Revision 4, dated November 17, 2021, or later FAA approved revision.

1. Approval of this change in type design applies to the model of rotorcraft listed above only.

2. This STC is applicable to all serial numbers for these Make/Models.

July 3, 1996Date of Application: Date Reissued:

December 5, 1997 November 24, 2021Date of Issuance: Date Amended:

Robert C. Jones Acting Manager, Denver ACO Branch Title: Compliance and Airworthiness Division $Q\DOWHUDWLRQRIWKLVFHUWLILFDWHLVSXQLVKDEOHE\D ILQHRIQRWH[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 3DJH RIBBB 3

I o United States of America Department of Transportation Federal AviationAdministration Supplemental Type Certificate SR00489SENumber:

Date oI transfer:

$Q\DOWHUDWLRQRIWKLVFHUWLILFDWHLVSXQLVKDEOHE\D ILQHRIQRWH[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 3DJH RIBBB 3

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SR00489SE Limitations and Conditions Continued:

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.

5. 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.

6. Certification Basis:

For components and areas not affected by the change, the original certification basis as shown on TCDS H2SW, Revision 50.

For components and areas affected by the change, based on Title 14, Code of Federal Regulations Sections 21.115 and 21.101, and FAA Order 8110.48, the type certification basis due to this modification is the original certification basis for the Model Bell 407 shown on TCDS H2SW, Revision 50, plus 14 CFR part 27, effective February 1, 1965, including Amendments 27-1 through 27-37 as follows:

§§ 27.1(b) at 27-0, 27.21(a)(b) at 27-21, 27.25(a) at 27-14, 27.27(b) at 27-2, 27.301(a)

(b)(c) at 27-0, 27.303 at 27-0, 27.305(a) at 27-0, 27.307(a) at 27-26, 27.321(a) at 27-11, 27.337(a) at 27-26, 27.561(a)(b)(c)(d) at 27-30, 27.601(a) at 27-0, 27.603(a)(b)

(c) at 27-16, 27.605(a) at 27-16, 27.607(a) at 27-4, 27.609(a) at 27-0, 27.613(a)(b)(c)

(d) at 27-26, 27.619(a)(b) at 27-0, 27.625(a)(b)(c) at 27-0, 27.853(a) at 27-17, 27.1301

(d) at 27-0, 27.1351(a)(b)(1)(i) at 27-13, 27.1357(a)(c) at 27-13, 27.1365(a)(b) at 27-35,

27.1435(b) at 27-0, 27.1529 at 27-18, 27.1581(b)(c) at 27-14, 27.1583(a)(c)(d)(e)(g) at 27-16, 27.1585(a) at 27-21, 27.1587(b) at 27-21.

Part 27, Appendix A, A27.1(a)(b)(c) at 27-18, A27.2(a)(b) at 27-18, A27.3(a)(b)(c)(d)(e)

(f)(g) at 27-18, A27.4 at 27-24.

Regulations at a later amendment than specified in TCDS H2SW:

§ 27.1309(a) at 27-46.

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