STC SR02108NY-D

FAA Form 8110-2 (5/14) Page 1 of

Part of the

Signature

Title SR02108NY-D Sikorsky Aircraft Corporation 6900 Main Street Stratford, CT 06615 Federal Aviation Regulations.

1. Installation of an Executive VIP Interior in accordance with Keystone Helicopter Installation drawing List:

Configuration 1: IDL00793 Rev. A, dated 01/10/2006 or later FAA approved revision.

Configuration 2: IDL00793.1 Rev. –, dated 05/19/2006 or later FAA approved revision.

Configuration 3: IDL00793.2 Rev. A, dated 06/29/2008 or later FAA approved revision.

Configuration 4: IDL00793.3 Rev. A, dated 11/04/2009 or later FAA approved revision.

Configuration 5: IDL00793.4 Rev. B, dated 05/11/2010 or later FAA approved revision.

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

1. Pre-Requisites: AAR STC SR03077AT is a pre-requisite for Configurations #1,# 2 and #3. Sikorsky TC Top Kit 92276-50016-011 is a pre-requisite for Configuration # 4 and #5. KHC STC SR01973NY-D is a pre-requisite for Configurations #2, #4 and #5.

2. Sikorsky Type Design approved or FAA approved life rafts must be stored external to the rotorcraft with this STC installed when over-water operation is conducted.

(See Limitations and Conditions continued on Page 3 of 3) Gaetano Sciortino Manager New York Aircraft Certification Office Sikorsky S-92A October 1, 2011, December 17, 2014 January 12, 2006, May 19, 2006, June 30, 2008, October 28, 2009, November 10, 2009, June 2, 2010 June 16, 2004 December 20, 2005 R00024BO 3

FAA Form 8110-2 (5/14) Page 2 of

To (Name and address of transferee)

From (Name and address of grantor)

3 SR02108NY-D

FAA Form 8110-2 (5/14) Page 3 of

3 Date Reissued: December 17, 2014

Description of Type Design Change (continued):

2. Keystone Helicopter Instructions for Continued Airworthiness, Executive VIP Interior Installed on Sikorsky S-92A Aircraft is required for this modification:

Configuration 1: Report No. IC00793 Rev. B, dated October 27, 2009 or later FAA accepted revision Configuration 2: Report No. IC00793.1 Rev. A, dated October 27, 2009 or later FAA accepted revision Configuration 3: Report No. IC00793.2 Rev. A, dated October 27, 2009 or later FAA accepted revision Configuration 4: Report No. IC00793.3 Rev. –, dated October 01, 2009 or later FAA accepted revision Configuration 5: Report No. IC00793.4 Rev. –, dated March 08, 2010 or later FAA accepted revision

3. FAA Approved Rotorcraft Flight Manual Supplement is required for this modification:

Configuration 1: Supplement No. FM00793 Rev. 1, dated 10/28/2009 or later FAA approved revision Configuration 2: Supplement No. FM00793.1 Rev.1, dated 10/28/2009 or later FAA approved revision Configuration 3: Supplement No. FM00793.2 Rev. 1, dated 10/28/2009 or later FAA approved revision Configuration 4: Supplement No. FM00793.3 Rev. –, dated 11/10/2009 or later FAA approved revision Configuration 5: Supplement No. FM00793.4 Rev. –, dated 06/02/2010 or later FAA approved revision

3. Equivalent Level of Safety Finding has been made for the following regulation: 14 CFR §29.807(d)(2) at amendment 29-30 documented in ELOS Memo # N02095-C-1.

4. Compliance with the following regulations has not been demonstrated for Configuration#5– 14 CFR §29.801(a) [Amdt. 29-12], 29.1411(f)[Amdt. 29-0] and 29.1415(b) [Amdt. 29-33; Life Vests Only]

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

6. 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.

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