# STC SR09474RC

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Keystone Helicopter Corp., United States
- Description: Installation of a VIP Interior configurations.
- Applied: November 21, 2005
- Status date: November 26, 2007
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21
- Data sheets: [TCDS R00024BO](https://openairdocs.org/tcds/R00024BO)
- Certificate PDF: https://openairdocs.org/files/sha256/9c/bf/9cbf08259ddb493b3075653081c1ee302d44fe24a1dcc3ee37d42bf84ca7641a
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/6954A5901341037F862575FC005E85DE.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SR09474RC

## ADs that name it (0)

None.

## Approved models (1)

- Sikorsky Aircraft Corporation S-92A ([TCDS R00024BO](https://openairdocs.org/tcds/R00024BO))

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number SRO947ARC This certificate issued to: Keystone Helicopter Corporation 110 E. Stewart Huston Drive Coatesville, PA 19320 Part 29 of the Reyulations.

Original Product -- Type Terlificut Number: R00024BO Make: Sikorsky Model: S- 92A Certification Basis:

suspended, revoked or a terminution date is otherwise established by the Administrater of the Telerat Aviatien Administration.

Lute of applicatica: November 21, 2005 Date Reissued: November 26, 2007 Late o/issuunce: August 18, 2006 Date Amended: 2/21/07; 5/25/07 FEDERAL AVIATION By Direction of the Administrator , (Signanire) Lance T. Gant, Manager TOMNISTRATO Rotorcraft Certification Office, Southwest Region ‹Title)

Page 1 of 3 nce with FAR 21.47.

The FAN will reissue the certificate in the name of the transferee and forward it to him.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number_ to (Name of transferee) (Address of transferee) (Number and street) (City, State, and ZIP code) Iron (Name of grantor) (Print or type) (Address of grantor) (Number & street) (City, State, and ZIP code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SRO9474RC Date of Issuance: August 18, 2006 Date Amended: May 25, 2007 Reissuance Date: November 26, 2007 Certificatien Basis (Continued):

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). (ST2858RC-R Issue Paper A-1, dated 08/10/2006)

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). (ST2858RC-R Issue Paper A-1, dated 08/10/2006) Description of Type Design Change: (Continued):

Installation of a VIP Interior configuration in accordance with Heritage Aviation Ltd.

Master Drawing List S00-13005 Revision E, dated 05/17/2007, or later FAA approved For the S00-13005-01 Split Cabin VIP Interior Configuration:

Rotorcraft Flight Manual Supplement, Heritage Aviation Ltd. Document S09-63001, Revision A, dated 02/20/2007, or later FAA approved revision is required for this installation. Instructions for Continued Airworthiness, Heritage Aviation Ltd.

Document S04-73007, Revision B, dated 01/31/2007, or later revision is required for this installation.

For the S00-13005-03 Full Cabin VIP Interior Configuration:

Rotorcraft Flight Manual Supplement, Heritage Aviation Ltd. Document S09-63002, Revision -, dated 05/25/2007, or later FAA approved revision is required for this installation. Instructions for Continued Airworthiness, Heritage Aviation Ltd.

Document s04-73005, Revision A, dated 05/25/2007, or later revision is required for this installation.

Limitations and Conditions: (Continued):

The four side facing seats are only approved for these interior arrangements.

changes in location will require additional FAA approval. Installation of AAR Manufacturing Group, Inc. Structural Provisions for a Composite Passenger Cabin VIP Interior Composites, STC SR03077AT, is 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 Sikorsky S92A TCDS RO0024BO. Additional FAA approval is necessary to install the final floor covering. 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 the product, the holder must give the other person written evidence of that permission.

PAA Form 8110-2-1 (10-69) Page 3 of 3

## Every issue (2)

- November 26, 2007: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/9c/bf/9cbf08259ddb493b3075653081c1ee302d44fe24a1dcc3ee37d42bf84ca7641a)
- May 25, 2007: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/b1/c3/b1c316675077721004ad9c97965750dac6a97655b9aa259680f50004169fe14a)

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