STC SA00475SE

Supplemental type certificate · Dart Aerospace USA Inc.

Holder
Dart Aerospace USA Inc. · United States
Status
Current · Reissued
Status date
October 17, 2018
Applied
April 22, 1997
Product
Aircraft · Rotorcraft
Certification basis
Part 21, Part 27
Data sheet
TCDSH2SW

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Replacement of the original land gear skid tubes and saddles with DART Aerospace Model D206-642 skid tubes and saddles.

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.

Un ited S tates of Am erica Department of Transportation - Federal Aviation Administration Supplemental Type Certificate

Number SA00475SE

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: H2SW Make: Bell Model: 206, 206A, 206A-1, 206B, 206B-1, 206L, 206L-1, 206L-3, 206L-4, and 407

Description of the Type Design Change: Replacement of the original landing gear skid tubes and saddles with DART Aerospace Model D206-642 skid tubes and saddles fabricated in accordance with DART Aerospace Master Drawing List No. MDL-D206-642, Revision Q, dated March 8, 2007, or later Federal Aviation Administration (FAA) approved revision, and installed in accordance with DART Aerospace Installation Instructions No. D206-642, Revision K, dated September 25, 2006, or later FAA-approved revision. These skid tubes and saddles must be maintained in accordance with DART Aerospace Instructions for Continued Airworthiness ICA-D206-642, Revision 0, dated March 7, 2007, or later FAA-accepted revision.

Limitations and Conditions: Approval of this change in type design applies to the above model rotorcraft only.

This approval should not be extended to other rotorcraft of these models on which other previously approved modifications are incorporated unless it is determined by the installer that the relationship between this change and any previously approved modifications, including changes in type design, will intro duce no adverse effect upon the airworthiness of that rotorcraft. A copy of this certificate must be maintained as part of the permanent records for the modified rotorcraft.

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: April 22, 1997 Date reissued: October 28, 2015; October 17, 2018 Date of issuance: October 23, 1997 Date amended: April 20, 2007

(Signature)

Manager, Seattle Aircraft Certification Office (Title)

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 10

MakeModelData sheet
Bell Helicopter Textron Canada Limited206H2SW
Bell Helicopter Textron Canada Limited206AH2SW
Bell Helicopter Textron Canada Limited206A-1 (OH-58A)H2SW
Bell Helicopter Textron Canada Limited206BH2SW
Bell Helicopter Textron Canada Limited206B-1H2SW
Bell Helicopter Textron Canada Limited206LH2SW
Bell Helicopter Textron Canada Limited206L-1H2SW
Bell Helicopter Textron Canada Limited206L-3H2SW
Bell Helicopter Textron Canada Limited206L-4H2SW
Bell Helicopter Textron Canada Limited407H2SW

Every issue · 4

DRS keeps each issue of an STC as its own record, with its own certificate and attachments.

DateStatusFiles
October 17, 2018Reissued, currentCertificate
October 28, 2015Reissued, earlier issueCertificate
April 20, 2007Amended, earlier issueCertificate
April 9, 2007Amended, earlier issueCertificate