What it approves
Installation of Airglas Engineering Model L2700AS350 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 21.29 and 27 of the Federal Aviation Regulationx plus Amendments 27-1 through 27-16.
Description of Type Design Change: Installation of Airglas Engineering Company, Inc., Model L2700AS350 skis per Revision B of Airglas drawing L2700AS350, Sheet 1 of 1, dated April 16, 1982. The L2700AS350 skis are fabricated per the following Airglas Engineering Company, Inc., Drawings: Revision “A” of L2700AS-350-1, Sheet 1 of 1, dated May 19, 1982;
Revision “A” of L2700AS350-2, -3, Sheet 1 of 1, dated May 20, 1982; Revision “A” of L2700SA341-6, -7, Sheet 1 of 1, dated October 13, 1980; and 30185, Sheet 1 of 1, dated January 20, 1972.
See continuation page 3 of 3
3500 O’Malley Rd Anchorage, AK 99507
H11EU Make: Societe Nationale Industrielle Aerospatiale Model: AS355E and AS355F
Date reissued : August 14, 2012
(Signature) August A. Asay Manager, Anchorage Aircraft Certification Office
(Title) Date of application : April 20, 1982
Date of issuance : May 25, 1982
FAA Form 8110-2-1(10-69) Page 3 of 3
Number SH730AL
This approval applies only to those Societe Nationale Industrielle Aerospatiale Model AS355E and AS355F helicopters which are fitted with the standard landing gear or the high skid landing gear. The FAA Approved Airglas Engineering Company Rotorcraft Flight Manual Supplement for the Model AS355E, dated May 25, 1982, or the Model AS355F helicopter, dated May 25, 1982 is a part of this STC and must be included in the basic Rotorcraft Flight Manual when the helicopter is operated with the Airglas Model L2700AS350 skis installed.
The approval of this change in type design applies basically to Societe Nationale Industrielle Aerospatiale Model AS355E and AS355F helicopters only. This approval should not be extended to other helicopters of this model on which other previously 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 affect on the airworthiness of that helicopter.
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