# TCDS A00122IB: Elixir Aircraft - Type: Type certificate data sheet - Status: Current - Holder: Elixir Aircraft - Revision: 4 - Revised: September 25, 2026 - Product: Aircraft, Small Airplane - Certification basis: Part 23, Part 21, Part 21 - Registered aircraft: 3, by the registry models matched to it (OpenAirDocs) - Data sheet PDF: https://openairdocs.org/files/sha256/9e/5b/9e5b4f92767cc624857a4d995110bdd830879046376d53abd52424cbd08ad0ec - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID116898978320260925175826.0001 - Page: https://openairdocs.org/tcds/A00122IB ## Models (1) As the data sheet lists them. - Elixir ## 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 Rev. No. 4 3 4 4 DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A00122IB Revision 4 ELIXIR AIRCRAFT Elixir September 25, 2026 TYPE CERTIFICATE DATA SHEET No. A00122IB This Data Sheet, which is part of Type Certificate No. A00122IB, 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 ELIXIR AIRCRAFT Rue du Jura 17000 La Rochelle France I. Model Elixir (Normal Category), Approved July 22, 2025 Engine One Rotax 912 iSc3 Sport Engine (TC E00051EN) Fuel AVGAS 100LL or 100VLL (ASTM D910) AVGAS UL91 or UL94 (ASTM D7547) Engine Limits For Rotax 912 iSc3 Sport Engine: Maximum Power, 100 hp @ 5,800 rpm (5 min) Maximum Continuous Power, 97 hp @ 5,500 rpm Propeller and Propeller Limits MT Propeller MTV-34-1-A/156-203 (TC P00038BO) Three blades, constant speed, variable pitch, wood composite Diameter: 61,4 in (1560 mm) Clockwise rotation (pilot’s view) Airspeed Limits KIAS KCAS VA (Design Maneuvering Speed) 123 122 VFE (Maximum Flap Extended Speed) 88 87 Flap T/O 88 87 Flap LAND VNO (Maximum Structural Cruising Speed) 136 135 VNE (Never Exceed Speed) 156 155 Center of Gravity (C.G.) Range Mean Aerodynamic Chord (MAC) = 36.3 in (0.922 m) Forward limit: 29.76 in (0.756 m) (28% MAC) aft of datum up to 1,287 lb (584 kg) 32.28 in (0.820 m) (33% MAC) aft of datum for MTOW Aft Limit: 33.86 in (0.860 m) (39% MAC) aft of datum up to 1,543 lb (700 kg) Empty Weight C.G. Range None Datum Firewall (the aircraft must be levelled in the longitudinal plane) Levelling Means Refer to the seat track supporting beams (See Aircraft Flight Manual (AFM), Document No. LXR-AI-REC-Manual – Aeroplane Flight Manual – Elixir B - Full A00122IB Page 2 of 4 Glass Cockpit – 0003030, Section 6 for the procedure) Maximum Weight Take-off 1543 lbs (700 kg) Landing 1543 lbs (700 kg) Minimum Crew 1 Pilot Number of Seats 2 Baggage/Cargo Compartments Weight Maximum 55 lbs (25 kg) Fuel Capacity Total (1 tank): Useable (total): 27.5 U.S. Gal. (104 L) 26.4 U.S. Gal. (100 L) Oil Capacity Maximum: 3.70 U.S. Qts (3.5 L) plus the volume in the pipe Minimum: 3.22 U.S. Qts. (3.05 L) plus the volume in the pipe Maximum Operating Altitude 16000 ft (4877 m) Control Surface Movements (*) Ailerons 21°±1° TEU (**); 14°±1° TED (***) Ailerons trim tab (****) 17°-0°/+3° TEU; 17°-0°/+3° TED Stabilator 5.0°±0.2° TEU; 6.5°±0.5° TED (Flap Cruise position) 7.0°±0.2° TEU; 6.5°±0.5° TED (Flap Take-off position) 7.5°±0.2° TEU; 6.5°±0.5° TED (Flap Landing position) Stabilator trim tab (*****) 0°±1° TEU; 17°±1° TED Rudder Reach the built-in, non-adjustable control stops on both sides Flaps 0° -0°/+1° TED (Cruise position) 20°±1° TED (Take-off position) 41°-1°/+0° TED (Landing position) (*) Nominal Values (**) Trailing Edge Up (***) Trailing Edge Down (****) with Ailerons set 0° (*****) with Stabilator set 0° Manufacturer’s Serial Numbers MSN054 – B – N and subsequent Serial numbers with the letter “-N” are the only aircraft eligible for United States standard airworthiness certificates per the US type certificate. (NOTE 5) Import Requirements A U.S. airworthiness certificate may be issued on the basis of an NAA Export Certificate of Airworthiness (Export of C of A) signed by a representative of the Direction Générale de l’Aviation Civile (DGAC) on behalf of the European Community. The Export C of A should contain the following statement "The aircraft covered by this certificate has been examined, tested, and found to comply with U.S. Type Certificate No. A00122IB and to be in a condition for safe operation." Title 14 CFR § 21.183 (c) is the U.S. airworthiness certification basis for an aircraft type certificated under 14 CFR § 21.29 and imported from the country of manufacture. Refer to the applicable bilateral agreement to verify eligibility for import into the United States of both new and used aircraft based on the scope of the agreement, to identify any required statements by the exporting authority on the export certificate of A00122IB Page 3 of 4 airworthiness (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 Type Certification under 14 CFR Section 21.29 including the following requirements: 1. 