STC SA4043WE

Shited States of Dience:

Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number 51404318 This certificate issued to: Aircraft Technical SerVICE.

Certifies that the change in the type design for the fillowing freduci with the limitations and conditions thereforasspecifed heranmeets the wireerhiness squirements / Furt 03 of the CIV11 Air Rugulations: (Refer to SIC continuation sheets, pages 3 through 8.)

Original Product -Typelestificate Number: A-771 Make: Beech Model: E-35 Description of Type Design Change: Installation of Continental I0-520-BA engine and McCauley 3A32C propeller in accordance with FAA sealed Aircraft Technical Service Master Drawing List 1716, Revision N, dated October 22, 1979, or later FAA-approved revisions. Supplement No. 1, dated October 26, 1979, to Becch AFM No. 35-590060-3 or later Aircraft Technical Service Airplane Flight Manual FAA-approved revisions is required with this installation.

Limitations and Conditions: The approval of this type design change applies . basically to the Beech listed models only. This approval should not be extended to other specific airplanes of this model on which other previously approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those previously approved modifications will introduce no adverse effect upon the airworthiness of that airplane. Refer to continuation sheets page 3 through 8.

This verificate and the supjuring dute which is the tresis for spferval shall vemain in effect undit sur-.

senderet, suspended, sevted, or a termination dale is theraie cataltished by the Stamini truler of the Federal Aviation Administration .

Date of Application: June 22, 1977 Date Reissued:

Tale sfissuance: October 26, 1979 AVIATION Drydinchin Lease (Signature ) AHINISTRATO Acting Chief, Aircraft Engineering Division (Title) Any alteration of this ertificate is punishable by a fine of not exceeding $1,000, or in- sonment not extreding 3 years, or both This conficate ma be befored in cordance with FAR 21.47

Sinical States of Steria Department of Transportation Federal Aviation Administration 10/26/79 (I) Supplemental Type Certificate (Continuation Sheet) Number: SA10A34E Supplemental Type Certificate Addendum No. SA4043WE Limitations and Conditions: continued

(a) This aircraft is approved for normal category operation only.

(b) No takeoff is permitted when fuel quantity gauges indicate in yellow band or with less than 13 gallons in each main tank.

(c) Installation of two 15 gallon Beryl D'Shannon Aviation Specialties Inc. auxiliary wing tip fuel tanks in accordance with STC SA153EA is required with this installation.

Installation of Beryl filtrator air-oil separator in accordance with STC SA2653WE is required with this installation.

(e) Installation of Beryl exhaust silencers in accordance with STC SA884S0 is required with this installation.

Installation of Beryl fiberglass inlet and exhaust scoops in accordance with STC SA838SO is required with this installation.

For at Technical Service A Supplement do. card ATS raving 1716. Aircraft Technical Service The conditions and limitations of Aircraft Specification No. A-777 apply except as follows:

This data sheet, which is a part of Supplemental Type Certificate No. SA4043WE, prescribes conditions and limitations under which the product for which the STC was issued meets the airworthiness requirements of the Federal Aviation Regulations.

Supplemental Type Certificate Holder: Aircraft Technical Service 6701 Odessa Avenue Van Nuys, California

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rital State of Steric Department of Transportation Federal Aviation Administration 10/26/79 (I) Supplemental Type Certificate (Continuation Sheet) Number: SA90931E Supplemental Type Certificate Addendum No. SA4043WE I - Model Beech E-35, 4 PCLM (Normal Category) is modified by STC SA4043WE, approved Engines Two Continental I0-520-BA Fuel 100/130 Minimum grade aviation gasoline Engine Limits HP RPM MAN. Pr. Hg Takeoff, S.L. 285 2700 Full Throttle Maximum Continuous, S.L. 185 2300 23.8 For non-standard sea level and altitude conditions, the maximum continuous power limit is indicated by the following manifold pressure limit table:

MAXIMUM CONTINUOUS POWER SETTING FOR 185 H.P.

