STC SR09474NY-D

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

Part of the

Signature

Title SR09474NY-D Sikorsky Aircraft Corporation 6900 Main Street Stratford, CT 06615 Federal Aviation Regulations.

1. Installation of a VIP Interior configuration in accordance with Keystone Helicopter Master Drawing List S00-13005 Revision E, dated May 17, 2007, or later FAA approved revision:

a. Configuration 1: Split Cabin VIP defined by S00-13005-01

b. Configuration 2: Full Cabin VIP defined by S00-13005-03

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

1. For all configurations listed above, FAA STC SR03077AT is a pre-requisite for installation.

2. The four side facing seats are only approved for these interior arrangements. Any changes in location will require additional FAA approval.

3. 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 November 26, 2007, October 1, 2011, December 17, 2014 February 21, 2007, May 25, 2007, January 18, 2010 November 21, 2005 August 18, 2006 R00024BO 3

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

To (Name and address of transferee)

From (Name and address of grantor)

3 SR09474NY-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, VIP Interior Installed on Sikorsky S-92A Aircraft is required for this modification:

a. Configuration 1: Report No. S04-73007 Rev. D, dated December 30, 2009 or later FAA accepted revision

b. Configuration 2: Report No. S04-73005 Rev. D, dated December 30, 2009 or later FAA accepted revision

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

a. Configuration 1: Supplement No. S09-63001 Rev. B, dated January 18, 2000 or later FAA accepted revision

b. Configuration 2: Supplement No. S09-63002 Rev. A, dated January 18, 2000 or later FAA accepted revision

4. 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 # N02109-C-1

5. The VIP State Interior is not compatible with any standard aircraft seating installations defined on Sikorsky S-92A TCDS R00024BO.

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

7. 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.

Certification Basis:

The Certification Basis for this modification is the same as defined on Type Certificate Data Sheet R00024BO, FAR part 29 through Amendment 29-47, with the following additional requirements:

1. No door may be installed in any partition between passenger compartments unless that door has a means to latch it in the open position. The latching means must be able to withstand the loads imposed upon it by the door when the door is subjected to the inertia loads resulting from the ultimate static load factors prescribed in Sec. 29.561(b)(3).

(STC2858RC-R Issue Paper A-1, dated August 10, 2006).

2. If it is necessary to pass through a doorway separating the passenger cabin from the other areas to reach a required emergency exit from any passenger seat, the door must have a means to latch it in the open position. The latching means must be able to withstand the loads imposed upon it by the door when the door is subjected to the inertia loads resulting from the ultimate static load factors prescribed in Sec. 29.561 (b)(3). (STC2858RC-R Issue Paper A-1, dated August 10, 2006).

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