What it approves
Installation of Shadin Company 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 23 of the Federal Aviation Regulations. (See Type Certificate Data Sheet No. A23CE for complete certification basis.)
Installation of a Shadin Company Fuel Flow Indicating System in accordance with Shadin Company Report Number 4024, revised March 3 1986, or other FAA approved revision.
1) If original Analog Fuel Flow Indicator is removed, FAA Approved Airplane Flight Manual Supplement dated June 12, 1986 is required.
2) The approval of this change in type design applies to the basic Beech Model 58P, 58PA, 58TC, and 58TCA airplanes which are otherwise unmodified. 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.
Shadin Avionics 6831 Oxford Street St. Louis Park, MN 55426 A23CE Make : Beech Model : 58P, 58PA, 58TC, and 58TCA (Serial Nos. TJ-3 and up, TK-1 and up) Date of application : September 5, 1980
Date of issuance : February 12, 1981
Date reissued : June 8, 2006
Date amended : January 26, 1982, December 16, 1982, June 12, 1986
( Signature) Charles L. Smalley Manager, Systems and Flight Test Branch Chicago Aircraft Certification Office
( Title)
FAA FORM 8110-2-1(10-69) PAGE 2 of 2 PAGES
Number SA501GL
Date of issuance : June 8, 2006
3) 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.
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