STC SA2924NM

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA2924NM This certificate issued to: Power Systems, InC.

Purt 3 of the CiVil Air Regulations* Original Product - Type Certificate Number: A4CE Make: Cessna Model: TU206A, B, C, D, E, F, G and TP206A, B, C, D, E Description of Type Design Change: Installation of the exhaust system of the Continental Model TSIO-520-C engine in accordance with an FAA sealed copy of Frasier/Schauer Drawing No. 1, Sheets 1 through 5, and associated Procedures dated March 15, 1985, or later FAA approved revision.

modelaineard oditionthis approval should not be extended to other aircraft of this Approval of this change in type design applies to the above model on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse 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.

NOTE: No significant change to airplane or engine performance was observed for this FIERBian ShE pting tion Sheet) the lasis fur appreval shull menuin in effect until sur sendered, suspended, newsked, or a termination dale is sherwise is tallished by the SIdminis trater of the Federal Aviation Administration Date of Application: April 25, 1985 Date Reissued:

December 8, 1987 Date of Issuance: May 17, 1985 Jate ununded: June 26, 1992 FEDERAL AVIATION A the Administrater Kо1ї (Signalure ) TOMINIST RANION Manager, Special Certification Branch Seattle Aircraft Certification Office (Title)

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United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA2924NM Limitations and Conditions: (Continued) This approval applies to those airplanes equipped with an exhaust system consisting of the following major components:

PART NUMBERS DESCRIPTION 1250860-110 Tailpipe Assembly 1250860-104 Exhaust Stack Assembly - Front Right 1250860-105 Exhaust Stack Assembly - Turbo Inlet 1250860- 90 Exhaust Stack Assembly - No. 1 Cylinder 1250860-203 Exhaust Stack Assembly - Left Side This modification does not relieve the operator from the inspection requirements of AD 71-09-07.

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