STC SA00718CH

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number 5A00718CH 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 meets the airoorthiness requirement's of Part 3 of the Civil Air Poegulations.

Sce Type Certificate Data Sheet Number 3A15 for complete certification basis.

Original Product Type Certificate Number: 3A15 Make: Beech Model:

35-33; 35-A33; 35-B33; 35-C33;

E33; F33; G33;

J35; K35; M35; N35; P35 Description of Type Design Change:

Installation of McCauley Propeller Model 3A36C434/80VEA-0 in accordance with McCauley Technical Report (TR) 888, no revision, dated May 29, 1997, and Installation of McCauley Governor Model C290D3/T35 in accordance with McCauley Technical Report No. TR 889, no revision, dated June 2, 1997, and McCauley Drawing No. D-60220, 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.

2. This modification did not increase the noise level and was not considered an acoustical change as defined in paragraph 21.93(b) of the Federal Aviation Regulations.

Date of Application: May 30, 1997 Date Reissued: September 21, 2005 Date of Issuance: July 29, 1997 Date FEDERAL AVIATION firection of the Adminis for (Signature) Thaddeus D. Krolicki, Jr.

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

PAA 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 S00718CH Date of Issuance: July 29, 1997 Reissued: September 21, 2005 Limitations and Conditions: (Continued):

3. FAA Approved Airplane Flight Manual Supplement, Technical Report (TR) 887 for the Beech Aircraft Models 35-33, 35-A33, 35-B33, 35-C33, E33 and F33, dated July 22, 1997, or later FAA approved revisions is required.

FAA Approved Airplane Flight Manual Supplement, Technical Report (TR) 890 for the Beech Aircraft Models J35, K35, and M35, dated July 22, 1997, or later FAA approved revisions is required.

FAA Approved Airplane Flight Manual Supplement, Technical Report (TR) 891 for the Beech Aircraft Models G33, N35, and P35, dated July 22, 1997, or later FAA approved revisions is required.

4. The Teledyne Continental Motors engine models and Beech aircraft models eligible with the McCauley propeller model 3A36C434/80VEA-0:

Aircraft Model Engine Model Maximum Continuous

HP RPM 35-33, 35-A33 10-470-J, -K 225 2600 35-B33, 35-C33, B33, F33 IO-470-K 225 2600 G33, N35, P35 IO-470-N 260 2625 J35, K35, M35 10-470-C 250 2600

5. Aircraft specifications are the same as listed on Aircraft Specification No. 3A15 except as listed in McCauley Technical Reports (TR) 887, 890, and 891.

6. If the holder agrees to permit another person to use this certificate to alter that product, the holder shall give the other person written evidence of that permission.

...END...

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