TCDS A00080CE

Page No. 1 2 3 4 Rev. No. 0 0 0 0 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A00080CE Revision 0 Blackshape S.p.A. BK 160-200 June 21, 2024 TYPE CERTIFICATE DATA SHEET No. A00080CE This Data Sheet which is a part of Type Certificate No. A00080CE 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 Blackshape S.p.A. S.S. 16 km 841 +900 Z.I. 70043 Monopoli (BARI) Italy Type Certificate Holder Record -/- I. Model BK 160-200 (Special Class), Approved June 21, 2024 Engine Textron Lycoming IO-320 D1B, TCDS 1E12 Fuel AVGAS 100 or 100LL minimum grade aviation gasoline Engine Limits Maximum take-off and maximum continuous: 160 SHP/2700 RPM Propeller Hartzell Raptor series Hub: 3C1-L675A1 Governor: S-1-78 Blades: 76C03-7 No. of Blades: 3 Type Certificate: TCDS IM.P.137 Propeller Limits Diameter 69. 0 in. (1.75 m) Airspeed Limits Never Exceed Speed VNE 172 KCAS Maximum Structural Cruising Speed V NO 148 KCAS Design Manoeuvring Speed V A 122 KCAS Maximum Flap Fully Extended Speed V FE-LND 100 KCAS Maximum Flap Take-Off Speed V FE-T/O 110 KCAS Max. Landing Gear Extended Speed V LE 110 KCAS Max. Landing Gear Operating Speed V LO 110 KCAS Maximum Weight Take-Off 1874 lbs. (850 kg) Landing 1874 lbs. (850 kg) Center of Gravity (C.G.) Range Forward C.G. (aft of datum) up to 1686 lbs. (765 kg) 34.2 in. (0.868 m) up to 1874 lbs. (850 kg) 36.3 in. (0.923 m) Varying Linearly with weight in between Rear C.G. (aft of datum) at 1874 lbs. (850 kg) 39.3 in. (0.998 m) Empty Weight C.G. Range None Page 2 of 4 A00080CE Reference Datum Composite Bulkhead Surface Leveling Means Plumb Composite Bulkhead Surface Minimum Crew 1 pilot (Front seat) Number of Seats 2 (43.3 in. (1.1 m) and 78.7 in. (2.0 m) aft of datum) Maximum Baggage 73 lbs. (33 kg) total in baggage area behind rear seat at 98.4 in. (2.5 m) aft of datum Fuel Capacity T otal capacity: 34 gal. (129 liters) Usable fuel in the system: 30 gal. (113.5 liters) Unusable fuel in the system: 4 gal. (15 liters) Oil Capacity Minimum 4 qts (3.78 liters) Maximum 8 qts (7.57 liters) Maximum Operational Altitude 11500 ft (3505 m) Density altitude Control Surface Movements Aileron 14°±1° upward 13°±1° downward Elevator 25°±1° upward 8°±1° downward Trim tab 4°±1° upward 30°±2° downward Rudder 25°±2° left 25°±2° right Flap Take-off: 15°±1° Landing: 30°±2° Serial Numbers Eligible Each individual aircraft manufactured under this type certificate mus t be accompanied by a n Export C ertificate of Airworthiness as noted below under “Import Requirements” when an application for a U.S. airworthiness certificate is made. Model BK 160-200 - serial number XXX and subsequent Import Requirements A U.S. airworthiness certificate may be issued on the basis of the Italian Certificate of Airworthiness for Export signed by a representative of the Italian Civil Aviation Authority (ENAC) on behalf of the European Community, containing the following statement: ‘The aircraft covered by this certificate has been examined, and found to comply with U.S. 14 CFR Part 21.17(b) covered under U.S. Type Certificate No. A00080CE and to be in a condition for safe operation.’ Refer to the applicable bilateral agreement to verify eligibility for import into the United States of both new and used aircraft based on the scop e of the agreement, to identify any required statements by the exporting authority on the export certificate of a irworthiness (or equivalent document), and for procedures for coordinating exceptions to conformity statements on these documents. Refer to FAA Order 8130.2, Airworthiness Certification of Aircraft, for requirements for issuance of an airworthiness certificate for imported aircraft. Certification Basis 14 Code of Federal Regulations (CFR) part 21 § 21.29, § 21.183(c) and Special Class provisions of § 21.17(b) -- 1) EASA CS-VLA, Amendment 1, dated March 5, 2009 and additional requirements adopted by the FAA and identified in FAA “Policy for Type Certification of Very Light Airplanes as a Special Class of Aircraft” (88 FR 70344, October 11, 2023) for Advanced Avionic Displays, Night-VFR Operations, Increased Maximum Certificated Takeoff Weight and Increased Stall Speed, and Rechargeable Lithium Ion Battery. Page 3 of 4 A00080CE BK 160-200 specific airworthiness criteria issued February 16, 2024, and published in Docket No. FAA-2022-1135 in Federal Register 89 FR 37, February 23, 2024. Additional Requirements for Advanced Avionic Displays for this model: 14 CFR part 23 § 23.1307 at amendment 23-49, “Miscellaneous Equipment”. 