STC SA1691GL

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

Number SA1691GL

This certificate issued to

Part 3 of the Civil Air Regulations.

( See Type Certificate Data Sheet 3A15 for complete certification basis)

Installation of McCauley Propeller Model 3A34C423/90DFA-10 in accordan ce with D’Shannon Drawing No. 533420, Revision C, dated October 26, 1991, or later FAA Approved revision.

1. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated, unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft.

This certificate and the supporting data, which is the basis for approval, shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.

D’Shannon Products, Ltd.

1309 County Road 134 Buffalo, MN 55313 3A15 Make : Beech Model :

E33, F33, G33, 35-33, 35-A33, 35-B33, 35-C33, H35, J35, K35, M35, N35, P35 Date reissued : March 15, 2011, June 17, 2011

By direction of the Administrator Original Signed By:

Timothy Smyth

( Signature) Timothy Smyth Manager, Propulsion Branch Chicago Aircraft Certification Office

( Title) Date of application: October 26, 1991

Date of issuance : January 14, 1992

Date of Issuance: January 14, 1992

Limitations and Conditions: (Continued from Page 1 of 3)

2. FAA-Approved Airplane Flight Manual Supplement for Beech Model Aircraft H35; N35, P35, or G33; J35, K35, or M35; and 35-33, 35-A33, 35-B33, 35-C33, E33, F33, all dated December 26, 1991 or later FAA-Approved revisions are required.3. Aircraft specifications are the same listed on Type Certificate Data Sheet No. 3A15, except as follows:

Propeller and Propeller Limits

McCauley 3A34C423 hub with 90DFA-10 blades

Diameter: 80 to 78 inches

Teledyne Takeoff & Propeller Continental Maximum Pitch Setting Beech Motors Combustion Continuous (at 30’ station) Aircraft Engine Damper Ratio HP RPM Low High ( ± 0 . 2 °) (±0.5 °)

35-33, -A33, -B33 IO-470-J, -K 1-5, 1-6 7:1 225 2600 8.8° 29.0°

35-C33 IO-470-K 1-5, 1-6 7:1 225 2600 8.8° 29.0°

E33, F33 IO-470-K 1-5, 1-6 7:1 225 2600 8.8° 29.0°

G33, N35, P35 IO-470-N 4-6 8.6:1 260 2625 11.8° 29.0°

J35, K35, M35 IO-470-C 4-6 8:1 250 2600 11.0° 29.0°

H35 O-470-G 1-6.5, 1-9 8.1 240 2600 10.0° 29.0°

3. 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…