# STC SR03077AT

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: AAR Composites, USA
- Description: Structural Provisions for a Composite Passenger Cabin VIP Interior
- Applied: November 25, 2003
- Status date: February 28, 2008
- Product: Aircraft, Rotorcraft
- Certification basis: Part 29
- Data sheets: [TCDS R00024BO](https://openairdocs.org/tcds/R00024BO)
- Certificate PDF: https://openairdocs.org/files/sha256/c4/1c/c41c543c2b371803bf6eea64ec483d0a826b1c0918f0d1770edcca094c3cbdcd
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID140310710020231013185724.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SR03077AT

## 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: SR0307TAT This certificate issued to: AAR Composites 14201 Myerlake Circle Clearwater, FL 33760 Part 29 c/the 14. Poegulutions.

Original Product - - Type Certificula Number: R00024BO Make: Sikorsky Model: S-92A Description of Type Design Change: Structural Provisions for a Composite Passenger Cabin VIP Interior in accordance with Master Document List (MDL) S92-620-011 Rev L dated February 22nd, 2008 or later FAA approved revision.

Limitaticas and Conelilions: Apply Instructions for Continuing Airworthiness AAR-ER-1116 Rev E, dated January 25th, 2008 or later FAA approved revision for maintenance and inspections. MDL items under this STC meet 29.853. The installer is responsible for the addition of decorative finish to continue to comply with

29.853. AAR Bulkheads are for interior partitions only and are not the intended means of compliance for cargo or smoke retention that the installer must ensure is covered by other FAA design approvals. The installer is responsible for systems and structural provisions for monitors that may weigh up to 7 pounds.

Weight and Balance is in accordance with AAR-ER-1264 Rev IR, dated February 21" , 2008 or later FAA approved revision. The installer is responsible for the compatibility of this STC with other previously approved modifications incorporated in the aircraft and must determine that the interrelationship between this change and any of those other previously approved modifications will produce no adverse effect upon the airworthiness of the aircraft. If the installer 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.

Dale of uppliculion: November 25"h , 2003 Dele of issuence: March 31st, 2005 Lute reissueel :

Bale umended: May 8", 2006, February 28", 2008 By Direction of the Administrator

EDERAL AVIATION (Signature) Melvin Taylor TOMINISTRATO FAA Atlanta Aircraft Certification Office Manager (Jutle) by a fine of not exceeding $1,000, oz imprisonment noc exceeding 3 pears, or bath.

**FAA FORY 8110-2(10-69) PAGES**

## Every issue (1)

- February 28, 2008: Amended, Current. [certificate](https://openairdocs.org/files/sha256/c4/1c/c41c543c2b371803bf6eea64ec483d0a826b1c0918f0d1770edcca094c3cbdcd)

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