# TCDS A00057SE: Cub Crafters Inc. - Type: Type certificate data sheet - Status: Current - Holder: Cub Crafters Inc. - Revision: 0 - Revised: February 14, 2019 - Product: Aircraft, Small Airplane - Certification basis: Part 23 - Data sheet PDF: https://openairdocs.org/files/sha256/f2/2c/f22c91b65daac9d2f3bcbedfef4a386dd9bcd68e50aa8a99086937c3947ba2a9 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/BB6D6B8AE9416B92862583C9006553AB.0001 - Page: https://openairdocs.org/tcds/A00057SE ## Models (1) As the data sheet lists them. - CC21-180 ## 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. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A00057SE Initial Release CUB CRAFTERS CC21-180 February 14, 2019 TYPE CERTIFICATE DATA SHEET A00057SE This data sheet, which is part of Type Certificate No. A00057SE, 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: Cub Crafters, Inc. 1918 South 16th Ave. Yakima, WA 98903 I - Model CC21-180 (Primary Category), Approved February 14, 2019 Engine: Engine Manufacturer: Lycoming Engines, An Operating Division of AVCO Corporation Number of Engines: One (1) Engine TC Number: E-286 Engine Model Designation: O-360-C1G Fuel: 100 (green) or 100LL (blue) grade aviation fuel. Engine Limits: Maximum takeoff power: 180 horsepower at 2700 RPM Maximum continuous power: 180 horsepower at 2700 RPM See Engine Type Certificate Data Sheet E-286 for additional limitations. Propeller: Propeller Manufacturer: Hartzell Propeller, Inc. Number of Propellers: One (1) Propeller TC Number: P-920 Propeller Model Designation: HC-C2YR-1N/NG8301-5 Diameter Limits: 78 inches. No diameter reduction allowed High Pitch angle: 29.0º-30.0º Low Pitch Angle: 9.7º-10.0º See Propeller Type Certificate Data Sheet P-920 for additional limitations. Airspeed Limits VO (2300 lbs) 86 KCAS VO (1980 lbs) 79 KCAS VFE (46º) 73 KCAS VNO 117 KCAS VNE 142 KCAS Center of Gravity (C.G.) Range Aft Limits: 79.5” aft of datum (1,600 lbs. to 2,300 lbs.) 78.5” aft of datum (1,300 lbs.) Forward Limits: 72.0” aft of datum ((1,300 lbs. to 1,680 lbs.) 79.1’ aft of datum (2,300 lbs.) Straight line variation between points. A00057SE Page 2 of 3 When equipped with Wipaire 2100A amphibious and 2100S seaplane floats Aft Limits: 79.5” aft of datum (2,070 lbs. to 2,300 lbs.) 78.0” aft of datum (1,500 lbs.) Forward Limits: 71.5” aft of datum ((1,500 lbs. to 2,015 lbs.) 75.0’ aft of datum (2,300 lbs.) Straight line variation between points. Datum: Datum is 60” forward of the wing leading edge. Levelling means: See latest approved revision of the CC21-180 “Pilot’s Operating Handbook and FAA Approved Flight Manual”. Maximum Weights: Maximum Ramp: 2,300 lbs. Maximum Takeoff: 2,300 lbs. Maximum Landing: 2,300 lbs. Minimum Crew: One (1) Pilot Number of Seats: Two (2) seats total Pilot located at 72.2” aft of datum Passenger located at 97.5” aft of datum Maximum Compartment As defined in the latest approved revision of the CC21-180 “Pilot’s Operating Handbook and Weights: FAA Approved Flight Manual”. Fuel Capacity: One 24.5 gallon tank in each wing at 84.5” aft of datum; 23 gallons usable in each wing, 1.5 gallons unusable in each wing (49 gallons total; 46 gallons usable; 3 gallons unusable). Note: add weight of unusable fuel to the certificated weight. Oil Capacity: 8 quart total See Lycoming Service Instruction 1014 for approved oil . Maximum Operating 14,000 feet Altitude Control Surface Wing flaps: 0º, 16º, 33º, 46º ± 1.0º Movements: Ailerons: Up: 20º ± 1.5º Down 14º ± 1.5º Elevator: Up 25º ± 1.5º Down 15º ± 1.5º Stabilizer Up 4.9º +0.1º/-0.0º Down 2.5º +0.0º/-0.1º Rudder Left 22.5º +0/-0.75º Right 25º +0/-0.75º See the latest FAA approved revision of the CC21-180 “Airplane Maintenance Manual, or other FAA approved data, for control system rigging instructions and setting flaps up (0º) configuration. Manufacturer’s The information contained herein is applicable to Serial Numbers CC21-0001 and greater. Serial Numbers: Certification Basis: Part 23 of the Federal Aviation Regulations (FAR) effective December 18, 1964, as amended by 23- 1 through 23-62. FAR 36 as amended on the date of certification. Equivalent Level of Emergency exit requirements of FAR 23.807 in accordance with ELOS No TC10279SE-A-C-1. Safety Finding Electronic display instruments of FAR 23.1311 in accordance with ELOS No AT12936SE-A-S-1. Correction to errors in Amendment 23-62 in accordance with ELOS No TC10279SE-A-G-9. Trim requirements of FAR 23.161(c)(1)(i) and (c)(4)(i) in accordance with ELOS AT12949SE-A-F- 1 Page 3 of 3 A00057SE Exemption: Exemption from the requirements of §23.562 of Title 14, Code of Federal Regulations (14 CFR) Regulatory Docket No. FAA-2009-1161. TC Number: A00057SE TC Issuance Date: February 14, 2019 TC Application Date: August 14, 2018 Operational Limitations: Day-Night, Visual Flight Rules (VFR) Airframe Life Limits: See the latest FAA approved revision of the CC21-180 “Airplane Maintenance Manual”. Production Basis: Production Certificate 72NM. 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 The latest FAA Approved/ Revision of “CC21-180 Pilots Necessary for Type Certification: Operating Handbook and FAA Approved Flight Manual”. ______________________________________________________________________________________________________ NOTE 1: A current weight and balance report with a list of equipment included in the certificated empty weight must be provided for each aircraft at the time of original airworthiness certification. NOTE 2: The placards specified in the latest FAA Approved/Accepted Revision of “CC21-180 Pilots Operating Handbook and FAA Approved Flight Manual,” are required. NOTE 3 The airplane must be subsequently maintained in accordance with the Instructions for Continued Airworthiness, and Airworthiness Limitations section, as contained in the latest FA A approved data. NOTE 4 Installation of Wipaire 2100A amphibious or 2100S seaplane floats series floats in accordance with latest FAA Approved Cub Crafters drawings: XC44001 XC44100, XC44500, XC44700. Installation requires approved flight manual supplements. NOTE 5 Installation of Wipaire 2100A amphibious floats requires installation of Wipaire STC SA39CH “Installation of an Amphibian Landing Gear Position Advisory System”. END ``` ## ADs None name its models. ## STCs approved under this data sheet (1) - [STC SA02553AK](https://openairdocs.org/stc/SA02553AK): Fabrication and installation of a Tail Wheel Anti-Shimmy Dampener. Keller Engineering Group 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.