TCDS A00034LA

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET No. A00034LA This data sheet, which is part of Type Certificate No. A00034LA, prescribes conditions and limitations under which the product for which the type certificate was issued meets the airworthiness requirements of Title 14 of the Code of Federal Regulations (Title 14 – Aeronautics and Space). Type Certificate Holder ICON Aircraft, Inc. 2141 ICON Way Vacaville, CA 95688 Page No. 1 2 3 4 Rev. No. 0 0 0 0 I. MODEL A5-B (PRIMARY CATEGORY) - APPROVED DECEMBER 20, 2023 ENGINE Rotax 912iSc2 Sport CONFIGURATION Fixed Wing FUEL Unleaded automotive fuel with up to 10% maximum ethanol content meeting ASTM D4814 with minimum RON 95 (minimum Anti-Knock Index 91) Grade 100LL aviation gasoline (AVGAS) meeting ASTM D910 OIL Viscosity—SAE 10W-40 multi-grade API classification SG or higher The FAA Approved PILOT’S OPERATING HANDBOOK, ICA014866, Issue A3, dated August 31, 2023, or later FAA Approved Revision, identifies types of oils and additives that may damage the engine. A00034LA Rev. 0 ICON Aircraft, Inc. A5-B December 20, 2023 A00034LA Page 2 of 4 COOLANT The engine coolant must be a mixture of 50% ethylene glycol based antifreeze and 50% distilled water. The antifreeze portion of the coolant mixture should be a low silicate and nitrite-free formula. See FAA Approved PILOT’S OPERATING HANDBOOK, ICA014866, Issue A3, dated August 31, 2023, or later FAA Approved Revision, for a list of approved coolants. ENGINE LIMITS One Rotax 912iSc2 Sport, 4-stroke, 4-cylinder horizontally opposed, spark ignition. Maximum Rated Power at Sea Level, Standard Day 100 hp at 5,800 RPM. NOTE: Per the Rotax Manual, the engine should only be run at this setting for a maximum of 5 minutes. Maximum Continuous Power 97 hp at 5,500 RPM PROPELLER Sensenich, 3-blade propeller, 3B0R5-L68CS NOTE: Although the propeller is ground adjustable, ICON does not permit propeller pitch adjustments. Speed Limitation: 5,800 RPM AIRSPEED LIMITS SPEED KIAS REMARKS VS0 Stall Speed, MTOW, Flaps 30° 39 Idle power VS Stall Speed, MTOW, Flaps 0° 45 Idle power VFE and VLE Maximum Flap and Landing Gear Extended Speed 75 Operation and extended speeds are the same. VO-min Operating Maneuvering Speed, 1,145 lbs., Min Flight Weight 76 Do not make full or abrupt control movements above this speed. VO-max Operating Maneuvering Speed, MTOW 87 Do not make full or abrupt control movements above this speed. VN0 Max Structural Cruising Speed 95 Do not exceed this speed except in smooth air. VNE Never Exceed Speed 120 Do not exceed this speed in any operations. A00034LA Page 3 of 4 WEIGHT AND CG ENVELOPE LIMITS REFERENCE DATUM FS 154.75 (located on forward face of wing spar carry-through). LEVELING MEANS The A5-B weight and balance can be established using two different methods. The first (and more accurate) method uses three jack points—one on each wing and one under the tail skid. The second method uses the aircraft on its landing gear—two main wheels and the nose wheel. In both methods, the aircraft is leveled by use of a built-in bubble level located under the passenger floorboard panel. MAXIMUM WEIGHT 1,51 0 lbs. MINIMUM CREW 1 Pilot NUMBER OF SEATS 2 Seat Moment Arms 128.5 in. MAXIMUM BAGGAGE 60 lbs. FUEL CAPACITY Total Fuel Capacity 20.1 US Gallons Total Usable Fuel 20 US Gallons OIL CAPACITY 0.94 Gallons MAXIMUM OPERATING- 15,000 ft at MTOW, standard conditions ALTITUDE A00034LA Page 4 of 4 CONTROL SURFACE MOVEMENTS Ailerons: 25 deg TE up, 15 deg TE down Flaps: 0 deg, 15 deg, 30 deg Elevator: 19 deg TE up, 21 deg TE down Rudder: 11 deg TE left, 14 deg TE right SERIAL NUMBERS 00001-99999 CERTIFICATION BASIS 14 CFR Sections 21.17(f) and 21.24 FR Doc. 2023–27835 Date of Application for TC: August 3, 2020 Date of TC Issuance: December 20, 2023 PRODUCTION BASIS None EQUIPMENT There is no optional equipment that replaces required or standard equipment. Specified Optional Equipment for the Aircraft: NOTES: NOTE 1. Current weight and balance data, loading information and a list of equipment included in empty weight must be provided for each airplane at the time of original certification. NOTE 2. All Placards required in the FAA Approved PILOT’S OPERATING HANDBOOK, ICA014866, Issue A3, dated August 31, 2023, or later FAA Approved Revision, must be installed in the appropriate location. NOTE 3. The type design of the ICON Aircraft, Inc., A5-B, is defined by FAA Approved Master Drawing List, ICA015689, Revision A, dated March 10, 2023, or later FAA Approved Revision. END ID Name Weight (lbs) Arm (in) 001 ICON Parachute System (IPS) 35.7 161.8