# TCDS A2WI: The King’s Engineering Fellowship (TKEF) - Type: Type certificate data sheet - Status: Current - Holder: The King’s Engineering Fellowship (TKEF) - Revision: 5 - Revised: June 27, 2025 - 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/sha256/6a/06/6a06fa0a5712b5d16b4be28cfdba410c3539e015e77e35083bf3e18e29db69e7 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID152722290120250707175420.0001 - Page: https://openairdocs.org/tcds/A2WI ## Models (1) As the data sheet lists them. - 44 ## What the data sheet says From the PDF's text layer, line by line; tables lose their columns. The PDF is the record. ```text Page No. 1 2 3 Rev. No. 5 5 5 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A2WI Revision 5 TKEF 44 June 27, 2025 TYPE CERTIFICATE DATA SHEET NO. A2WI This data sheet, which is part of Type Certificate No. A2WI, prescribes conditions and limitations 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 (TKEF) 1410 Arizona Place SW Orange City, IA 51041 I. Model 44, Angel, 8 PCLM (Normal Category), Approved October 20, 1992 Engines Two Lycoming IO-540-M1A5 (See NOTE 5) Or Two Lycoming IO-540-M1C5 Fuel 100LL/100 minimum grade aviation fuel Engine Limits For all operations, 2700 rpm (300 hp) Propeller and 1. Hartzell constant speed, full feathering propeller Propeller Limits Hub: HC-E3YR-2ALTF/FLC7468 (both engines) Blade: 3 blades aluminum alloy Diameter: 76 in. nominal Minimum allowed for repair: 75 in. No further reduction permitted Pitch setting at 30 in. station: Low pitch 13.2° ±0.2°, Feather 84.5° ±1° 2. Hartzel hydraulic governor: a. V-1-3 for narrow deck engine b. V-1-4 for wide deck engine 3. TKEF spinner assembly: 4459-3000 Airspeed Limits (IAS) Neve r exceed 209 knots (210 KCAS) Maximum structural cruising 174 knots (174 KCAS) Maneuvering 139 knots (138 KCAS) Flaps extended 104 knots (106 KCAS) Minimum control 65 knots (65 KCAS) Landing gear extension 130 knots (130 KCAS) Landing gear retraction 104 knots (104 KCAS) C.G. Range (Landing Gear Extended) (+176.0) to (+186.0) for all operating weights (5800 lb. maximum) Empty Weight C.G. Range None Datum 3.0 in. forward of nose gear pivot point A2WI 2 Rev. 5 I. Model 44, Angel (cont’d) Leveling Means Seat tracks Maximum Weight 5800 lb. for all operations Minimum Crew One (1) pilot No. of Seats 8 maximum (2 at +95, 2 at +128, 2 at +161, 2 at +198) Maximum Baggage 200 lb. Bay 1 (+96) 400 lb. Bay 2 (+126) 400 lb. Bay 3 (+161) 400 lb. Bay 4 (+195) 200 lb. Baggage Compartment (+258) Fuel Capacity 224 gal. (222 gal. useable), two 112 gal tanks in wings at +165.5. See NOTE 1 for data on system fuel and oil. Oil Capacity 12 qt. (9.25 qt. us eable) each engine at +216.5. See NOTE 1 for data on system fuel and oil. Control Surface Wing flaps Down 37° ±2° Ailerons Up 30° +3° Down 7° +5° Spoilers Up 60° ±4° Rudder Right 30° +2° Left 30° +2° Elevator Up 30° +0°, -1° Down 15° +2° Rudder tab Right 28° +2° Left 28° +2° Elevator tab Up 5° +1° Down 24° +2° (with elevator neutral) Serial No’s Eligible 001 and On Data Pertinent to Model 44 Certification Basis: Part 23 of Federal Aviation Regulations (FAR) dated February 1, 1965, as amended by 23-1 through 23-36 and FAR 36 dated December 1, 1969, as amended by 36-1 through 36-18 and Special Conditions 23-ACE-59. Exemption: Stall warning FAR 23.207(c). Production Basis: S/N 001: Manufactured under FAA Type Certificate A2WI only by TKEF S/N 002: Manufactured under FAA Type Certificate A2WI only by Angel Aircraft Corporation (AAC), Orange City, IA, under a licensing agreement between TKEF and AAC, dated October 4, 1986. S/N 003 thru 999: Production Certificate 342CE. The manufacturer (AAC) is authorized to issue airworthiness certificates under 14 CFR 21.183(a). NOTE: This model is listed on the AAC Production Limitation Record and is being produced under the Licensing Agreement between TKEF and AAC, dated October 4, 1986. S/N 1003: Manufactured under CAAC Type Certificate VTC0320A by ALoong Aircraft Company, Ltd. (ALAC), Jingmei, Hubei, PRC, under a Licensing Agreement between TKEF and Dingxuan Liang, dated May 21, 2016. S/N 1004 and On: Chinese Production Certif icate PC077A-ZN. The manufacturer (ALAC) is authorized to issue airworthiness certificates. This model is listed on the ALAC Production Limitation Record and is being produced under a Licensing Agreement between TKEF and Dingxuan Liang, dated May 21, 2016. Equipment: The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) must be installed in the aircraft for certification. This equipment must include the current Airplane Flight Manual (AFM). A2WI 3 Rev. 5 Data Pertinent to Model 44 (cont’d) NOTE 1. Current weight and ba lance report 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. 1. Basic empty weight includes unusa ble fuel of 12 lb. at +165.5. 