STC SA00797CH

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA00197CH This certificate issued to: McCauley Propeller Systems 7751 East Pawnee Wichita, KS 67207 Certifies that the change in the type design for the following product with the limitations and conditions therefor as specified hereon meet's the airvorthiness requirement's of Part 3 of the Civil Air Roegulations.

See Type Certificate Data Sheet No. 3A13 for complete certification basis.

Original Product - Type Certificate Number: 3A13 Make: Cessna Model: R182 Description of Type Design Change:

Installation of McCauley Propeller Model B3D36C431/80VSA-1 or B3D36C433/80VSA-1, and spinner assembly in accordance with McCauley Technical Report No. 873, no revision, dated June 26, 1997, and McCauley Drawing No. D-60202, no revision, dated July 10, 1997, or later FAA approved revisions.

1. Compatibility of this design change with previously approved modifications must be determined by the installer.

Date of Application: June 27, 1997 Date Reissued: September 21, 2005 Date of Issuance: November 25, 1997 Date Amended:

FEDERAL AVIATION (Signature) Thaddeus D. Krolicki, Jr.

TOMNISTRATOR Manager, Propulsion Branch Chicago Aircraft Certification Office (Title)

FAR FORM 8110-2 (10-68) PAGE 1 of 3 PAGES

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number S5A00797CH Date of Issuance: November 25, 1997 Reissued: September 21, 2005 Limitations and Conditions: (Continued):

2. FAA Approved Flight Manual Supplement, Technical Report Number 874, dated August 4, 1997, or later FAA approved revisions, is required.

3. Lycoming engine model O-540-J3C5D is eligible with the McCauley Propeller Model B3D36C433/80VSA-1 (S/N R18200001 through R18201313) with a maximum continuous and takeoff rating of 235 HP and 2400 RPM.

4. Lycoming engine model O-540-J3C5D is eligible with the McCauley Propeller Model B3D36C431/80VSA-1 (S/N R18201314 and up) with a maximum continuous and takeoff rating of 235 HP and 2400 RPM.

5. Aircraft Specifications are the same as listed on Type Certificate Data Sheet No. 3A13 except as listed in McCauley Technical Report Number 874.

6. 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.

..End...

FAR FORM 8110-2-1(10-69) PAGE 3 of 3 PAGES