14 CFR part 23 § 23.1311 at amendment 23-62, “Electronic Display Instrument Systems” 14 CFR part 23 § 23.1321 at amendment 23-49, “Arrangement and visibility” 14 CFR part 23 § 23.1359 at amendment 23-49, “Electrical System Fire Protection”. Additional Requirements for Night-VFR Operations. (88 FR 70344, October 11, 2023): VLA.005, VLA.010, VLA.015, VLA.020, VLA.025, VLA.030, VLA.035, VLA.040, VLA.045, VLA.050, VLA.055, VLA.060, VLA.065, VLA.070, VLA.075, VLA.080, VLA.085, VLA.090, VLA.095, VLA.100, VLA.105 Additional Requirements for Increased maximum Certificated Takeoff Weight and Increased Stall Speed. (88 FR 70344, October 11, 2023): VLA.110, VLA.115, VLA.120, VLA.125, VLA.130, VLA.135, VLA.140, VLA.145, VLA.150, VLA.155, VLA.160, VLA.165, VLA.170, VLA.175, VLA.180, VLA.185, VLA.190, VLA.195, VLA.200, VLA.205, VLA.210 Additional Requirements for Rechargeable Lithium Ion Battery. (88 FR 70344, October 11, 2023): V LA.215 2) 14 CFR Part 36 effective November 18, 1969, including Amendments 36-1 through 36-31 3) No Special Conditions 4) No Equivalent Level of Safety 5) No Exemptions 6) Approved for Day-Night VFR only. 7) Airplane is not approved for flight into known icing or forecasted icing. Type Certificate No. A00080CE was issued June 21, 2024 Date of Application for Type Certificate was January 15, 2020. Production Basis. No FAA production certificate. BK 160-200 airplanes, all serial numbers, are produced under production approval Ref. IT.21G.0051, issued by the Italian aviation authority ENAC. Equipment The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) must be installed in the aircraft for airworthiness certification. In addition, the following items of equipment are required: Ref.: Section 6 of BK 160-200 FAA approved Airplane Flight Manual Doc. No. BCV-00-38-06 Revision 1, dated June 14, 2022, or later EASA (on behalf of FAA) approved revision. Service Information Each of the documents listed below must state that it is approved by the European Union Aviation Safety Agency (EASA): Page 4 of 4 A00080CE • Service bulletins, • Structural repair manuals, • Vendor manuals, • Aircraft flight manuals, and • Overhaul and maintenance manuals. The FAA accepts such documents and considers them FAA-approved for type design data only unless one of the following conditions exists: • The documents change the limitations, performance, or procedures of the FAA approved manuals; or • The documents make an acoustical or emissions changes to this product’s U.S. type certificate as defined in 14 CFR § 21.93. The FAA uses the post type validation procedures to approve these documents. The FAA may delegate on case-by-case to EASA to approve on behalf of the FAA for the U.S. type certificate. If this is the case it will be noted on the document. Available documents for the BK 160-200 are: Aircraft Flight Manual: • Blackshape BK 160-200 Doc. No. BCV-00-38-06 Revision 1, dated June 14, 2022, or later approved revisions. (NOTE 2) Instructions for Continued Airworthiness (ICA): • Airplane Maintenance Manual (AMM) Document Blackshape BK 160-200 Doc. No. BCV-00-39-02 Revision 2, dated January 19, 2023, or later approved revisions. (NOTE 3) NOTES NOTE 1. A current weight and balance report including 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. The certificated empty weight and corresponding center of gravity location must include full oil and unusable fuel. NOTE 2. All required placards are contained in Chapter 2 of the Airplane Flight Manual (AFM) No. BCV-00-38-06 Revision 1, dated June 14, 2022, or later approved revisions and must be installed in the appropriate locations. Revisions to this report may be approved by EASA on behalf of the FAA, unless they are changes to the limitation section. These changes require FAA approval for the US version. NOTE 3. Instructions for Continued Airworthiness and Service Life Limited components is included in the Airplane Maintenance Manual Doc. No. BCV-00-39-02 Revision 2, dated January 19, 2023. All revisions to the Airworthiness Limitations Section must be approved by both the EASA and the FAA. – END –