STC SA1036GL

FAA FORM 8110-2(10-68) PAGE 1 of 3 PAGES Number SA1036GL This certificate issued to McCauley Propeller Systems 7751 East Pawnee Wichita, KS 67207

Part 23 of the Federal Aviation Regulations. See Type Certificate Data Sheet A24CE for complete certification basis.

Original Product-Type Certificate Number : A24CE Make : Raytheon Aircraft Company (Beech) Model : 200, 200C, 200CT, 200T, A200C (UC12B), A200CT (RC-12D), (C-12D) and (FWC-12D), B200, B200C (C-12F), B200CT, C200T Description of Type Design Change:

Installation of McCauley Propeller Systems propeller model 4HFR34C755/94LA-0 in accordance with McCauley Technical Report No. 661, dated June 19, 1986 and McCauley Drawing No. D-60000, revised May 2, 1998, or later FAA approved revision; or Installation of McCauley Propeller Systems propeller model 4HFR34C754/94LA-0 in accordance with McCauley Technical Report No. 701, dated April 22, 1988 and McCauley Drawing No. D-60034, dated May 2, 1988, or later FAA approved revision; or Installation of McCauley Propeller Systems propeller model 4HFR34C771/94LA-0 in accordance with McCauley Technical Report No. 830, dated November 30, 1994 and McCauley Drawing No. D-60145, dated December 20, 1994, or later FAA approved revision.

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

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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.

Date reissued : July 19, 2006

Date amended : June 1, 1988, January 11, 1996

( Signature) Thaddeus D. Krolicki, Jr.

Manager, Propulsion Branch Chicago Aircraft Certification Office

(Title) Date of application: April 12, 1985

Date of issuance : June 20, 1986

2. FAA Approved Airplane Flight Manual Supplement TR 660, dated June 20, 1986 with the installation of propeller model 4HFR34C755/94LA-0, or later FAA approved revision, is required.

FAA Approved Airplane Flight Manual Supplement TR 702, dated June 1, 1988 with the installation of propeller model 4HFR34C754/94LA-0 or 4HFR34C771/94LA-0, or later FAA approved revision, is required.

3. Aircraft specifications are the same as listed on Aircraft Specification Data Sheet No. A24CE

Propeller and Propeller Limits For aircraft with propeller model 4HFR34C755/94LA-0 installed:

2 McCauley 4HFR34C755 hubs with 94LA blades Diameter: 90 to 93 inches Flight idle stop: Flight idle propeller low pitch stop is set so that at 1800 RPM there shall be an indicated 750±40 ft-lb torque corrected to seal level standard day.

Propeller blade angle at 30 inches:

Feathered: +87.2° ± 0.3° Reverse: -10.0° ± 0.4° Minimum propeller ground idle RPM for continuous operation shall not be less than 1150 RPM; however, propeller may be feathered on the ground and idled at rotational speeds below 600 propeller shaft RPM.

For aircraft with propeller model 4HFR34C754/94LA-0 installed:

2 McCauley 4HFR34C754 hubs with 94LA blades Diameter: 94 to 93.5 inches Flight idle stop: Flight idle propeller low pitch stop is set so that at 1800 RPM there shall be an indicated 660±40 ft-lb torque corrected to seal level standard day.

Propeller blade angle at 30 inches:

Feathered: +87.2° ± 0.3° Reverse: -10.0° ± 0.4° Minimum propeller ground idle RPM for continuous operation shall not be less than 1100 RPM; however, propeller may be feathered on the ground and idled at rotational speeds below 600 propeller shaft RPM.

For aircraft with propeller model 4HFR34C771/94LA-0 installed:

2 McCauley 4HFR34C771 hubs with 94LA blades Diameter: 94 to 93.5 inches Flight idle stop: Flight idle propeller low pitch stop is set so that at 1800 RPM there shall be an indicated 600±40 ft-lb torque corrected to seal level standard day.

Propeller blade angle at 30 inches:

Feathered: +87.2° ± 0.3° Reverse: -10.0° ± 0.4° Minimum propeller ground idle RPM for continuous operation shall not be less than 1100 RPM; however, propeller may be feathered on the ground and idled at rotational speeds below 600 propeller shaft RPM.

4. 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.

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