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Fiate Aviation MZ202 - User Manual

Fiate Aviation MZ202
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Summary

WARNING

Non-Aeronautic Approved Engine Warning

Engine not approved for aeronautic use; user assumes all risks and responsibility for failures.

INTRODUCTION

ENGINE DELIVERY

WARRANTY

IMPORTANT SAFETY TIPS

TECHNICAL SPECIFICATIONS

MZ202 FREE AIR PERFORMANCE DIAGRAM

MAIN TORQUE SETTINGS

OIL AND FUEL

HOW TO PREPARE YOUR FUEL;OIL MIXTURE

PRE-START PROCEDURES

STARTING UP ENGINE FOR THE FIRST TIME AND BREAK-IN

FINAL CHECK

START UP PROCEDURE

HOW TO USE THE ENGINE

ADJUSTING THE CARBURETOR

Choke and Idle Adjustment

Procedures for adjusting choke and idle settings on the carburetor.

Throttle Cable Adjustment

Adjusting throttle cable freeplay and synchronizing carburetors.

Choke Cable Adjustment

Setting the correct freeplay for the choke cable.

STOP PROCEDURE

THE GEAR DRIVE

Function of the Gear Drive

Explains the purpose and benefits of the engine's gear reduction system.

Choosing the Right Reduction

Details the type of gear reduction used and its advantages.

TROUBLESHOOTING

Engine Wont Start Troubleshooting

Lists probable causes and remedies for the engine failing to start.

Inconsistent Idle Troubleshooting

Identifies causes and solutions for irregular engine idling.

Irregular Engine Running Troubleshooting

Addresses common issues causing irregular engine operation.

Engine Stopped Troubleshooting

Provides troubleshooting steps for when the engine stops unexpectedly.

Unsatisfactory Performance Troubleshooting

Outlines causes and remedies for unsatisfactory engine performance.

WIRING DIAGRAM

Wiring Harness Safety Warning

Safety warning regarding the preassembled wiring harness and connections.

MZ202 ENGINE MAINTENANCE SCHEDULE

DAILY CHECKS

Pre-Flight Inspection Procedures

Procedures for inspection to be carried out before every flight.

Overview

The device is an MZ202 engine manufactured by FIATE Aviation. It is a two-stroke, double-cylinder in-line, reed valve engine designed for use in Ultralight (ULM) aircraft or other airplanes where engine failure would not lead to serious consequences. It is explicitly stated that this is not an aeronautic approved engine and has not undergone durability and safety tests in compliance with aeronautical standards. Users must assume all risks associated with its use, as sudden engine failure is possible and could result in emergency landings, material damage, injury, or death.

Function Description:

The MZ202 engine serves as a lightweight, sturdy, and reliable propulsion system. It incorporates an air cooling system with forced air (fan) and features a counter-clockwise rotation when viewed from the Power Take-Off (PTO). The engine is equipped with an electric starter motor and a 13.8 volt, 180-Watt alternator for ignition and battery charging. It utilizes an electronic double ignition switching type with variable automatic timing to ensure reliability, safety, and optimal performance. The engine is designed to operate with a mechanical gear reduction system, which includes helical gears and a centrifugal clutch. This gear reduction helps to reduce noise, boost performance by allowing the propeller to operate at lower RPMs, and mitigate dangerous torsion movements to the crankshaft during start-up. The centrifugal clutch allows the propeller to freewheel at start-up and engages only when the engine RPM exceeds 1900-2100 RPM.

Important Technical Specifications:

  • Model: MZ202
  • Type: Two-stroke, double-cylinder in-line, reed valve engine
  • Cooling System: Air cooling system, by means of forced air (fan)
  • Direction of Rotation: Counter-clockwise (seen from the PTO)
  • Capacity: 626cc (Nikasil cylinder)
  • Bore x Stroke: 76 mm x 69 mm
  • Compression Ratio: 9.1/1
  • Power Output: 63 hp at 6250 rpm
  • Peak Torque: 84 Nm at 5200 rpm
  • Lubrication: Fuel / oil blend 50:1 synthetic oil (Castrol TTS recommended)
  • Fuel Type: Super 95 RON (minimum octane rating)
  • Ignition: Magneto flywheel with electronic transducer with variable timing. Electric regulator and battery charger output: 180W 13.8 Volt
  • Carburetor: 2 x Bing 54 with float chamber and fuel pump
  • Spark Plug: NGK CR8HSA, spark gap 0.7 mm (0.027")
  • Operating Temperature: CHT max. 260 °C (500 °F), EGT max. 680 °C (1250 °F)
  • Starting: By 450 W electric starter motor
  • Engine Weight (without gear box): 34 kg (including electric starter, carburetors, fuel pump, cooling system, exhaust system)
  • Gear Box Weight: 9.27 kg
  • Main Torque Settings:
    • Cylinder head screws: M6, 16 Nm
    • Crankcase screws: M6, 16 Nm
    • Magneto flywheel nut: M10 x 1, 70 Nm
    • Cylinder nuts: M8, 26 Nm
    • Spark plug: M10 x 1.5, 16 Nm
    • Wooden Prop fastening screw: M8, 5+2 Nm
    • Other screws or nuts: M8, 20+2 Nm
    • Other screws or nuts: M6, 10+2 Nm
    • Fan case: M6, 10+2 Nm
    • Fan nut: M6, 15+3 Nm

