# TCDS A17CE: The King's Engineering Fellowship - Type: Type certificate data sheet - Status: Current - Holder: The King's Engineering Fellowship - Revision: 6 - Revised: March 23, 2004 - Product: Aircraft, Small Airplane - Certification basis: Part 23 - Registered aircraft: 3, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/b4/b8/b4b8e47e50a1661afc50f9c31e69a031fe4619777656ffd6eaedcae314493479 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/7F3DA4AA1E9F99C286256E6D006C3169.0001 - Page: https://openairdocs.org/tcds/A17CE ## Models (2) As the data sheet lists them. - 4500-300 Series II - 4500-300 ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A17CE Revision 6 King's Engineering Fellowship 4500-300 4500-300 Series II March 23, 2004 TYPE CERTIFICATE DATA SHEET NO. A17CE This data sheet which is a part of ty pe certificate No. A17C E prescribes conditions and limita tions under which the product for which the type certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations. Type Certificate Holder The King’s Engineering Fellowship 1410 Arizona Place S.W. Orange City, Iowa 51041 TC Holder History: Transferred from Evangel-Air to the King's Engineering Fellowship on March 23, 2004. I - Model 4500-300, 9 PCLM (Normal Category), Approved July 21, 1970 Engines 2 Lycoming IO-540-K1B5 Fuel 100/130 minimum grade aviation gasoline Engine limits For all operations, 2700 r.p.m. (300 hp.) at Sea Level Propeller and 1. (a) 2 Hartzell HC-C2YK-2( )/C 8475A-4 per dwg. 4569A1 propeller limits Diameter: 80 in., no reduction permitted Pitch setting at 30 in. station: low 13.5°, high 80-82° No additional tolerance permitted (b) 2 propeller spinner and bulkhead assemblies, Hartzell 836-29 assembly Airspeed limits (CAS) Never exceed 230 m.p.h. (200 knots) Maximum structural cruising 183 m.p.h. (159 knots) Maneuvering 149 m.p.h. (129 knots) Flaps extended 126 m.p.h. (109 knots) Landing gear extended 200 m.p.h. (174 knots) C.G. range (+102) to (+107.9) at 5500 lb. (+ 99.5) to (+107.9) at 4600 lb. Straight line variation between points given Empty weight C.G. range None Maximum weight 5500 lb. No. of seats 9 (Reference Weight and Balance Data) Maximum baggage 1400 lb. (cargo version) Fuel capacity 112 U.S. gal. (two 56 gal. wing tanks, 55.5 gal. usable in each tank) (+101.4) See NOTE 1 for data on system fuel Oil capacity 12 qt. each engine (See NOTE 1 for data on system oil) Control surface movements Wing flaps Takeoff 0° to 20° Landing 40° + 1.0° Aileron tab Fixed Aileron Up 14° + 1.5° Down 14° + 1.5° Elevator tab Up 30° + 2.0° Down 30° + 2.0° Elevator Up 30° + 1.0° Down 22.5° + 2.0° Rudder tab Right 30° + 2.0° Left 30° + 2.0° Rudder Right 30° + 1.0° Left 30° + 1.0° Serial Nos. eligible 001 thru 003 Page No. 1 2 3 Rev. No. 6 5 5 A17CE Page 2 of 3 II - Model 4500-300 Series II, 9 PCLM (Normal Category), Approved August 8, 1972 Engines 2 Lycoming IO-540-K1B5 Fuel 100/130 minimum grade aviation gasoline Engine limits For all operations, 2700 r.p.m. (300 hp.) at Sea Level Propeller and 1. (a) 2 Hartzell HC-C2YK-2B/C 8475-4 propeller limits Diameter: 80 in., no reduction permitted Pitch setting at 30 in. station: low 13.5°, high 80-82° No additional tolerance permitted (b) 2 propeller spinner and bulkhead assemblies, Hartzell 836-29 assembly Airspeed limits (CAS) Never exceed 230 m.p.h. (200 knots) Maximum structural cruising 183 m.p.h. (159 knots) Maneuvering 149 m.p.h. (129 knots) Flaps extended 126 m.p.h. (109 knots) Landing gear extended 200 m.p.h. (174 knots) C.G. range (+102) to (+107.9) at 5500 lb. (+ 99.5) to (+107.9) at 4600 lb. Straight line variation between points given Empty weight C.G. range None Maximum weight 5500 lb. No. of seats 9 (Reference Weight and Balance Data) Maximum baggage 1400 lb. (cargo version) Fuel capacity 112 U.S. gal. (two 56 gal. wing tanks, 55.5 