What it approves
Installation of higher strength main landing gear drag strut anchor fitting.
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.
$lnttcb of "(Eraitspflrtatum - ^fttatww jAimrimslrattan SA211SW signature Flight Support Corporation, a Delaware Corporation 7511 Lemraon Avenue, Hangar C Dallas, TX 75209 Air 723 Lockheed 18 Installation of higher strength main landing gear drag strut anchor fitting in accordance with HAI Drawing List SA302000-1A dated 3/18/63, or later FAA approved revision. ""
Compliance with repetitive inspections of AD 63-3-3 (a) is not required when this modification has been accomplished.
This STC is part of the basic H250 Tri-Gear configuration.
Compatibility of this modification with other previously approved modifications must be determined by the installer.
.-March 26, 1963 April 02, 1963 ; 12/21/98; 8/31/00 , June 30, 1982 Rev. 8 ice (Signature) S. Fran6es Cox Manager, Special Certification Office, Southwest Region (Title) Any aJteratlon of this certificate Ji punjs/ntja by a fine of not exceeding 11,0119, oz iBprisonaent not exceeding 3 yeses, or Form 8110-ZI10-68) Page 1 of Z TMs certificate wy be tr»nsf»rr«J in accordance with FUR 21. f.
INS I KUC I IONS: 1 he ir.insfcr cnriorsenn ni Mtiv. may be used !o notify ihc- appropriate FAA Regional Office of i he transfer of ihis Supplemental Type Ceriifirair.
The I-'AA will n-issui' thr ccrtificalr in the name of ihe transferee and forward it to him.
TRANSFER ENDORSEMENT Transfer (he ownership of Supplemental Type Certificate Number to (Name of transferee) (A ddress of transferee) VumAfr and street} (C:lj>, Stair, aait ZJP ted') from (Name of grantor) (Print or type) (Address of grantor) (Numl/ei and itrfel} (Cily, Slate, and £IP tode) Extent of Authority (if licensing agreement):
Signature of grantor (In ink):
C FAA AC 69-5536
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 1
| Make | Model | Data sheet |
|---|---|---|
| Lockheed Martin Aeronautics Company | 18 | A-723 |