# TCDS A00059SE: Epic Aircraft LLC - Type: Type certificate data sheet - Status: Current - Holder: Epic Aircraft LLC - Revision: 7 - Revised: June 12, 2026 - Product: Aircraft, Small Airplane - Certification basis: Part 23 - Registered aircraft: 133, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/f3/7f/f37fc0759cf39b1399e20726fee63da0eb1dbe093dae4b46ae34007d944bc9be - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184545329120260612140828.0001 - Page: https://openairdocs.org/tcds/A00059SE ## Models (1) As the data sheet lists them. - E1000 ## 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 4 5 Rev. No. 7 5 7 6 6 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A00059SE Revision 7 Epic Aircraft, LLC E1000 June 12, 2026 TYPE CERTIFICATE DATA SHEET NO. A00059SE This data sheet, which is part of Type Certificate No. A00059SE, prescribes conditions and limitations under which the product for which the type certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations TC Holder: Epic Aircraft, LLC 22590 Nelson Road Bend, Oregon 97701 Model E1000 (Utility Category), Approved November 6, 2019 Engine: Engine Manufacturer: Pratt and Whitney Canada, Corp. Number of Engines: One (1) Engine TC Number: E26NE Engine Model Designation: PT6A-67A Fuel: Primary Fuel: Jet A Alternate Fuels: JP-8, Any other fuel which complies with the latest revision of Pratt & Whitney Service Bulletin 14004 Engine Limits: Maximum Takeoff Power: 1,200 horsepower at 1,700 rpm, subject to ambient temperature and pressure conditions See the latest FAA Approved Revision of the appropriate Airplane Flight Manual: “Pilots Operating Handbook and FAA Approved Flight Manual-Epic E1000” , Epic document SK05000001 (SN K003 to K010), or “Pilots Operating Handbook and FAA Approved Flight Manual -Epic E1000 GX”, Epic document SK05001001 (SN K011to K013, SN K015 to K085, and SN K003 to K010 with Epic service bulletin SB-0017 incorporated), or “Pilot's Operating Handbook And FAA Approved AFM for E1000AX”, Epic document SK05003001 (SN K014 and SN K086 and on). Propeller and (4-Blade Propeller) Proleller Limits: Propeller Manufacturer: Hartzell Number of Propellers: One (1) Propeller TC Number: P10NE Propeller Model Designation: HC-E4A-3D/E10477SK/D-5500-1P Diameter Limits: 104” minimum, 105” maximum High Pitch Angle: 79.6° ± 0.5° Low Pitch Angle: 19.0° ± 0.2° Reverse Pitch Angle: -17.5° ± 0.5° Static RPM Limits: Stabilized operation on the ground between 350 and 950 RPM is prohibited . See Propeller TC Data Sheet P10NE for additional details and limitations (5-Blade Propeller) Propeller Manufacturer: Hartzell Number of Propellers: One (1) Propeller TC Number: P20NE Propeller Model Designation: HC-E5A-3A/NC10245B()/105820() Diameter Limits: 104” minimum, 105” maximum High Pitch Angle: 80.0° ± 0.5° Low Pitch Angle: 14.7° ± 0.2° A00059SE Page 2 of 5 Reverse Pitch Angle: -17.5° ± 0.5° Static RPM Limits: Stabilized operation on the ground between 400 and 900 RPM is prohibited See Propeller TC Data Sheet P20NE for additional details and limitations. Airspeed Limits: M MO: 0.6 Mach VMO: 270 kcas VO: 170 kcas VFE (T/O): 180 kcas VFE (FULL): 130 kcas VLO: 150 kcas VLE: 150 kcas Minimum speed with Flaps UP: 120 kcas Autopilot Engaged: Flaps T/O: 110 kcas Flaps FULL: 105 kcas Airframe Life Limits: See section 4 in the “Aircraft Maintenance Manual for the Epic E1000-E1000GX-E1000AX”, Epic document SK05000000 (latest FAA-approved revision), or other FAA approved data. Center of Gravity (C.G.) Range: Aft Limits: Forward Limits: 173.5" aft of datum at 8,000 lbs 172.0" aft of datum at 5,700 lbs 169.9” aft of datum at 5,000 lbs 172.8" aft of datum at 8,000 lbs 169.4" aft of datum at 7,600 lbs 163.0" aft of datum (5,700 lb to 5,000 lbs) Straight-line variation between points Empty Weight None C.G. Range: Datum: 107.62 inches forward of the forward face of the firewall Leveling Means: Place a calibrated level between the middle row seats oriented longitudinally in the airplane. See the latest FAA Approved Revision of the appropriate Airplane Flight Manual: “Pilots Operating Handbook and FAA Approved Flight Manual-Epic E1000” , Epic document SK05000001 (SN K003 to K010), or “Pilots Operating Handbook and FAA Approved Flight Manual -Epic E1000 GX”, Epic document SK05001001 (SN K011to K013, SN K015 to K085, and SN K003 to K010 with Epic service bulletin SB-0017 incorporated), or “Pilot's Operating Handbook And FAA Approved AFM for E1000AX”, Epic document SK05003001 (SN K014 and SN K086 and on). Maximum Weights: Maximum Takeoff: Maximum Landing: 8,000 lb 7,600 lb Minimum Crew: 1 Pilot Number of Seats: Up to 6 seats total in accordance with the latest FAA Approved Revision of the appropriate Airplane Flight Manual: “Pilots Operating Handbook and FAA Approved Flight Manual -Epic E1000” , Epic document SK05000001 (SN K003 to K010), or “Pilots Operating Handbook and FAA Approved Flight Manual -Epic E1000 GX”, Epic document SK05001001 (SN K011to K013, SN K015 to K085, and SN K003 to K010 with Epic service bulletin SB-0017 incorporated), or “Pilot's Operating Handbook And FAA Approved AFM for E1000AX”, Epic document SK05003001 (SN K014 and SN K086 and on). A00059SE Page 3 of 5 Maximum Compartment Weights: As defined in the appropriate Airplane Flight Manual: See the latest FAA Approved Revision of the appropriate Airplane Flight Manual: “Pilots Operating Handbook and FAA Approved Flight Manual -Epic E1000” , Epic document SK05000001 (SN K003 to K010), or “Pilots Operating Handbook and FAA Approved Flight Manual -Epic E1000 GX”, Epic document SK05001001 (SN K011to K013, SN K015 to K085, and SN K003 to K010 with Epic service bulletin SB-0017 incorporated), or “Pilot's Operating Handbook And FAA Approved AFM for E1000AX”, Epic document SK05003001 (SN K014 and SN K086 and on). Fuel Capacity: One 139 US gal tank in each wing at 180.9" aft of datum when full and 178.0” aft of datum when empty; (278 US gal total; 264 gal usable, 14 gal unusable) Note: add weight of unusable fuel to the certificated empty weight Oil Capacity: Maximum System Capacity 3 US gal (11.35 L), Usable Capacity 2.5 US gal (9.4 L) Any oil conforming to MIL-PRF-23699G, Type II (5cSt) and as specified in the latest revision of Pratt and Whitney Service Bulletin 14001. Note: add weight of unusable oil to the certificated empty weight Maximum Operating FL340 Altitude: Control Surface Wing Flaps: Up: 0 Takeoff: 12° ±2° Full: 42.8° - 43.4° Movements: Ailerons: Up: 20° ±2° Down: 15.5° ±0.5° Aileron Trim Tab: Up: 17° ±2° Down: 17° ±2° Elevator: Up: 25.5°-25.8° Down: 13.5° ±2° Elevator trim tab: Up: 7.5° ±1° Down: 19.5° ±0.5° Rudder: Left: 18°-19° Right: 18°-19.5° Rudder trim tab: Left: 20° ±0.5° Right: 5°±1° Rudder Limiter: Left: 5.5°-6.5° See the latest FAA accepted revision of the E1000 “Aircraft Maintenance Manual for the Epic E1000-E1000GX-E1000AX”, Epic document SK05000000, or other FAA approved data for flap rigging instructions and setting Flaps up (0°) configuration Manufacturer’s K003 and on Serial Numbers: Certification Basis: Title 14, Code of Federal Regulations (14 CFR) Part 23 effective February 1, 1965, as amended by 23-1 through 23-62. For SN K014 and SN K086 and on (E1000AX configuration, see NOTE 7), 14 CFR Part 23 sections 23.2010, 23.2135, 23.2325, 23.2405, 23.2440, 23.2500, 23.2505, 23.2510, 23.2525, and 23.2605 as amended by 23-1 through 23-64. 14 CFR Part 34 as amended through 34-4 14 CFR Part 36 as amended through 36-30. Equivalent Level of 14 CFR Part 23.221 Spinning by installing a stick pusher/shaker in accordance with Safety Finding: ELOS Memo No. TC11773SE-A-F-1 14 CFR Part 23 Amendment 23-62 errors with ELOS Memo TC11773SE-A-F-2 TC Number: A00059SE TC Issuance Date: November 6, 2019 TC Application Date: October 10, 2015 Operational Restrictions: Day-Night, Visual Flight Rules (VFR) and Instrument Flight Rules (IFR). Flight into known icing (FIKI) conditions is allowed for aircraft SN K056 and on when the required equipment listed is installed, and the airplane operated, in accordance with the appropriate Airplane Flight Manual: “Pilots Operating Handbook and FAA Approved Flight Manual-Epic E1000” , Epic document SK05000001 (SN K003 to K010), or “Pilots Operating Handbook and FAA Approved Flight Manual -Epic E1000 GX”, Epic document SK05001001 (SN K011to K013, SN K015 to K085, and SN K003 to K010 with Epic service bulletin SB-0017 incorporated), or “Pilot's Operating Handbook And FAA Approved AFM for E1000AX”, Epic document SK05003001 (SN K014 and SN K086 and on). A00059SE Page 4 of 5 For airplanes that were not equipped with the required equipment for FIKI) during production (SN K003 through K055), flight into known icing conditions is allowed only when the airplane is retrofitted in accordance with Epic