# STC SR09630RC

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: PHI Inc, United States
- Description: Installation of Emergency Medical System (EMS) Interior with a dual or single litter configurations
- Applied: October 4, 2012
- Status date: November 2, 2012
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21, Part 29
- Data sheets: [TCDS H4SW](https://openairdocs.org/tcds/H4SW)
- Certificate PDF: https://openairdocs.org/files/sha256/e6/27/e6270674f4982e90cb301d5c556bb08a627d473d00fa6d9c9fd7c37bf5e080f1
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C8B1ED8EA43A6A69862585AF005DF6D5.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR09630RC

## ADs that name it (0)

None.

## Approved models (1)

- Bell Textron Inc. 412EP ([TCDS H4SW](https://openairdocs.org/tcds/H4SW))

## What the certificate says

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

PN: ST03476RC-R PE: MC ASW-170 United States of America O:IWPISTCIPHI STC DocsISR09630RC.doc Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SR09630RC This certificate issued to: PhI, inc.

2001 SE Evangeline Thruway Lafayette, LA 70508-2156 Part 29 of the Frederal Aviation Pegulations, *Iee Page 3 of 3 Original Product - Type Certificate Number : H4SW Make: Bell Helicopter Textron Model: 412EP Description of Type Design Change: Installation of Emergency Medical System (EMS) Interior with a dual or single litter configurations in accordance with Master Drawing and Document List No. PHI412-DL-0017, Rev. (1), dated October 31, 2012. Rotorcraft Flight Manual Supplement No. PHI-412-RFMS-0005, Rev. (0), dated October 25, 2012 or later FAA approved revision is required. Instructions for Continued Airworthiness No. PHI412-ICA-0013, Rev. (IR), dated September 25, 2012, or later FAA accepted revision is required.

Limitations and Conditions: This installation requires the incorporation of STCS SRO2075LA, SRO1082LA, and SR00871LA. 1) Compatibility of this design change with previously approved modifications must be determined by the installer. 2) A copy of this certificate must be maintained as part of the permanent records for the modified aircraft.

3) If the holder 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.

Date of Application: 10/04/2012 Date Reissued:

Date of Issuance: 11/02/2012 Date Amended:

By Direction of the Administrator FEDERAL AVIA TON (Signature) Scott A. Horn, Acting Manager Rotorcraft Certification Office TOMNISTRATO Southwest Region (Title)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SR09630RC Date of Issuance: 11-02-2012 Certification Basis: The certification basis for this modification is as shown on TCDS HASW for the Model 412EP plus 14 CFR § 29.853 at Amendment 29-17.

FAA FORM 8110-2-1(10-69) PAGE 3 of 3 PAGES

## Every issue (1)

- November 2, 2012: Issued, Current. [certificate](https://openairdocs.org/files/sha256/e6/27/e6270674f4982e90cb301d5c556bb08a627d473d00fa6d9c9fd7c37bf5e080f1)

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