185 HP (1) NO RAM for 2300 RPM (2) NO CARB TEMP INLET RISE TEMP (0° F) - 20 +20 +40 +60 +80 +100 +120

ALTITUDE M.P. LIMIT S.L. 2000 22.81 23.14 23.46 23.80 24.14 24.48 22.80 23.14 24.83 24.50 4000 21.75 22.10 22.45 22.79 23.81 6000 21.38 21.74 22.08 22.43 22.78 8000 21.02 21.38 21.74 F.T. F.T.

10000 F.T. F.T. F.T.

F.T. FULL THROTTLE

FAA FORM 8110-2-1 (10-69) PAGE OF8 PAGES FAA AC 730551

Department of Transportation Federal Aviation Administration 0/26/79 (I) Supplemental Type Certificate (Continuation Sheet) Number SA4043WE Supplemental Type Certificate Addendum No. SA4043WE Propeller and Propeller Limits McCauley 3A32C, Constant Speed, Hydraulic

(a) Hub 3A32C76

(b) Blades 82NB2

(c) Diameter: Maximum 80 inches Minimum 78.5 inches

(d) Pitch setting at 30 inch station Low 13.3° + •2° High 29.0° ‡ .5°

(e) Woodward governor assembly Model D210680 Maximum Permissible Temperatures Cylinder head (bayonet) 460° F Oil inlet 240° F Fuel Flow Normal (gph) Minimum (psi) Maximum (psi)

6.9 to 24.3 1.5 17.5 0/26/79 (I) Supplemental Type Certificate (Continuation Sheet) Number SA4043WE Supplemental Type Certificate Addendum No. SA4043WE Oil Pressure Minimum (psi) Maximum (psi) Normal (psi) Maximum allowable 100 Normal operating 30 - 60 Idle 10 Oil Capacity 12 qts Alternator Prestolite alternator, 12 volt, ALX9424

(a) Max. load on ground, 30 amp at less than 1000 rpm

(b) Max. load in flight, 50 amp Airspeed Limits Refer to Type Certificate Data Sheet A-777 Center of Gravity Limits Maximum Weight: 2925 pounds CG Limitations (wheels down) (Gear Extended) 2925 Gross Weight 2240 -- --

76.5 83.2 84.9 (CG of tip tank fuel is Inches Aft of Datum 87 inches aft of datum).

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nina States of Certica Department of Transportation Federal Aviation Administration 10/26/79 (I) Supplemental Type Certificate (Continuation Sheet) Nembox SA4043WF Supplemental Type Certificate Addendum No. SA4043WE Empty Weight CG Range Refer to Type Certificate Data Sheet A-777 Maximum Weight 2925 1b.

No. of Seats Refer to Type Certificate Data Sheet A-777 Maximum Baggage 10 gallon auxiliary baggage tank. With this item installed, baggage and auxiliary fuel shall not exceed 258 1b.

Fuel Tank Capacity Refer to Type Certificate Data Sheet A-777 note: (a) fo one 10-960 Fuel system consists of two 20 gallon (17 gal. useable) main tanks in wings and one 10 gallon auxiliary tank installed in baggage compartment.

(D) Wing tip fuel transfer tanks with a useable capacity of 15 gallons each are required per STC SA153EA.

Flight Load Factor Limits Design Structural Load Factor:

(a) Wing flaps up, 3.8G

(b) Wing flaps down, 2.0G Maximum Operating Altitude 18,000 ft.

Certification Basis For STC Modification SA4043WE Part 03 of Civil Air Regulations effective November 13, 03. 124) 13 incis (ng eat graphs 23.51(3), 23.85(5),

23.75(b), and 23.77(b) of Federal Aviation Regulations dated February 1, 1965, as amended by 23-1 through 23-20.

or imprisonment not exceeding 3 years, or boin FAA FORM 8110-2-1 (10-59) This eatifusie may be trasfered in accordance with FAR 21.47.

FAA AC 73-2953

Shital Sistes of Scree Department of Transportation Federal Aviation Administration 10/26/79(I) Supplemental Type Certificate (Contimacion Sheet) Neertex SA40431E Supplemental Type Certificate Addendum No. SA4043WE Note 1. Current weight and balance report, based on actual weighing of each modified serial number airplane, together with list of equipment included in certificated empty weight, and loading instructions, must be provided for each aircraft.

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PROR 8 OKS PAGES FAA AG 75-2051