SB-0035. Aircraft properly retrofitted and operated in FIKI conditions must be operated in accordance with the “Pilots Operating Handbook and FAA Approved Flight Manual-Epic E1000”, Epic document SK05000001 Revision D or later FAA approved revision (SN K003 through K010), or the “Pilots Operating Handbook and FAA Approved Flight Manual- Epic E1000 GX”, Epic document SK05001001 Revision A or later FAA approved revision (SN K011 and on, or SN K003-K010 with Epic SB-0017 incorporated). Flight into known severe icing, freezing rain, freezing drizzle, or supercooled large drops is prohibited. Flight into known icing conditions requires the ice protection system to be fully-operational. All operational restrictions as defined in latest approved revision of the latest FAA Approved Revision of the appropriate Airplane Flight Manual: “Pilots Operating Handbook and FAA Approved Flight Manual-Epic E1000” , Epic document SK05000001 (SN K003 to K010), or “Pilots Operating Handbook and FAA Approved Flight Manual -Epic E1000 GX”, Epic document SK05001001 (SN K011to K013, SN K015 to K085, and SN K003 to K010 with Epic service bulletin SB-0017 incorporated), or “Pilot's Operating Handbook And FAA Approved AFM for E1000AX”, Epic document SK05003001 (SN K014 and SN K086 and on). For airplanes equipped with optional weather radar, the airplane must be operated in accordance with the appropriate Pilots Operating Handbook and FAA Approved Flight Manual listed above and the latest FAA approved revision of the “Pilot’s Operating Handbook and FAA Approved Airpalne Flight Manual Supplement for Garmin GWX 8000 Weather Radar”, Epic document SK05001501. For airpalnes equipped with optional Starlink antenna, the airplane must be operated in accordance with the appropriate Pilots Operating Handbook and FAA Approved Flight Manual listed above and the latest FAA approved revision of the “ Pilot’s Operating Handbook and FAA Approvrf Airplane Flight Manual Supplement for Starlink Antenna”, Epic document SK05001502. Production Basis: PC 733NM Equipment: The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) must be installed in the aircraft for airworthiness certification. Additional Equipment Necessary for Type Certification: The latest FAA Approved Revision of the appropriate Airplane Flight Manual: “Pilots Operating Handbook and FAA Approved Flight Manual -Epic E1000”, Epic document SK05000001 (SN K003 to K010), or “Pilots Operating Handbook and FAA Approved Flight Manual -Epic E1000 GX”, Epic document SK05001001 (SN K011to K085, or SN K003 to K010 with Epic SB-0017 incorporated), or “Pilot's Operating Handbook And FAA Approved AFM for E1000AX”, Epic document SK05003001 (SN K086 and on). For airplanes equipped with optional weather radar, the latest FAA approved revision of the “Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual Supplement for Garmin GWX 8000 Weather Radar”, Epic document SK05001501. For airpalnes equipped with optional Starlink antenna, the latest FAA approved revision of the “Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual Supplement for Starlink Antenna”, Epic document SK05001502. NOTE 1: A current weight and balance report, including a list of equipment included in the certificated empty weight, and loading instructions when necessary must be provided for each aircraft at the time of original certification. This is in accordance with 14 CFR 23.23, 23.25, and 23.29. NOTE 2: All placards required by either FAA Approved Airplane Flight Manual, the applicable operating rules, or the Certification Basis must be installed in the airplane. The required approved placards are specified in the latest FAA approved revision of t he latest FAA Approved Revision of the appropriate Airplane Flight Manual: “Pilots Operating Handbook and FAA Approved Flight Manual-Epic E1000” , Epic document SK05000001 (SN K003 to K010), or A00059SE Page 5 of 5 “Pilots Operating Handbook and FAA Approved Flight Manual -Epic E1000 GX”, Epic document SK05001001 (SN K011to K013, SN K015 to K085, and SN K003 to K010 with Epic service bulletin SB-0017 incorporated), or “Pilot's Operating Handbook And FAA Approved AFM for E1000AX”, Epic document SK05003001 (SN K014 and SN K086 and on). NOTE 3: The airplane must be subsequently maintained in accordance with the Instructions for Continued Airworthiness, and Airworthiness Limitations section, as contained