STC SH207WE

Supplemental type certificate · ROBERTSON FUEL SYSTEMS LLC

Holder
ROBERTSON FUEL SYSTEMS LLC · United States
Status
Current · Reissued
Status date
July 19, 2011
Applied
November 20, 1977
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 6, 2025.

What it approves

Installation of range extension fuel tank in cargo area.

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.

This Certificate issued to ROBERTSON FUEL SYSTEMS LLC 800 West Carver Road, Suite 101 Tempe, Arizona 85281 Part 6 of the Civil Air Regulations, dated October 8, 1963, including Amendments 6-1 through 6-7 and parts of 14 CFR part 27 (see TCDS for specific applications).

H3WE

Boeing (McDonnell Douglas Helicopter Systems) 369, 369A, 369H, 369HM, 369HS, 369HE, 369D, 369E, 369F, 369FF, 500N, 600N Description of Type Design Change: Installation of a range extension fuel tank in the cargo area of Boeing (McDonnell Douglas Helicopter System s) 369 series, 500N, and 600N model helicopters in accordance with Robertson Aviation, FAA Approved Master Drawing List MDL-HA-010, dated January 9, 1978, or later FAA approved revision. FAA Approved Robertson Aviati on Rotorcraft Flight Manual Supplement RA-010-369/500- RFM, dated January 10, 1978, or later FAA approved revision is required as part of the installation for the 369 series and 500N models. FAA Approved Robertson Aviation Ro torcraft Flight Manual Supplement RA-010-600N-RFM, dated September 18, 1998, or later FAA approved revision is required as part of the installation for the 600N model.

Limitations and Conditions : The approval of this change in the type design applies to the above aircraft model(s) only. This approval should not be extended to ai rcraft of this model on which other previously approved modifications are incorporated unless it is determined that the interrelationship 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 aircraft. A copy of this STC mu st be included in the perman ent records of each aircraft modified in accordance with this STC. If the holder agrees to permit anot her 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 20, 1977

Date of issuance : January 10, 1978

Date reissued : June 19, 2000; July 3, 2002;

July 7, 2003; June 28, 2006; July 19, 2011

Date amended : February 1, 1985, March 24, 1987, October 23, 1992, September 30, 1998

( Signature) Haifa Haj-Eid Supervisor, Technical & Administrative Support Staff, Los Angeles Aircraft Certification Office ( l )

NOTE:

DO NOT DELETE THIS PAGE.

DO NOT ADD ANY DATA TO THIS PAGE.

THIS PAGE IS FOR PAGE NUMBERING PURPOSES, PLEASE DISCARD PRINTED COPY.

Number (STC No.)

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 · 12

MakeModelData sheet
MD Helicopter Inc.369H3WE
MD Helicopter Inc.369AH3WE
MD Helicopter Inc.369DH3WE
MD Helicopter Inc.369EH3WE
MD Helicopter Inc.369FH3WE
MD Helicopter Inc.369FFH3WE
MD Helicopter Inc.369HH3WE
MD Helicopter Inc.369HEH3WE
MD Helicopter Inc.369HMH3WE
MD Helicopter Inc.369HSH3WE
MD Helicopter Inc.500NH3WE
MD Helicopter Inc.600NH3WE

Every issue · 2

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

DateStatusFiles
July 19, 2011Reissued, currentCertificate
June 28, 2006Reissued, earlier issueCertificate