TYPE CERTIFICATE DATA SHEET No. A00066CE

• 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: A00066CE Page 4 of 5 • 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. Each airplane is provided with the following approved documents: a) AFM doc. 2010/100 Ed. 2, Rev. 0, or later FAA approved revision. b) Airplane Maintenance Manual (AMM) doc. 2010/101 Ed. 1, Rev. 2, or later FAA approved revision, including Chap. 4: "Airworthiness Limitations" and Chap. 5: "Time Limits/ Maintenance Check". c) The appropriate Lycoming series engine maintenance manuals. d) The appropriate MT Propellers Instruction Manual. NOTES NOTE 1 Current weight and balance 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. The certificated empty weight and corresponding center of gravity location must include: Unusable fuel: 14.28 lbs at 24.1 in aft of datum NOTE 2 Airplane operation must be in accordance with the EASA approved AFM listed above. All placards listed in Section 2 must be displayed. NOTE 3 Airworthiness Limitations are specified in the Section 2 LIMITATIONS of the AFM and Chapter 4 of the AMM and are approved by EASA and the FAA. These LIMITATIONS specify mandatory replacement times, and operating limitations, and may not be changed without FAA approval. Revisions to the Airworthiness Limitations must be approved by the FAA. The inspections, maintenance, repair and painting must be accomplished according to the Maintenance Manual or other procedures acceptable to the FAA. NOTE 4 Information essential for the proper operation, maintenance and inspection of the airplane is contained in the Tecnam P2010 AFM and AMM. NOTE 5 Optional Variable Pitch Propeller Tecnam Modification No. MOD2010-002 (Variable Pitch Propeller - MTV-15-B/193-52 (TC P23BO)). Airplanes with this modification must have at least Tecnam AFM doc. 2010/100 Ed. 2, Rev. 0, Supplement No. D-2 or later FAA/EASA approved revisions and Tecnam P2010 AMM Supplement No. S-1, Ed. 1, Rev. 0, or later FAA/EASA approved revisions. NOTE 6 Optional GFC 700 Autopilot Tecnam Modification No. MOD2010-001 (Garmin GFC 700 Autopilot). Airplanes can be modified by Tecnam at the factory under their major level 1 type design change approval. Airplanes with this modification must have Tecnam AFM Section 9 Supplement No. D01, Ed. 1, Rev. 0 (Aircraft equipped with fixed pitch propeller), or AFM Section 9 Supplement No. D07, Ed. 1, Rev. 0 (Aircraft equipped variable pitch propeller), or later FAA/EASA approved revisions and Tecnam P2010 AMM Supplement No. S-3, Ed. 1, Rev. 0, or later FAA/EASA approved revisions. Aircraft in service can incorporate this modification using Tecnam Service bulletin SB -180-CS (Aircraft equipped with fixed pitch propeller) or Tecnam Service bulletin SB -220-CS(Aircraft equipped with variable pitch propeller). A00066CE Page 5 of 5 NOTE 7 Alternative Avionics Configuration Tecnam Modification No. MOD2010-003 (Alternative Avionics Configuration – Garmin G500). This modification cannot be installed as retrofit. Airplanes can be modified by Tecnam at the factory under their major level 1 type design change approval. Airplanes with this modification must have Tecnam AFM Section 9 Supplement No. D03, Ed.1, Rev. 0, or later FAA/EASA approved revisions and Tecnam P2010 AMM Supplement No. S-2, Ed.1, Rev. 0, or later FAA/EASA approved revisions. NOTE 8 Optional Automotive Fuel Tecnam Modification No. MOD2010-032 (Automotive Fuel-MOGAS). Airplanes can be modified by Tecnam at the factory under their major level 1 type design change approval. Airplanes with this modification must have Tecnam AFM Section 9 Supplement No. D04, Ed. 1, Rev 0, or later FAA/EASA approved revisions. Aircraft in service can incorporate this modification using Tecnam Service bulletin SB -182-CS. NOTE 9 Optional Engine and Avionic Suite Tecnam Modification No. MOD2010/078 (Lycoming IO-390 Engine and G1000Nxi avionic suite installation). This modification cannot be installed as a retrofit. Airplanes with this modification must have Tecnam AFM Supplement No. D10, Ed. 2, Rev. 1 or later FAA/EASA approved revisions and Tecnam P2010 AMM Supplement No. S6, Ed. 1, Rev. 1, or later FAA/EASA approved revisions. NOTE 10 Optional GFC 700 Autopilot for Airplanes Equipped with IO390 Engine Tecnam Modification No. MOD2010/133 (Garmin GFC 700 Autopilot for IO390-Equipped Airplanes). Airplanes with this modification must have Tecnam AFM Section 9 Supplement No. D16, Ed. 2, Rev. 0, or later FAA/EASA approved revisions and Tecnam P2010 AMM Supplement No. S12, Ed. 1, Rev. 1, or later FAA/EASA approved revisions. Aircraft in service can incorporate this modification using Tecnam Service bulletin SB -308-CS. - END -