# STC SR09259RC

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Metro Aviation Inc, United States
- Description: Installation of Single Pilot IFR Avionics
- Applied: February 20, 2000
- Status date: January 3, 2013
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21, Part 27
- Data sheets: [TCDS H88EU](https://openairdocs.org/tcds/H88EU)
- Certificate PDF: https://openairdocs.org/files/sha256/69/32/6932f086cba42a86bc982d0e7592e631f02241ad1745150eb18fc58b9be2a28c
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/990BE364AAE8166686257B8600472DF6.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SR09259RC

## ADs that name it (0)

None.

## Approved models (1)

- Eurocopter Deutschland GmbH EC135 ([TCDS H88EU](https://openairdocs.org/tcds/H88EU))

## 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.

1214 Hawn Avenue Shreveport, LA 71107 Part 27 of the Federal Aviation Regulations.

Original Product – Type Certificate Number : H88EU Make: Eurocopter Deutschland GmbH Model: EC135 P1, P2, P2+, T1, T2, T2+ Description of Type Design Change: Installation of Single Pilot IFR Avionics in accordance with Metro Aviation, Inc. Master Drawing List MDL 135M-150, Revision M, dated 18 December 2012, or later Federal Aviation Administration (FAA) approved revision.

Limitations and Conditions : Rotorcraft Flight Manual Supplement (RFMS) FMS135M-150 Revision E, dated March 15, 2007 or later FAA approved RFMS is required for Kit 135M-150-1/-3. Rotorcraft Flight Manual Supplement (RFMS) FMS135M-150-1 Revision IR, dated May 05, 2008 or later FAA approved RFMS is required for Kit 135M-150-4,-5 & -6. Rotorcraft Flight Manual Supplement (RFMS) FMS135M-150002 Revision IR, dated December 17, 2012 or later FAA approved RFMS is required for Kit 135M-150-7/-8. Metro Aviation, Inc. Document SW135M-150001, Rev. A, dated December 5, 2012, or later FAA approved revision, defines the software configuration for Kit 135M-150-4 through -8. Instructions for Continued Airworthiness Rev. A, dated August 10, 2001, or later FAA accepted revision is required for Kit 135M-150-1/-3.

Date of application: February 20, 2000 Date reissued: December 20, 2007, January 3, 2013 Date of issuance: December 29, 2000 Date amended: March 22, 2005, March 15, 2007, May 5, 2008, December 19, 2012

(Signature) Scott A. Horn, Acting Manager Rotorcraft Certification Office Southwest Region

(Title)

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

Number SR09259RC Date of Issuance: December 29, 2000 Date Amended: December 19, 2012 Date of Reissuance: January 3, 2013

Limitations and Conditions: Cont ’d.

Instructions for Continued Airworthiness, EMM135M-150-1, Rev. A, dated November 15, 2012, or later FAA accepted revision is required for Kit 135M-150-4 through -8. The installer must determine whether this design change is compatible with previously approved modifications. A copy of this certificate must be maintained as part of the permanent records for the modified aircraft. 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.

ECD Battery Kit Number L243M3815052 or American Eurocopter LLC Supplemental Type Certificate SR09105RC-D with RG-380/44 is required with Kit 135M-150-4/-5/-6/- 7/-8.

## Every issue (2)

- January 3, 2013: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/69/32/6932f086cba42a86bc982d0e7592e631f02241ad1745150eb18fc58b9be2a28c)
- March 22, 2005: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/7f/a3/7fa3526e55bc4651314fa4c2db911742303d8da64e5441df0ae7bb9c7b51eee6)

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