# STC SR00848SE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Dart Aerospace USA Inc., United States
- Description: Replacement of the original landing gear skid tubes with DART Aerospace Model D315-668-011(LH) and 012(RH) skid tubes fabricated in accordance with DART Aerospace Master Drawing List (MDL) No. MDL-D315-668, Revision C , dated July 6, 2000, or later Federal Aviation Administration (FAA) approved revision and installed
- Applied: September 24, 1999
- Status date: October 17, 2018
- Product: Aircraft
- Certification basis: Part 21, Part 27
- Data sheets: [TCDS H1IN](https://openairdocs.org/tcds/H1IN)
- Certificate PDF: https://openairdocs.org/files/sha256/6f/a4/6fa45ae5235b6af8c70810552ec9caa2b6c41fd82d512f018b03c2777ef28c83
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/01FF3810B6DB0EA48625832E004E8DC9.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR00848SE

## ADs that name it (0)

None.

## Approved models (1)

- Eurocopter France SA.315B Alouette III ([TCDS H1IN](https://openairdocs.org/tcds/H1IN))

## 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.

Un ited S tates of Am erica Department of Transportation - Federal Aviation Administration Supplemental Type Certificate Reissued on October 28, 2015 to supersede the original STC, which has been lost or misplaced Number SR00848SE

This certificate, issued to Dart Aerospace USA, Inc.

3845 NE 30th Avenue Hillsboro, OR 97124

Part 27 of the Federal Aviation Regulations.

Original ProductType Certificate Number: H1IN Make: Eurocopter France Model: SA.315B

Description of the Type Design Change: Replacement of the original landing gear skid tubes with DART Aerospace Model D315-668-011(LH) and -012(RH) skid tubes fabricated in accordance with DART Aerospace Master Drawing List (MDL) No. MDL-D315-668, Revision C, dated July 6, 2000, or later Federal Aviation Administration (FAA) approved revision and installed in accordance with DART Aerospace Installation Instructions No. IIN-D315-668, Revision A, dated September 20, 1999, or later FAA-approved revision. These skid tubes and saddles must be maintained in accordance with DART Aerospace Maintenance Manual Supplement No. MMS-D315-668, Revision A, dated September 13, 1999, or later FAA-approved revision.

Limitations and Conditions: Approval of this change in type design applies to SA 315B rotorcraft only. This approval should not be extended to other rotorcraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that rotorcraft. A copy of this certificate and FAA-approved maintenance manual must be maintained as part of the permanent records of the modified rotorcraf t.

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: September 24, 1999 Date reissued: October 28, 2015; October 17, 2018 Date of issuance: October 10, 2000 Date amended:

(Signature)

Manager, Seattle Aircraft Certification Office (Title)

## Every issue (3)

- October 17, 2018: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/6f/a4/6fa45ae5235b6af8c70810552ec9caa2b6c41fd82d512f018b03c2777ef28c83)
- October 28, 2015: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/ad/8b/ad8b4845a1afcd57fa4378a780140b008fc896de991241054e73b9d3a5d9bf5d)
- October 10, 2000: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/d2/32/d232ea6632fdea439d9b09d27ff3326f69b834e266d550c5941c7c3d986f5df4)

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