What it approves
Installation of a Micro Systems, Inc. VM1000 Engine Monitoring 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.
FAA Form 8110-2(10-68) Page 1 of 2 Number SA02259AK This Certificate issued to Department Of The Interior Office Of Aircraft Services 4405 Lear Ct.
Anchorage, Alaska 99502-1052
CAR 3 of the Federal Aviation Regulations.
Original Product Type Certificate Number: 1A2
Make: Piper
Model: PA-18 “150”, PA-18S “150”
Description of Type Design Change: Installation of a Micro Systems, Inc. VM1000 Engine Monitoring System in accordance with Office of Aircraft Services Document No. OAS-AKRO 2000-1, Installation Instructions and Instructions for Continued Airworthiness, dated October 3, 2005 or later FAA approved revision.
Limitations and Conditions: Compatibility of this design change with previously approved modifications must be determined by the installer. The approval of this modification is limited to Piper PA-18 “150”, and PA-18S “150”. Aircraft must have an approved installation of the equipped Lycoming 0-320-A2B or modified with an FAA Approved Lycoming O-320-B2B engine. FAA approved Airplane Flight Manual Supplement dated November 9, 2005, or later FAA approved revision is a required part of this approval. For installation instructions and Instructions for Continued Airworthiness, refer to Document Number OAS- AKRO 2000-1, Rev. C, dated October 3, 2005.
Date of application: August 12, 2005
Date of issuance: November 17, 2005 Date reissued:
( Signature) Gregory J. Holt Manager Anchorage Aircraft Certification Office
(Title)
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