STC SA4-1189

(7-56) LIVE VERDAU TASYAN INSTRATON

FEDERAL AVIATION AGENCY Supplemental Type Certificate

1. NAME AND ADDRESS OF APPLICANT Form Approved, Budget Bureau No. 41-R1823 INSTRUCTIONS - Submit in triplicate to local FAA Flight Operations and Airworthiness Inspector. Copy will be returned to applicant upon issuance.

Supplemental Type Certificate APPLIED FOR:

Mr. Basil Nikhalkin AIRCRAFT ENGINE PROPELLER Lomita. California 24707 Cypress BELLANCA 14-9. N130E, Serial 1029 ORIGINAL MODEL DESIGNATION NEW MODEL DESIGNATION (If desired) None

3. DESCRIPTION OF CHANGE Installation of Franklin 6A4-150-B3 engine and Universal (Koppers) Aeronatic propeller 1200/00-74B in accordance with Bastl Mikhalkin Drawings Nos 14-9-1 through 14-9-5 inclusive LIMITAFIOV OF APPLICABILITY Data not suitable for reproduction of instaliation in other aircraft; therefore, it is satisfactory for Bellanca 14-9, Ni30b, Serial 1029 only. No additional modifications of this type are to be approved solely by reference to this Supplemental Type Certificate or to the data submitted there- See Reverse Side for Operating Limitations.

4a. WILL DATA BE AVAILABLE FOR SALE OR RELEASE TO OTHER PERSONS? YES NO

b. WILL PARTS BE MANUFACTURED FOR SALE (Ref. CAR 1.55)? YES NO

5. SIGNATURE AND TITLE OF APPLICANT Basid Mishall

SIGNATURE July 1. 1959 Ommer Date of Application: TITLE

6. TO BE COMPLETED BY CAXX FAA

NATURE AND LOCATION OF DATA Basil Mikhalkin Dwgs Nos. 14-9-1 through 14-9-5.

Basil Vikhalkin Report No. BM-RJ dated June 20 1960 Data are on file in the Engineering & Manufacturing Branch. FAA Region IV.

Los Angeles California Certification Basis: CAR 4a ORIGINAL TYPE CERTIFICATE NO. CAXAPPROVAL 716 Original signed by Supplemental Type Certificate NO. SIGN AFORE L LippiS Charles R. Hawks SA4-1189

DATE OF APPROVAL Acting Chief . Engineering & Manufacturing Branch June 28. 1960 TITLE USCOMM-DC 32772 FORM ACA-2417 (7-56)

OPERATIONS LIMITATIONS ENGINE: Franklin 6A4-150-B3 ENGINE LIMITS: For all operations 2600 RPM (150 H.P.)

FUEL: 80/87 Minimum Octane Aviation Gasoline PROPELLER: Universal (Koppers) F200/0074B Hub F200 Blades 00-74B Parts List Assembly No. 4275 Installation must be in accordance with Koppers Installation and Operating Limitation No. 1.B (without altitude control)" Pitch setting at 24" Station LoW: 14° High: 25° Static RPM at Maximum Permissible Throttle Setting:

Maximum - 2500 Minimum - 2450 Diameter:

Maximum - 74" Minimum - 74" POWER PLANT INSTRUMENTS: Tachometer: 2600 RPM (Red Line) 011 Temperature: 230°F (Red Line) Oil Pressure: Minimum 30 psi (Red Line) Maximum 60 psi (Red Line) Green arc between 30 psi and 50 psi Fuel Pressure: Minimum 1.0 psi (Red Line) Maximum 7.0 psi (Red Line) Green arc between 1.0 psi & 7.0 psi Cylinder head temperature: 530°F (277°C) (Red Line) C. G. RANGE: +19.6" to +24.2" The following placard shall be installed on the instrument panel in full view of the pilot and passenger:

"TOTAL WEIGHT OF PILOT AND PASSENGER SHALL NOT EXCEED 410 LBS. PASSENGER (IF CARRIED) SHALL OCCUPY THE REAR SEAT.

A COPY OF THESE LIMITATIONS SHALL BE CARRIED IN THE AIRCRAFT AT ALL TINES.