# STC SR09415RC

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Erickson Air Crane Inc. dba Erickson Air-Crane, United States
- Description: Installation of Engine Monitoring System and Fuel Indication with multifunction displays (MFD-5200).
- Applied: December 17, 2003
- Status date: May 7, 2012
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21, Part 29
- Data sheets: [TCDS H6EA](https://openairdocs.org/tcds/H6EA)
- Certificate PDF: https://openairdocs.org/files/sha256/e8/6b/e86bd6381a7aa92bb71db6aae237dc1bfb807c16a9e9744d87eb3ff5de54f926
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/490D676706F085B4862579F800570172.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SR09415RC

## ADs that name it (0)

None.

## Approved models (1)

- Erickson Air-Crane Company S-64F ([TCDS H6EA](https://openairdocs.org/tcds/H6EA))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

Number SR09415RC This certificate issued to Erickson Air-Crane Incorporated 3100 Willow Springs Road Central Point, OR 97502-9362

Part 29 of the Federal Aviation Regulations. See continuation sheet 3 of 3 for additional requirements.

Original Product -- Type Certificate Number : H6EA Erickson Make :

S-64F

Description of Type Design Change: Installation of Engine Monitoring System and Fuel Indication with multifunction displays (MFD-5200) in accordance with Heritage Aviation, LTD., Master Drawing List R00-12000, Revision A, dated July 25, 2004, or later Federal Aviation Administration (FAA) approved revision(s).

Limitations and Conditions: Rotorcraft Flight Manual Supplement (RFMS) R09-62000, Revision IR, dated July 26, 2004, or later FAA approved RFMS is required. Instructions for Continued Airworthiness, Heritage Aviation, LTD., Document R08-72000, Revision IR, dated July 21, 2004, or later FAA accepted revision is required for this installation.

Date of application : December 17, 2003

Date of issuance : July 27, 2004 Date reissued :

( Signature) Carl F. Mittag, Manager Rotorcraft Certification Office Southwest Region

(Title)

FAA Form 8110-2-1(10-69) Page 2 of 2

Number SR09415RC Date of Issuance: July 27, 2004

Certification Basis of this change is as follows:

FAR Part 29, dated 1 February 1965, including Amendment 29-1 and 29-2, except section

29.855(d) and Special Condition No 29-6-EA-2, also compliance has been found specifically to sections;

29.853(a)-(b) and 29.1305 (a)(3), (a)(4), (a)(6), (a)(8) – (a)(15), (c)(1) and

(c)(2) at Amendment 29-3

29.1322 at Amendment 29-12

29.1353(a)-(b) at Amendment 29-15

29.1321 at Amendment 29-21

29.771(a)-(c), 29.1355, 29.1357(a), (c), (d), and (e), 29.1583(b), and (e) at Amendment 29-24

29.1163(a)-(b), and (c)(1), and 29.1337(b)-(c) at Amendment 29-26

29.1529 at Amendment 29-20, and Appendix A to Part 29, Sections A29.1, A29.2, and A29.3 at Amendment 29-27

29.1549 at Amendment 29-34

29.901(a)-(c) and 29.903(d)(2) at Amendment 29-36

29.1309(a), (b)(1), (c) and (g) at Amendment 29-40

29.1359(b)-(c) at Amendment 29-42

Compatibility of this design with previously approved modifications must be determined by the installer.

Installation of STCs SR09411RC, SR09412RC, SR09413RC, SR09414RC, and SR09416RC is required.

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.

## Every issue (2)

- May 7, 2012: Amended, Current. [certificate](https://openairdocs.org/files/sha256/e8/6b/e86bd6381a7aa92bb71db6aae237dc1bfb807c16a9e9744d87eb3ff5de54f926)
- July 27, 2004: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/e8/6b/e86bd6381a7aa92bb71db6aae237dc1bfb807c16a9e9744d87eb3ff5de54f926)

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