# STC SR02341AK

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Vector Aerospace Helicopter Services USA Inc., United States
- Description: Installation of a SAGEM integrated cockpit display system and Crossbow attitude and heading reference system
- Applied: September 25, 2008
- Status date: January 21, 2011
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21, Part 27
- Data sheets: [TCDS H11EU](https://openairdocs.org/tcds/H11EU)
- Certificate PDF: https://openairdocs.org/files/sha256/2b/c8/2bc8ae0e33f50a1156dfb27deb8d4a9ede989a3929c5166eb19b2c1464ac6207
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C117718D43DAF2088625782500574C87.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR02341AK

## ADs that name it (0)

None.

## Approved models (2)

- Eurocopter France AS355F1 ([TCDS H11EU](https://openairdocs.org/tcds/H11EU))
- Eurocopter France AS355F2 ([TCDS H11EU](https://openairdocs.org/tcds/H11EU))

## 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.

This certificate issued to Vector Aerospace Helicopter Services USA Inc.

1873 Shell Simmons Drive, Suite 110 Juneau, AK 99801

Part 27 of the Federal Aviation Regulations.

Original Product — Type Certificate Number: H11EU Make: Eurocopter France Model : AS355F1, AS355F2

Description of Type Design Change: Installation of a SAGEM integrated cockpit display system and Crossbow attitude and heading reference system in accordance with Vector Aerospace Helicopter Services USA, Inc., Master Drawing List, HP 355-34-33-102, Rev. C, dated January 21, 2011, or later FAA approved revision.

1) The following Supplemental Type Certificates (STC) are required as part of this modification; Heli-Lynx Helicopter Services, Inc. STC’s SR02015NY, SR02281NY, and SR02082NY.

2) Rotorcraft Flight Manual Supplement, Doc. No. FMS HP 355-34-33-302, Rev. A, dated January 21, 2011, or later FAA approved revision is a required part of this installation.

3) A rotorcraft modified in accordance with this STC is limited to VFR flight only.

(Limitations and Conditions continued on page 3 of 3)

Date of application: September 25, 2008 Date reissued:

Date of issuance: May 12, 2009 Date amended: January 21, 2011

( Signature) August A. Asay Manager, Anchorage Aircraft Certification Office

( Title)

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

Number SR02341AK Limitations and Conditions: (continued)

4) Instructions for Continued Airworthiness, Vector Aerospace Helicopter Services USA, Inc., Doc. No. HP 355-34-33-251, Rev. Reissue, dated August 9, 2010, or later FAA accepted revisions are a required part of this modification.

5) 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.

6) The installer must determine whether this design change is compatible with previously approved modifications.

7) The Certification Basis for this modification is:

 The original certification basis as found on Type Certificate Data Sheet (TCDS) number H11EU.

 Additionally, 14 Code of Federal Regulations, Part 27 effective February 1, 1965, as amended by 27.610 amdt. 27-21; 27.1305(c), (d), (f), (g), (h), (i), (j), (k), (l), (n), (o), (p) amdt. 27-37; 27.1309(a), (b), (d) amdt. 27-21; 27.1317(a),(4), (b), (c) [Aug 6, 2007];

27.1365 amdt. 27-35; 27.1555(a) amdt. 27-21.

## Every issue (2)

- January 21, 2011: Amended, Current. [certificate](https://openairdocs.org/files/sha256/2b/c8/2bc8ae0e33f50a1156dfb27deb8d4a9ede989a3929c5166eb19b2c1464ac6207)
- May 12, 2009: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/2b/aa/2baa5d1544944cd3fb5748cb9073b40739e7fa816adf80d5f0eae94d1ab0c1e9)

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