Usage Features:

The engine requires careful preparation of the fuel/oil mixture, emphasizing the use of clean, approved containers and filtering the fuel to prevent impurities. It is crucial to use a 50:1 synthetic oil blend (Castrol TTS recommended) and Super 95 RON fuel. Users are advised to stick to the same type and brand of oil and avoid switching between synthetic and mineral-based oils due to incompatibility risks. Before starting, a general inspection is required, including checking carburetor and fuel feed circuits, vacuum pressure tubing, electrical cables, spark plug leads, engine mounts, gearbox bolts, and propeller condition. The engine requires a specific break-in procedure, involving two steps of controlled RPM increases and monitoring of Cylinder Head Temperature (CHT) and Exhaust Gas Temperature (EGT). Prolonged full throttle should be avoided for the first two hours of use, with optimal performance achieved after ten hours. Carburetor adjustment, including choke and idle settings, is detailed, with a minimum idle speed of 1800 rpm. The throttle cable requires proper adjustment to ensure free movement and correct end play. A "STOP PROCEDURE" is outlined, recommending a cool-down period at 2000-2500 RPM before shutting down to extend engine life.

Maintenance Features:

The manual provides a comprehensive maintenance schedule, with checks and work to be carried out at specified hour intervals (1, 9, 12, 25, 50, 75, 100, 125, 150, 175, 200, 225, 250, 275 hours). Key maintenance tasks include:

  • Tightening: Cylinder head screws (1h, 75h, 150h, 225h), other screws/nuts (25h, 100h, 175h, 250h), fan case/nut (25h, 100h, 175h, 250h).
  • Checks: Starter cable (25h, 100h, 175h, 250h), starter ring gear (25h, 100h, 175h, 250h), spark plug (9h, 50h, 125h, 200h, 275h), spark plug cap (25h, 100h, 175h, 250h), ignition alternator (75h, 150h, 225h), gearbox oil (1h, 50h, 100h, 150h, 200h, 250h), control cables (25h, 50h, 75h, 100h, 125h, 150h, 175h, 200h, 225h, 250h, 275h), propeller balance and tracking (25h, 50h, 75h, 100h, 125h, 150h, 175h, 200h, 225h, 250h, 275h), carburetor, idle setting and cable tension (25h, 100h, 175h, 250h), carburetor and idle pipe condition (50h, 125h, 200h, 275h), fuel pump (100h, 200h), cylinder head and piston (125h, 250h), wear and freeplay of components (50h, 125h, 200h, 275h).
  • Replacements: Spark plug (25h, 100h, 175h, 250h), exhaust springs (75h, 150h, 225h), propeller fastening screws (50h, 200h), fuel filter (75h, 150h), float pointer (125h).
  • Cleaning: Spark plug cap (25h, 100h, 175h, 250h), air and fuel filters (25h, 50h, 75h, 100h, 125h, 150h, 175h, 200h, 225h, 250h, 275h), carburetor (25h, 100h, 175h, 250h), fuel pump (100h, 200h).
  • Lubrication: Air filter (25h, 50h, 75h, 100h, 125h, 150h, 175h, 200h, 225h, 250h, 275h), control cables (25h, 50h, 75h, 100h, 125h, 150h, 175h, 200h, 225h, 250h, 275h).
  • Overhaul: A complete overhaul is recommended every 500 hours.

Daily checks and pre-flight inspections are also detailed, covering electrical contact, fuel tank water, inlet manifold, carburetor float chamber, air filter, cylinder head leakage, ignition coil connections, starter motor security, engine attachment to frame, reduction and starter motor bolts, fuel lines, unusual noises, and propeller condition. A logbook is provided to record engine repairs.

Fiate Aviation MZ202 Specifications

General IconGeneral
BrandFiate Aviation
ModelMZ202
CategoryEngine
LanguageEnglish