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General| Type | Light Sport Aircraft |
|---|---|
| Manufacturer | Zenith Aircraft Company |
| Engine | Rotax 912ULS |
| Seating Capacity | 2 |
| Seats | 2 |
| Horsepower | 100 hp (75 kW) |
| Rate of Climb | 1, 000 ft/min (5.1 m/s) |
| Crew | 1 |
| Capacity | 1 passenger |
| Stall Speed | 39 mph (63 km/h) |
| Maximum speed | 120 mph (193 km/h) |
Table detailing revisions made to the flight manual.
Provides an overview of the flight manual's purpose and content for homebuilt aircraft.
Details the aircraft's authorization for flight under specific regulations, not standard airworthiness.
Defines the meaning of warning, caution, and note symbols used throughout the manual.
Provides physical specifications, dimensions, weight, and performance data of the aircraft.
Illustrates the aircraft's dimensions and configuration from multiple viewpoints.
Introduces operating limitations, instrument markings, and placards for safe aircraft operation.
Details airspeed limitations and their operational significance for safe flight.
Explains the color-coded markings on the airspeed indicator and their significance.
Provides detailed specifications and operating limits for the aircraft's engine and related systems.
Describes the color-coded markings on powerplant instruments for safe operation.
Details markings for electrical instruments like voltage and ammeter.
Specifies the maximum take-off, landing, and baggage weights for the aircraft.
Defines the datum reference and forward/aft CG limits for safe operation.
Lists maneuvers the aircraft is approved for and prohibits aerobatics and spins.
Specifies the positive and negative load factors allowed with flaps up and extended.
Specifies the minimum flight crew requirement for operating the aircraft.
Defines the approved operational category, VFR day operation only.
Details tank capacity, usable fuel, and approved fuel grades.
States the maximum number of passengers the aircraft can accommodate.
Specifies additional operational limitations, such as service ceiling.
Lists various placards found inside and outside the aircraft for identification and warnings.
Introduces procedures for coping with emergencies, emphasizing pre-flight inspections.
Provides checklists and procedures for engine failure during takeoff, after takeoff, and during flight.
Details procedures for attempting an engine air start after failure.
Outlines procedures for handling engine/fuel smoke and fire on ground and in flight.
Describes establishing best glide speed and actions after engine failure in flight.
Covers precautionary landings, forced landings, zero flaps, and flat tire landings.
Provides instructions for recovering from an unintentional spin.
Addresses carbon monoxide alerts and electrical system failures.
Introduces procedures for the normal conduct of aircraft operation.
Information regarding the assembly and disassembly of the aircraft.
Procedures for daily checks of the aircraft.
Detailed walk-around checklist for inspecting the aircraft before flight.
Checklists for pre-flight, engine start, taxi, run-up, takeoff, climb, cruise, descent, approach, and landing.
Introduces approved data for airspeed calibration, stall speeds, and takeoff performance.
Provides data for calibrating the airspeed indicator based on flight tests.
Lists stall speeds for power off and power on conditions with different flap settings.
Presents ground run and distance over obstacle data for takeoff at various conditions.
Provides ground run and distance over obstacle data for landing at various conditions.
Graph and data showing rate of climb versus density altitude.
Details cruise speed, fuel consumption, and range at different power settings.
Provides endurance and range data based on fuel capacity and power settings.
Details demonstrated crosswind capabilities of the aircraft.
Introduces payload range, weighing procedures, and calculation methods.
Details the reference datum, horizontal reference, and procedures for weighing the aircraft.
Records the empty weight CG, including itemized weights, arms, and moments.
Defines maximum gross weight, CG limits, and sample calculations for payload.
Lists all installed equipment, including powerplant, landing gear, and avionics.
Introduces the description and operation of the airplane and its systems.
Details the all-metal construction, fuselage, and wing design of the aircraft.
Describes the Y-control stick, rudder pedals, flaperons, and pitch trim system.
Identifies instruments and controls on the main panel, middle console, and control sticks.
Describes the main gear, nose gear, and their suspension systems.
Details the side-by-side seating, ventilation, cabin heater, and harness system.
Describes the location, capacity, and securing of baggage.
Details the operation of the aircraft doors, including hinges and latches.
Describes the Rotax 912 ULS engine, its features, and propeller.
Explains the fuel tanks, shutoff valve, fuel pump, and check valves in the system.
Details the 12V battery system, fuses, breakers, and essential bus components.
Describes the Pitot/AOA tube, ADAHRS, and static pressure ports.
Details the ACK E-04 ELT and Smartwaves RM386 CO2 Detector.
Describes the Dynon Avionics Skyview system, VHF COM, and Transponder.
Recommends procedures for ground handling, servicing, and maintenance requirements.
Refers to the Maintenance Manual for details on airplane inspection periods.
Stipulates contacting EAS for alterations and repairs to ensure airworthiness.
Covers taxiing, propeller blast, pulling/pushing, parking, and tie-down procedures.
Provides instructions for cleaning frontal surfaces, windows, and doors.
Details connecting ground power for battery charging and avionics programming.
Introduces supplements for operating the airplane with optional systems and equipment.
A table for recording details of inserted supplements, including affected sections and pages.
Guidelines for supplement content, approval by EAS, and required sections.
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