What it approves
Installation of Airglas model L-2700-369 skis
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
Part 6 of the Civil Air Regulations, dated December 20, 1956, including Amendments 6-1 through 6.4, and Special Conditions
Description of Type Design Change: Installation of Airglas model L-2700-369 skis per Airglas Engineering Company, Inc. drawing L2700-369 (sheet 1 of 1), dated October 3, 1968. The L-2700-369 ski is fabricated per Airglas Engineering Company, Inc. drawings L-2700-369-1 (sheet 1 of 1), dated May 27, 1974, L-2700-369-2, -3, -4, -5 (sheet 1 of 1), dated June 4, 1968 and 30185 (sheet 1 of 1), dated January 20, 1972.
3500 O’Malley Rd Anchorage, AK 99507
H3WE Make : Hughes Model : 369A, 369H, 369HM, 369HS, and 369HE
Date reissued : August 14, 2012
Date amended : June 26, 1974
(Signature) August A. Asay Manager, Anchorage Aircraft Certification Office
(Title) Date of application : February 4, 1970
Date of issuance : February 26, 1970
FAA Form 8110-2-1(10-69) Page 3 of 3
Number SH358AL
This approval applies only to Huges model 369A, 369H, 369HM, 369HS, and 369HE helicopters which are fitted with the Airglas standard gear (Part No. 369A6000 or 369H6000). The approved Airglas Engineering Company, Inc. Rotorcraft Flight Manual Supplement for Hughes 369A, 369H, 369HM, 369HS, and 369HE helicopters, dated June 24, 1974 is a part of this STC and must be included in the Rotorcraft Flight Manual proper when the Airglas model L-2700-369 skis are installed.
The approval of this change in type design applies to Hughes model 369A, 369H, 369HM, 369HS, and 369HE helicopters only. This approval should not be extended to other helicopters of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect on the airworthiness of that helicopter. This determination should include consideration of significant changes in weight distribution such as an increase in the fixed disposable weight in the fuselage.
ADs that name this STC · 0
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