gal. usable in each tank) (101.4) See NOTE 1 for data on system fuel Oil capacity 12 qt. each engine (See NOTE 1 for data on system oil) Control surface movements Wing flaps Takeoff 0° to 20° Landing 40° + 1.0° Aileron tab Fixed Aileron Up 14° + 1.5° Down 14° + 1.5° Elevator tab Up 20° + 2.0° Down 30° + 2.0° Elevator Up 30° + 1.0° Down 22.5° + 2.0° Rudder tab Right 30° + 2.0° Left 30° + 2.0° Rudder Right 30° + 1.0° Left 30° + 1.0° Serial Nos. eligible 004 and up (See NOTE 4) DATA PERTINENT TO ALL MODELS Datum 60 in. forward of aft face of front door post Leveling means Cabin rear floor Certification basis Part 23 of th e Federal Aviation Regulations dated February 1, 1965 as amended by 23-1 thru 23-6 Application for Type Certificate dated September 16, 1968 Type Certificate No. A17CE issued July 21, 1970 Production basis Production Certificate No. 321 Equipment The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) must be installed in the aircraft for certification. In addition, the following items of equipment are required: 1. On Model 4500-300 airplanes use FAA A pproved Flight Manual dated July 17, 1970. 2. On Model 4500-300 Series II airplanes use FAA Approved Flight Manual dated May 31, 1972. Page 3 of 3 A17CE NOTE 1. Current weight and balance re port, including list of equipment included in certificated empty weight, and loading instructions when necessary, must be provided for each aircraft at the time of original certification. The certificated empty weight and corresponding center of gravity location must include undrainable oil of 4.0 lb. at +50 and unusable fuel of 6 lb. at +101.4 with standard wing tanks. NOTE 2. The placards specified in the FAA Approved Airplane Flight Manual must be displayed. NOTE 3. Reserved. NOTE 4. Model 4500-300 airplanes, Serial Nos. 001 through 003, eligible to be modified as Series II with factory installation of Modification 2 as shown on Evangel dwg. MOD 2-01. ....END.... ``` ## ADs (3, in force first) - [AD 2023-09-09](https://openairdocs.org/ad/2023-09-09): Exhaust Turbine System (Recip) · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 292 more. Effective Jul 17, 2023 - [AD 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI or SA02658SE). Effective Mar 21, 2022 - [AD 81-19-04](https://openairdocs.org/ad/81-19-04): Hose Assembly · Rajay Hose Assemblies, 500A, 500B and 87 more. Effective Sep 17, 1981 ## Registered aircraft by registry model (OpenAirDocs) - [Evangel Air 4500-300-II](https://openairdocs.org/model/evangel-air-4500-300-ii): 2 aircraft (registry code 3340106) - [Evangel Air 4500-300](https://openairdocs.org/model/evangel-air-4500-300): 1 aircraft (registry code 3340104) ## STCs approved under this data sheet (33) - [STC SA12428CH](https://openairdocs.org/stc/SA12428CH): Installation of the Lycoming Engines Electronic Ignition System (EIS). Lycoming Engines, An Operating Division of AVCO Corporation - [STC SA04046CH PAGE 1](https://openairdocs.org/stc/SA04046CH%20PAGE%201): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc. - [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc. - [STC SA01435LA](https://openairdocs.org/stc/SA01435LA): Installation of engines modified with Firewall Forward Technologies LLC modified camshaft. Centri-Lube Technologies LLC - [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc. - [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC - [STC SA11174SC PAGE 1](https://openairdocs.org/stc/SA11174SC%20PAGE%201): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King) - [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation - [STC SA03286CH](https://openairdocs.org/stc/SA03286CH): Install an electronic engine ignition system. Electroair Acquisition Corporation - [STC SA04032CH](https://openairdocs.org/stc/SA04032CH): Install rocker switch assemblies. Electroair Acquisition