What it approves
Installation of a Shadin Co. 911218 temperature compensated fuel flow indicating 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.
Part 3 of the Civil Air Regulations.
(See Type Certificate Data Sheet No. A8EA for complete certification basis.)
Installation of a Shadin Company 911218 Temperature Compensate d Fuel Flow Indicating System in accordance with Shadin Company Report number 4041, dated March 8, 1982, or subsequent FAA approved revision.
1) FAA Approved Airplane Flight Manual Supplement dated June 18, 1982, or subsequent FAA approved revision is required. This approval should not be extended to other airplanes of this model that incorporate any other previously approved modification, unless it is determined that the interrelationship between this change and any other previously approved modification will introduce no adverse effect on the airworthiness of these airplanes.
2) If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.
Shadin Avionics 6831 Oxford Street St. Louis Park, MN 55426 A8EA Make : Piper Aircraft Corporation Model : PA-31T, PA-31T1, PA-31T2
Date of application : March 8, 1982
Date of issuance : June 18, 1982
Date reissued : June 8, 2006
( Signature) Charles L. Smalley Manager, Systems & Flight Test Branch Chicago Aircraft Certification Office
( Title)
ADs that name this STC · 0
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