What it approves
Installation of a replacement auxiliary fuel pump.
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.
Description of Type Design Change: Installation of a replacement auxiliary fuel pump in accordance with CJ Aviation Drawing No. 210-2801 Rev. C, dated July 21, 1995 and Drawing No. 210-2800 Rev. B, dated July 21, 1995 or later FAA approved revision of either document.
Limitations and Conditions: "This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated, unless it is determined by the installer that the interrelationship between this chang e and any other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane. 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."
C J Aviation, Inc.
12215 SW 131 Ave.
Miami, FL 33186 3A21 Make : Cessna Model : 210D thru 210N; T210F through T210N
Date of application : September 09, 1994
Date of issuance : February 27, 1995
Date reissued : March 11, 2010
Date amended : August 24, 1995
( Signature) Melvin D. Taylor Manager Atlanta Aircraft Certification Office
( Title)
FAA FORM 8110-2-1(10-69) PAGE 2 of 2 PAGES
Number
Comment [RL1]: Page: 1
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 18
| Make | Model | Data sheet |
|---|---|---|
| Cessna Aircraft Company | 210D | 3A21 |
| Cessna Aircraft Company | 210E | 3A21 |
| Cessna Aircraft Company | 210F | 3A21 |