in the“Aircraft Maintenance Manual for the Epic E1000-E1000GX-E1000AX “ Epic document SK05000000 Revision I or later FAA-approved reivsion, or other FAA approved data. For aircraft equipped for flight into known icing, the ice protection equipment must be maintained in accordance with the “Aircraft Maintenance Manual for the Epic E1000-E1000GX-E1000AX”, Epic document SK05000000 Revision G or later FAA-accepted revision. NOTE 4: The airplane shall be manufactured in accordance with the latest FAA approved revision of the “E1000 Master Drawing List”, Epic document CK00000127, or other FAA approved data. NOTE 5: Exterior colors are limited to those specified in the latest FAA approved revision or Epic Aircraft “Process Specification: Paint”, Epic Document SX51200003, or other FAA approved data. NOTE 6: Major structural repairs must be accomplished at FAA certified repair stations rated for composite aircraft structure work, in accordance with FAA approved Epic Aircraft, LLC repair methods contained in “Aircraft Maintenance Manual for the Epic E1000-E1000GX-E1000AX”, Epic document SK05000000, or other methods approved by the FAA. NOTE 7: Airplanes SN K003 through K010 use the marketing name “E1000” for model configuration, with four-bladed propellers and Genesys Aerosystems Intelliflight 2100 Digital Flight Control Systems. These aircraft use the “Pilots Operating Handbook and FAA Approved Flight Manual-Epic E1000”, Epic document SK05000001. Ai rplanes SN K011 to K013 and SN K015 to K085 use the marketing name “E1000 GX” for model configuration, with five-bladed propellers and Garmin GFC 700 Automatic Flight Control Systems. These aircraft use the “Pilots Operating Handbook and FAA Approved Flight Manual-Epic E1000 GX”, Epic document SK05001001. Airplanes S N K014 and SN K 086 and on use the marketing name “E1000AX” for model configuration, with autothrottle, electic brake hold, and other changes. These aircraft use the “Pilot's Operating Handbook And FAA Approved AFM for E1000AX”, Epic document SK05003001. An airplane can be modified from the “E1000” model configuration to the “E1000 GX” model configuration by incorporating Epic SB-0017. NOTE 8: Airplanes SN K003 through K055 must have SB-0035 incorporated for flight into known icing (FIKI) operations. This service bulletin incorporates required changes to the aircraft, the appropriate Pilots Operating Handbook and FAA Approved Flight Manual for the model configuration. Airplanes SN K056 and on will be produced with the required equipment for FIKI operations installed. NOTE 9: Airplanes SN K086 and on may have optional Garmin GWX 8000 weather radar installed during production. Airplanes SN K003 through K0085, or airplanes SN K086 and on that were not delivered with the optional weather radar installed, may have the weather radar retrofitted in accordance with Epic Service Bulletin SB-0062. Airplanes retrofitted with weather radar by Epic Service Bulletin SB- 0062 must be operated in accordance with the appropriate Pilots Operating Handbook and FAA Approved Flight Manual and the latest FAA approved revision of the “Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual Supplement for Garmin GWX 8000 Weather Radar”, Epic document SK05001501. NOTE 10: Airplanes SN K086 and on may have optional Starlink antenna installed during production. Airplanes SN K003 through K0085, or airplanes SN K086 and on that were not delivered with the optional Starlnk antenna installed, may have the Starlink antenna retrofitted in accordance with Epic Service Bulletin SB-0063. Airplanes retrofitted with the Starlink antenna by Epic Service Bulletin SB-0063 must be operated in accordance with the appropriate Pilots Operating Handbook and FAA Approved Flight Manual and the latest FAA approved revision of the “Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual Supplement for Starlink Antenna”, Epic document SK05001502. .....END..... ``` ## ADs (1, in force first) - [AD 2023-20-07](https://openairdocs.org/ad/2023-20-07): TE Flap Control System · Epic E1000. Effective Nov 22, 2023 ## Registered aircraft by registry model (OpenAirDocs) - [Epic E1000](https://openairdocs.org/model/epic-e1000): 133 aircraft (registry codes 3390119, 05634CH) ## STCs approved under this data sheet (1) - [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC --- 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.