STC SR01179SE

Supplemental type certificate · Winco Inc.

Holder
Winco Inc. · United States
Status
Current · Amended
Status date
June 29, 2009
Applied
February 28, 2000
Product
Aircraft · Rotorcraft
Certification basis
Part 21, Part 27
Data sheet
TCDSH3WE

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

What it approves

Fabrication of the Winco Side Pull Handle Assembly per Drawing No. W002, Revision N/C, dated December 13, 2002, or later FAA-approved revision, and the Hook Link Assembly, Part No. 369SP-200, per Colorado Helicopters Drawing No. 369SP-200, Revision C, dated September 11, 1991, or later FAA-approved revision; and installation and maintenance of this system

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.

Number SR01179SE This certificate, issued to Winco, Inc.

22300 NE Yellow Gate Lane Aurora, OR 97002 Part 27 of the Federal Aviation Regulations.

Original Product⎯Type Certificate Number: H3WE Make: MDHI Model: 369D, 369E, 369F, 369FF, 500N, 600N

Description of the Type Design Change: Fabrication of the Winco Side Pull Handle Assembly per Drawing No.

W002, Revision N/C, dated December 13, 2002, or later FAA-approved revision, and the Hook Link Assembly, Part No. 369SP-200, per Colorado Helicopters Drawing No. 369SP-200, Revision C, dated September 11, 1991, or later FAA-approved revision; and installation and maintenance of this system in accordance with Winco Installation and Continued Airworthiness Manual SPH-CAM, Revision 1, dated June 10, 2009, and Winco, Inc.

Continued Airworthiness Manual No. 980518, Revision 2, dated January 6, 2003, or later FAA-approved revision.

Limitations and Conditions: Approval of this change in type design applies to the above listed 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 interrelationship between this change and any other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that rotorcraft. Rotorcraft modified in accordance with this STC must be operated in accordance with a copy of the FAA-approved Rotorcraft Flight Manual Supplement (RFMS) SPH- RFM, Revision 1, signed June 11, 2009, or later FAA-approved revision. A copy of this Certificate, FAA-approved RFMS, Installation and Continued Airworthiness Manual, and Winco, Inc. Continued Airworthiness Manual No.

980518 must be maintained as part of the permanent record of 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.

This certificate and the supporting data which is the ba sis for approval shall remain in effect until surrendered, suspended, revoked, or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.

Date of application: February 28, 2000 Date reissued:

Date of issuance: February 20, 2003 Date amended: June 29, 2009

(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 · 5

MakeModelData sheet
MD Helicopter Inc.369DH3WE
MD Helicopter Inc.369EH3WE
MD Helicopter Inc.369FH3WE
MD Helicopter Inc.369FFH3WE
MD Helicopter Inc.500NH3WE