STC SR00790SE

Supplemental type certificate · Simplex Manufacturing Company

Holder
Simplex Manufacturing Company · United States
Status
Current · Issued
Status date
March 29, 2000
Applied
November 30, 1999
Product
Aircraft
Certification basis
Part 21
Data sheet
TCDSH2SW

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Fabrication of Simplex Model 918 adjustable mirror system in accordance with Simplex Master Drawing List No. MDL 918, dated January 10, 2000, or later Federal Aviation Administration (FAA) approved revision; and installation of this system in accordance with Installation Document No. 918-102 002-001, dated December 28, 1999, or later FAA approved revision. This modification must be maintained in accordance with Simplex Maintenance Manual Supplement, Document No. 918-102 005-001, dated December 30, 1999, or later FAA approved revision.

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.

United States of America Department of Transportation_Federal Aviation Administration Supplemental Type Certificate Number SR00790SE

This certificate, issued to Simplex Manufacturing Company 13340 NE. Whitaker Way Portland, OR 97230 Part 6 of the Civil Air 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: Fabrication of Simplex Model 918 adjustable mirror system in accordance with Simplex Master Drawing List No. MDL 918, dated January 10, 2000, or later Federal Aviation Administration (FAA) approved revision; and installation of this system in accordance with Installation Document No. 918-102 002-001, dated December 28, 1999, or later FAA approved revision. This modification must be maintained in accordance with Simplex Maintenance Manual Supplement, Document No. 918-102 005-001, dated December 30, 1999, or later FAA approved revision.

Limitations and Conditions: Approval of this change in type design applies to the Bell model rotorcraft listed above. This approval should not be extended to other rotorcraft of these models on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that helicopter.

Rotorcraft modified in accordance with this STC must be operated in accordance with an FAA approved copy of the Rotorcraft Flight Manual Supplement (RFMS), Simplex Document No. 918-102 003-002, dated March 29, 2000, or later FAA approved revision. A copy of this Certificate, Maintenance Manual Supplement and FAA approved RFMS must be maintained as part of the permanent records of the modified helicopter.

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: November 30, 1999 Date reissued:

Date of issuance: March 29, 2000 Date amended:

(Signature) Acting 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