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General| Manufacturer | Aeroprakt |
|---|---|
| Model | A32 |
| Category | Light Sport Aircraft |
| Engine | Rotax 912ULS |
| Horsepower | 100 hp |
| Seating Capacity | 2 |
| Takeoff Distance | 150 m (492 ft) |
| Landing Distance | 150 m (492 ft) |
| Service Ceiling | 4, 000 m (13, 123 ft) |
| Maximum Takeoff Weight | 600 kg |
| Range | 1, 000 km (621 mi) |
| Gross Weight | 600 kg |
| Fuel Capacity | 100 liters |
| Stall Speed | 65 km/h |
Purpose of the handbook for safe and efficient airplane operation.
List of ASTM standards used for design, construction, and airworthiness.
Details of the aircraft manufacturer and support contacts.
Overview of the Aeroprakt-32 (A-32) design, layout, and certification.
Key physical and performance specifications of the aircraft.
Airspeed limitations, indicator markings, and their meanings.
Maximum altitude the aircraft can operate at.
Limit load factors for the airplane at gross weight.
Description of permitted maneuvers and prohibited aerobatics.
Details on fuel tank capacity, usable fuel, and approved fuel types.
Operational data and limitations for the Rotax engine.
Approved flight conditions and prohibited operations.
Maximum allowable crosswind component.
General recommendations for emergency situations.
Specific checklists for various emergency scenarios.
Procedure for handling engine failure while flying level.
Steps to restart the engine in flight.
Procedure for forced landing due to engine failure.
Procedure for a precautionary landing with the engine running.
Steps to take in case of a fire in flight.
Procedure for handling loss of engine oil pressure.
Procedure for handling high engine oil pressure.
Steps for performing an emergency descent.
Procedure for handling alternator failure.
Procedure for handling electrical system overvoltage.
Procedure for recovering from an inadvertent spin.
Procedure for handling unexpected icing conditions.
Procedures for handling failure of key flight instruments.
Procedure for handling failure of engine instruments.
Procedures for handling loss of primary flight controls.
General description of normal procedures for safe operation.
Detailed steps for performing the preflight inspection.
Inspection details for the right wing and its components.
Inspection details for the right side of the fuselage.
Inspection details for the tail section.
Inspection details for the left side of the fuselage.
Inspection details for the left wing and its components.
Inspection of cockpit interior, seats, belts, doors, and instruments.
Step-by-step guide for starting the aircraft engine.
Steps for taxiing the aircraft on the ground.
Final checks before commencing takeoff.
Detailed steps for a standard takeoff.
Procedure for takeoff from short or soft runways.
Procedures for climbing after takeoff.
Procedures for maintaining cruise flight.
Procedures for approaching the landing area.
Detailed steps for a standard landing.
Procedure for landing on short or soft runways.
Procedure for aborting a landing.
General notes on performance data conditions and variability.
Minimum takeoff and landing distances under standard conditions.
Data on climb rate and speed.
Table of cruise speeds and fuel burn at different engine RPMs.
Weighing data, CG location, and calculation examples.
CG position calculation for maximum takeoff weight.
Table for listing installed optional equipment affecting weight and balance.
General overview of aircraft systems and optional equipment.
Detailed description of wing, fuselage, and tail construction.
Detailed description of the tricycle landing gear.
Description of the Rotax engine and its control systems.
Information regarding approved propellers for the aircraft.
Description of the all-flying horizontal tail control system.
Description of the system for controlling pitch forces.
Description of the rudder and nose wheel steering system.
Description of the system for controlling flaperons as ailerons and flaps.
Description of engine RPM, choke, and carburetor heating controls.
Procedure for operating the carburetor heating system.
Description of the hydraulic brake system and parking brake.
Arrangement and identification of flight instruments and controls.
Detailed identification of instruments, switches, and placards on the panel.
Description of the system supplying air pressure to instruments.
Description of power generation, storage, and distribution.
Block diagram of the Garmin G3X avionics system installation.
Wiring diagram details for the Garmin G3X system.
Wiring diagram details for the Garmin G3X system.
Wiring diagram details for the Garmin G3X system.
Wiring diagram details for the Garmin G3X system.
Wiring diagram details for the Garmin G3X system.
Wiring diagram details for the Garmin G3X system.
Wiring diagram for Push-To-Talk button installation.
Wiring diagram for the Artex ELT 345 installation.
Description of seat adjustment and 4-point harness belt system.
Description of the cockpit doors, hinges, and locking mechanism.
Description of the baggage compartment volume and weight limit.
Description of the parachute recovery system installation and deployment.
Guidelines for safely moving, parking, and securing the aircraft.
Procedures for checking and servicing aircraft fluids.
Specifications for approved fuel and oil types.
Recommendations for cleaning and maintaining the aircraft.
Procedures for removing and reinstalling major aircraft components.
Detailed steps for removing the aircraft wings.
Detailed steps for removing the all-flying horizontal tail.
Steps for safely removing the aircraft propeller.
Steps for safely removing the aircraft engine.
Procedure for reassembling the aircraft after disassembly.
Table for listing installed equipment and their details.
Recording actual empty weight and CG position after modifications.
Training on preflight checks, takeoff mass, and CG position determination.
Training on airfield traffic and flight characteristics to training area.
Familiarization with flight elements, takeoff, and landing in circuit.
Training on taxiing, circuit flying, and specific maneuvers.
Training on handling balked landing situations.
Training on low speed handling, stall recognition, and recovery.
Training on high speed handling and steep spiral recovery.
Training on short field takeoff and landing with obstacles.
Training on takeoff and landing in crosswind conditions.
Training on handling simulated engine failures.
Process for reporting operational safety issues to the manufacturer.