14 CFR Part 23 effective February 1, 1965, including amdt 23-1 through 23- 65, “Airworthiness Standards: Normal Category Airplanes.” a. § 23.2005 Certification Level and Performance Level: Level 1, Low Speed b. The detailed design standards used as a means of compliance in accordance with § 23.2010 are documented in 0003048, Elixir Detailed Design Standard Summary - R01, dated September 8, 2025 2. 14 CFR Part 36 effective December 1, 1969, including amdt 36-1 through 36-32 3. Equivalent levels of safety (ELOS): None 4. Special Conditions: None 5. Exemptions: None 6. Approved Kinds of Operation: Day, Visual Flight Rules (VFR) only 7. Prohibited Kinds of Operation: Night, Visual Flight Rules (VFR) Instrument Flight Rules (IFR) Flight into known icing conditions 8. The airplane is not approved for ditching Type Certificate No. A00122IB issued July 22, 2025. Date of Application for FAA Type Certificate was July 13, 2021, amended to July 14, 2024. The European Aviation Safety Agency (EASA) originally type certified this aircraft under its type certificate number EASA.A.633. Equipment The basic required equipment as prescribed in the applicable airworthiness regulations (see Certification Basis) must be installed in the airplane for certification. In addition, the following item of equipment is required: • AFM, Document No. LXR-AI-REC-Manual – Aeroplane Flight Manual – Elixir B - Full Glass Cockpit – 0003030, Ed 00, Rev 03, dated July 22, 2026, or later approved revision, for the Model Elixir. Service Information Each of the documents listed below must state that it is approved by EASA: • Service bulletins, • Structural repair manuals, • Vendor manuals, • Aircraft flight manuals, and • Overhaul and maintenance manuals. A00122IB Page 4 of 4 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 Model Elixir: • AFM, Document No. LXR-AI-REC-Manual – Aeroplane Flight Manual – Elixir B - Full Glass Cockpit – 0003030, Ed 00, Rev 03, dated July 22, 2026, or later approved revision. • Airplane Maintenance Manual (AMM), Document No. LXR-AI-REC- Manual-Aircraft Maintenance Manual – 0001392, Issue 02 Rev 05 dated April 15, 2026, or later approved revision. • The appropriate Rotax 912 iSc3 Sport Engine maintenance manuals. • 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: 6.34 lbs (2.88 kg) at 30.5 in (0.774 m) aft of datum Unusable oil: 4.7 lbs (2.13 kg) at 34.1 in (0.866 m) fwd of datum NOTE 2 Airplane operation must be in accordance with the FAA approved AFM listed above. All placards listed in Section 2 Limitations must be installed as specified. The AFM Limitations are EASA and FAA approved and may not be revised without EASA and FAA approval. NOTE 3 Limitations are specified in the Section 2 Limitations of the AFM and Chapter 4 AIRWORTHINESS LIMITATIONS 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 EASA and FAA approval. NOTE 4 Information essential for the proper operation, maintenance and inspection of the airplane is contained in the Elixir AFM and AMM. NOTE 5 Aircraft Manufacturer Serial Number designation: MSNXXX – B – N MSNXXX: Elixir Type Serial Number -B: Technical configuration - Elixir with a maximum take-off weight of 1543lbs (700kg) – technical designation “Elixir B” -N: Regional configuration – Only aircraft eligible for United States standard airworthiness certificates per the US type certificate. --- END --- ``` ## ADs (1, in force first) - [AD 2026-21-01](https://openairdocs.org/ad/2026-21-01): Prohibited Operation · Elixir Elixir. Effective Oct 14, 2026 ## Registered aircraft by registry model (OpenAirDocs) - [Elixir ELIXIR](https://openairdocs.org/model/elixir-elixir): 3 aircraft (registry code 2130050) --- 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.