STC SA3238NM

United States of America 8103 Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA3238NM This certificate issued to: AMERICAN PROPELLER SERVICE Redding Municipal Airport Redding, California 96002 Part * of the * Regulations.

Original Product -Iype berlificate Number: * *See attached FAA Approved Model Make: * * List (AML) No. SA3238NM for list of approved airplane models and Model: applicable airworthiness regulations.

Description of Type Design Change: Installation of a McCauley 2A34C203/90DCA-8 Propeller in accordance with American Propeller Service Installation Instructions and Airplane Flight Manual Supplements as listed on Approved Model List (AML) No. SA3238NM, dated February 26, 1993 or later FAA approved revision. This approval supersedes American Propeller Installation Instruction No. AP203-1, dated January 25, 1986, and Supplemental Airplane Flight Manual No. S1, dated March 17, 1986.

Limitations and Conditions: Approval of this change in type design applies to the above model aircraft only. This approval should not be extended to aircraft of these models that incorporate any other previously approved modification unless it is determined that the interrelationship between this change and any other modification will introduce no adverse effect on the airworthiness of these aircraft. (See Continuation Sheet Page 3 for further Limitations and Conditions: ).

Date of Issuance: . January 25, 1986 Jale umended:

EDERAL AVIATION March 17, 1986 ,I6, 1995 Manager Propulsion Branch (Signature ) ADMIN Los Angeles Aircraft Certification Office (Title)

47.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA3238NM Limitations and Conditions: (Continued):

A copy of this Certificate and FAA Approved Model List No. SA3238NM, dated February 26, 1993, or later FAA approved revision, must be maintained as part of the permanent records for the modified aircraft.

The Limitations and Conditions of Aircraft Specification No. 3A13 for models 182, 182A-L apply except as follows:

Propeller: McCauley Constant Speed Propeller 2A34C203/90DCA-8 Propeller Limits: Hub Model 2A34C203 Blade Model Maximum Diameter 82.0 inches Minimum Diameter 80.5 inches Pitch Settings at 30 inch station:

Low pitch 12.5° High Pitch 25.0° Spinner See NOTE 1 Governors Woodward: 210065, 210155, 210345, 210452 McCauley: C290D2/T1, C290D3/T1 Garwin: 34-828-01 (Aircraft models 182E-L only) NOTE 1: Cessna Spinner P/N 0752004 for models 182, 182A-G. Cessna Spinner P/N 0752637 for models 182H-L.

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