2. Basic empty weight includes en gine oil of 45 lb. at +216.5. NOTE 2. All required placards in the FAA Approved Airp lane Flight Manual (AFM) must be installed in the appropriate locations. NOTE 3. Mandatory replacement times for structural comp onents are contained in the Limitations Section of the Maintenance Manual. NOTE 4. All replacement seats (crew and passenger), although they may comply with TSO C39, must also be demonstrated to comply with FAR 23.321, 23.395, 23.561, 23.562, and 23.785. NOTE 5. Lycoming IO-540-M1A5 configur ed with two impulse magnetos per TKEF Engine Specification 4450-0001. .... END .... ``` ## ADs (1, in force first) - [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 ## Registered aircraft by registry model (OpenAirDocs) - [Angel 44](https://openairdocs.org/model/angel-44): 2 aircraft (registry code 1141000) - [Kings Engr Fellowship 44](https://openairdocs.org/model/kings-engr-fellowship-44): 1 aircraft (registry code 6560103) ## STCs approved under this data sheet (53, first 50) - [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 SA02636SE](https://openairdocs.org/stc/SA02636SE): Installation of Garmin GPS 175 Navigation System and GNX 375 Navigation System with ADS-B In/Out Transponder.. Garmin International Inc. - [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc. - [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc. - [STC SA04046CH PAGE 2](https://openairdocs.org/stc/SA04046CH%20PAGE%202): 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 SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).. Garmin International Inc. - [STC SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio.. Peregrine - [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 SA10822SC](https://openairdocs.org/stc/SA10822SC): Installation of EFD1000 Primary Flight Display. Aspen Avionics Inc. - [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation - [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems.. Garmin International Inc - [STC SA04032CH](https://openairdocs.org/stc/SA04032CH): Install rocker switch assemblies. Electroair Acquisition Corporation - [STC SA00744DE](https://openairdocs.org/stc/SA00744DE): Installation of the Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT31 Transponder and an approved position sensor. Peregrine - [STC SA00765DE](https://openairdocs.org/stc/SA00765DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine - [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation - [STC SA02153LA-D PAGE 2](https://openairdocs.org/stc/SA02153LA-D%20PAGE%202): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc. - [STC SA04424AT](https://openairdocs.org/stc/SA04424AT): Installation of Continental Motors, Inc. (CMI) Shower-of-Sparks Starting Vibrator Booster Systems. Continental Motors, Inc. - [STC SA01835WI](https://openairdocs.org/stc/SA01835WI): Installation of Trig Avionics TY-96 or TY-97 VHF Communications Radio. Peregrine - [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 2](https://openairdocs.org/stc/SA02119SE%20PAGE%202): 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 2](https://openairdocs.org/stc/SA02442AK%20PAGE%202): Approval of the L-3 Communications NGT 2000/2500 ADS-B system. ADS-B Technologies, LLC - [STC SA01933LA-D PAGE 2](https://openairdocs.org/stc/SA01933LA-D%20PAGE%202): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc - [STC SA02283SE PAGE 2](https://openairdocs.org/stc/SA02283SE%20PAGE%202): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P. Electronics International Inc. - [STC SA02402SE PAGE 2](https://openairdocs.org/stc/SA02402SE%20PAGE%202): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) CGR-30C. Electronics International Inc. - [STC SA02121SE](https://openairdocs.org/stc/SA02121SE): Installation of Garmin GTS 825 (TAS) or GTS 855 (TCAS I) Traffic 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 SA02015SE-D](https://openairdocs.org/stc/SA02015SE-D): Installation of Garmin G500 Primary Flight Display (PFD) and Multifunction Display (MFD) System.. Garmin International Inc - [STC SA02825NY PAGE 2](https://openairdocs.org/stc/SA02825NY%20PAGE%202): Installation of Aerospace Logic Aircraft Instruments. Aerospace Logic Inc. - [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 SA02016SE-D](https://openairdocs.org/stc/SA02016SE-D): Installation of Garmin GTS 800, GTS 820 or GTS 850 Traffic System. Garmin International Inc - [STC SA01487SE-D](https://openairdocs.org/stc/SA01487SE-D): Installation of a GDL 69 or GDL 69A XM Satellite Receiver. Garmin International Inc - [STC SA02018SE-D](https://openairdocs.org/stc/SA02018SE-D): Provisions installation of Garmin GPS/XM Antennas in accordance with FAA Approved Model List (AML) SA02018SE-D, dated January 4, 2011, or later FAA approved revision, and FAA Approved GPS/XM Antenna STC Master Drawing List, Document No.: 005-00638-01, Revision 1 , approved on January 4, 2011, or later FAA approved revision.. 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 SA02655AT](https://openairdocs.org/stc/SA02655AT): Installation of JAARS Model F5K Automatic Flight Following System (AFFS) in Helio H-295 type aircraft.. JAARS Inc. - [STC SA00765DE PAGE 1](https://openairdocs.org/stc/SA00765DE%20PAGE%201) (historical): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine - [STC SA02019SE-D PAGE 2](https://openairdocs.org/stc/SA02019SE-D%20PAGE%202) (historical): Installation of Garmin GTN 6XX/7XX Navigation System. Garmin International Inc - [STC SA02153LA-D](https://openairdocs.org/stc/SA02153LA-D) (historical): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc - [STC SA02717NY](https://openairdocs.org/stc/SA02717NY) (historical): Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module. VoiceFlight Systems LLC All 53: https://openairdocs.org/tcds/A2WI/stcs.md --- 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.