Corporation - [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation - [STC SA2657WE](https://openairdocs.org/stc/SA2657WE): Installation of turbocharged Lycoming 1O-540-K1B5 engines. TALCO Aviation Corp. dba RAJAY Turbo Products - [STC SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc - [STC SA00382BO](https://openairdocs.org/stc/SA00382BO): Installation of Globalstar Antenna and Cradle provisions to support a Globalstar GPS-1700 in non-composite airplanes. Avidyne Corporation - [STC SA00343BO](https://openairdocs.org/stc/SA00343BO): Installation of a single configuration or a dual configuration Avidyne Corporation Integrated Flight Display, Model IFD540 loaded with Release 10.0 software (or later FAA approved release). Avidyne Corporation - [STC SA00352BO PAGE 2](https://openairdocs.org/stc/SA00352BO%20PAGE%202): Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version),. Avidyne Corporation - [STC SA02119SE PAGE 1](https://openairdocs.org/stc/SA02119SE%20PAGE%201): Installation of Garmin GDL 88 ADS-B UAT Transceiver System. Garmin International Inc - [STC SA01229SE PAGE 1](https://openairdocs.org/stc/SA01229SE%20PAGE%201): Installation of GNS 480 (CNX80) GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Garmin International Inc - [STC SA02442AK PAGE 1](https://openairdocs.org/stc/SA02442AK%20PAGE%201): Approval of the L-3 Communications NGT 2000/2500 ADS-B system. ADS-B Technologies, LLC - [STC SA01933LA-D PAGE 1](https://openairdocs.org/stc/SA01933LA-D%20PAGE%201): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc - [STC SA02717NY PAGE 1](https://openairdocs.org/stc/SA02717NY%20PAGE%201): Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module. VoiceFlight Systems LLC - [STC SA01692SE](https://openairdocs.org/stc/SA01692SE): Installation of a Garmin GMX 200 Multi-Function Display. Garmin International Inc - [STC SA03148NY](https://openairdocs.org/stc/SA03148NY): The installation of the Latitude Technologies Corporation S100 Tracking System. Latitude Technologies Corporation - [STC SA01487SE-D](https://openairdocs.org/stc/SA01487SE-D): Installation of a GDL 69 or GDL 69A XM Satellite Receiver. Garmin International Inc - [STC SA00769CH](https://openairdocs.org/stc/SA00769CH): Installation of Champion Limited Authority Spark Advance Regulator (LASARTM) ignition system with Cylinder Head Temperature (CHT) monitoring capability on airframes with FAA approved installations of Textron Lycoming model IO-540, AEIO-540 and HIO-540 engines.. Champion Aerospace LLC - [STC SA593CH](https://openairdocs.org/stc/SA593CH): Install Champion SlickSTART magneto booster system.. Champion Aerospace LLC - [STC SA01695SE](https://openairdocs.org/stc/SA01695SE): Installation of an antenna. Garmin AT Inc. - [STC SA01487SE](https://openairdocs.org/stc/SA01487SE): Installation of a GDL 69 or GDL 69A XM Satellite Receiver in accordance with Garmin Supplemental Type Certificate Master Data List, P/N 005-C0217-00, Revision A, dated December 20, 2004, or later FAA approved revision.. Garmin AT Inc. - [STC SA5159NM](https://openairdocs.org/stc/SA5159NM): Installation of chip detector system.. Northwest Aircraft Inc - [STC SA19PC](https://openairdocs.org/stc/SA19PC): Installation of fuselage cutout and supporting structure for aerial camera.. Pacific Missionary Aviation - [STC SA02717NY](https://openairdocs.org/stc/SA02717NY) (historical): Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module. VoiceFlight Systems LLC - [STC SA01435DE](https://openairdocs.org/stc/SA01435DE) (historical): Installation of engines, modified with a Firewall Forward Technologies.. Centri-Lube Technologies LLC - [STC SA01933LA](https://openairdocs.org/stc/SA01933LA) (historical): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin AT Inc. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.