STC SA00077LA

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 1 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

(See Continuation Sheet Page 3 of 3 Pages) SA00077LA Aerospace Welding Minneapolis, Inc.

3344 Highway 149 Eagan, MN 55121 Part 21 Federal Aviation Regulations A9CE Cessna 188, 188A, 188B, A188, A188A, A188B Installation of a modified exhaust system in accordance with Knisley Welding, Inc. Master Drawing List (MDL) #2, Revision D, dated January 15, 1997, or later FAA Approved revision, and FAA Approved Supplemental Airplane Flight Manual (AFM), AFM/POH Supplement, Document No. 188, dated January 22, 1997, or later FAA Approved revision.

*NOTE: STC SA00077LA supersedes STC SA00079LA issued to Knisley Welding, Inc.

Approval of this change in type design applies to the above aircraft model(s) only. This approval should not be extended to aircraft of this model on which other previously approved modifications are incorporated unless it is determined that the interrelationship between this change and any of those other previously approved modifications will introduce no advese effect upon the airworthiness of that aircraft. A copy of this Certificate must be maintained as part of the permanent records for the modified aircraft.

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.

September 22, 1994 November 17, 2023 April 27, 1995 January 23, 1997* for Manager, West Certification Branch 3

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 2 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

SA00077LA 3

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page ___ of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number:

End SA00077LA Limitations and Conditions (Continued):

NOTE 1: This modification is limited to aircraft models certificated in the Restricted Category only.

NOTE 2: Noise characteristics: This modification is not considered an "acoustical change" as defined in § 21.93(b)(3)(i), Amendment 21-73 of the Federal Aviation Regulations.