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General| Manufacturer | Pipistrel |
|---|---|
| Seats | 2 |
| Engine Power | 80 hp |
| Wingspan | 15 m (49.2 ft) |
| Model | Sinus 912 LSA |
| Range | 1, 200 km (746 miles) |
Provides essential information for the appropriate and safe use of the Sinus 912 LSA aircraft.
Details the aircraft's key proportions, including wing span, length, height, and surface areas.
Presents a multi-view diagram of the aircraft with key dimensions indicated.
Outlines engine specifications, operating temperatures, RPM, fuel type, and oil capacity.
Lists aircraft weights including empty, takeoff, useful load, and baggage allowance.
Specifies the safe center of gravity position ranges in percentage of mean aerodynamic chord.
Defines the maximum positive and negative wing loads the aircraft can withstand.
Covers operating limitations, instrument markings, and basic placards for safe aircraft operation.
Details critical airspeeds such as stall speeds, VNE, VNO, and maneuvering speeds.
Specifies operating limits for the engine, including temperature, pressure, and fuel/oil recommendations.
Defines the maximum takeoff weight and combined cockpit crew weight limits.
Specifies the limitations regarding the number of occupants in the cockpit.
Details the acceptable range for the aircraft's center of gravity.
States the maximum positive and negative G-loads the aircraft structure can handle.
Explains how service ceiling affects VNE and the need for IAS to TAS correction.
Defines permitted non-aerobatic maneuvers and prohibits aerobatic maneuvers.
Specifies approved operations (DAY-NIGHT-VFR) and prohibits flight in known icing.
Lists essential equipment required for DAY-VFR and NIGHT-VFR operations.
Prohibits flight in adverse weather, IFR conditions, and specific operational restrictions.
Illustrates various placards found in the cockpit related to aircraft operation and safety.
Provides information for coping with emergencies, emphasizing preflight checks and judgment.
Outlines the procedure to recover from a stall by reducing angle of attack and adding power.
Details steps for recovering from a spin, including throttle, rudder, and stick inputs.
Covers procedures for engine failure during takeoff or in flight, including restart attempts.
Provides steps for executing an emergency landing or landing off an airport safely.
Describes procedures for handling engine fires on the ground and in flight.
Addresses smoke in the cockpit, usually due to electrical issues, and landing procedures.
Explains signs of carburetor icing and procedures for dealing with it.
Covers procedures for handling failures in the electrical system or battery.
Defines flutter and outlines actions to take if control surfaces start vibrating.
Provides guidance on actions to take if the VNE airspeed is exceeded.
Outlines the emergency procedure for landing the aircraft in water.
Covers procedures for exiting icing conditions and handling pneumatic instrument failures.
Describes the daily check-up procedure, which matches the preflight inspection.
Details the mandatory preflight inspection steps for every flight.
Covers cabin entry, safety harness, pedal adjustment, and engine start-up.
Provides information on airspeed calibration, stall speeds, and general performance data.
Explains that IAS to CAS correction values are insignificant for this aircraft.
Lists stall speeds at MTOM with various flap configurations.
Details takeoff ground roll and runway length under specific conditions.
Provides data on best climb speed, best climb rate at MTOM, and climb rate at 100 kts.
Recommends cruise power, airspeed, and fuel burn at MTOM.
Describes typical sink rates with flaps and airbrakes, and procedures for unpowered flight.
Details final approach speed, landing roll, and runway requirements.
Specifies maximum allowed crosswind speed and runway length increase.
Explains procedures for establishing basic empty weight and moment of the aircraft.
Details the steps for weighing the aircraft and calculating its center of gravity.
Provides space to record installed equipment and its impact on weight and balance.
Shows how to determine the center of gravity (CG) based on weight and lever arms.
Illustrates the calculation of CG for tailwheel and nosewheel editions.
Describes the aircraft's construction, composite materials, and general features.
Identifies individual and joint control levers in the cockpit.
Shows different instrument panel configurations and notes on instruments.
Details the tricycle undercarriage, wheel dimensions, tire pressure, and brakes.
Describes the seats, their adjustability, and the standard H type safety harness.
Explains the attachment and routing of the pitot tube and lines.
Details the function and operation of air brakes for approach and descent.
Provides a description of the Rotax 912 UL 80 HP engine and its schematic.
Describes the fuel system, including tanks, selector valves, capacity, and filters.
Outlines the electrical system, battery, switches, and power consumption.
Explains the Rotax 912 UL engine cooling system, including air and water cooling.
Describes the engine lubrication system, including oil pump, radiator, and oil quantity.
Details the wheel brake system, including type, fluid, and parking brake.
Outlines inspections required after exceeding VNE or landing in rough conditions.
Provides procedures for draining the fuel system and refueling the aircraft.
Details how to connect auxiliary power for engine starting when the battery is weak.
Describes the procedure for tying down the aircraft for parking or storage.
Provides recommendations for storing the aircraft, including battery disconnection.
Offers guidelines for cleaning the aircraft's exterior and interior surfaces.
Offers advice on cleaning, polishing, and maintaining the aircraft's appearance.
Explains the operation, handling, and servicing of the parachute rescue system.
Discusses the importance of respecting airspeed limits, particularly VNE.
Addresses the misconception about control deflection limits below maneuvering speed.
Provides additional guidance for pilots learning to operate the Sinus 912 LSA.
Includes tables for converting between km/h, kts, m/s, and feet.
Illustrates key components for the preflight inspection.
Explains the purpose and importance of this supplemental sheet for tail-wheel edition.
Defines safety terms and explains markings used in the supplemental sheet.
Provides specific updates for tail wheel preflight check-up and related procedures.
