STC SR09471RC

SR09471RC Summit Aviation, Inc.

4200 Summit Bridge Rd.

Middletown, DE 19709 Part 29 the Regulations (See continuation sheet) R00024BO Sikorsky S-92A Installation of a VIP State Interior in accordance with Heritage Aviation Ltd. Master Drawing List S00-13004 Revision C, dated 07/18/2006, or later FAA approved revision. Rotorcraft Flight Manual Supplement, Heritage Aviation Ltd. Document S09-73008, Revision -, dated 08/04/2006, or later FAA approved revision is required for this installation. Instructions for Continued Airworthiness, Heritage Aviation Ltd. Document S04-73004, Revision A, dated 02/13/2006, or later revision is required for this installation.

(See continuation sheet 3 of 4) November 30, 2004 October 27, 2023 August 4, 2006 for Paul (Vu) Nguyen Manager, Central Certification Branch Compliance & Airworthiness Division Aircraft Certification Service 4

SR09471RC 4

SR09471RC Date of Issuance: August 4, 2006 Date of Reissuance: October 27, 2023

Installation of Heritage Aviation Ltd. Cabin Door Replacement, STC SR09460RC, Cabin Extension and Modified Baggage Compartment, STC SR09470RC, Aft Cabin VIP Lavatory, STC SR09469RC, and AAR Manufacturing Group, Inc. Structural Provisions for a Composite Passenger Cabin VIP Interior Composites, STC SR03077AT, are required to be installed in conjunction with this VIP State Interior. The VIP State Interior is not compatible with any standard aircraft seating installations defined on the Sikorsky S92A TCDS. This VIP State Interior installation does not include FAA approval of all interior materials, such as carpeting and decorative wall finishes, necessary to complete an interior. Additional FAA approval is required to install this material. The FAA must evaluate the installation to ensure it complies with the applicable airworthiness standards. The installer must determine whether this design change is compatible with previously approved modifications. 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). (ST2787RC-R Issue Paper A-1 Dtd 05/02/2005) 3 4

SR09471RC Date of Issuance: August 4, 2006 Date of Reissuance: October 27, 2023

Certification Basis (continued):

2. If it is necessary to pass through a doorway separating the passenger cabin from 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). (ST2787RC-R Issue Paper A-1 Dtd 05/02/2005)

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