Product Data Sheet - 915 iS / iSc A

Product catalog summary

Overview
The 915 iS A engine offers a powerful and reliable flight experience with a power output of 141 HP. It is designed to provide the best power-to-weight ratio and reliability for aviation applications.

Specifications

Engine Type: 4-cylinder, 4-stroke liquid-/air-cooled with opposed cylinders
Lubrication: Dry sump forced lubrication with separate oil tank and automatic hydraulic valve tappet adjustment
Fuel System: Redundant electronic fuel injection and ignition
Starter: Electric (12 or 24 volt)
Gearbox: Propeller speed reduction with overload clutch
Additional Features: Air intake system with intercooler, turbocharger, stainless steel exhaust
TBO (Time Between Overhaul): 1,200 hours
Maximum Operating Altitude: 23,000 feet

Performance

Maximum Power: 104 kW (141 hp) at 5800 RPM
Continuous Power: 99.0 kW (135 hp) at 5500 RPM
Performance may vary based on conditions such as ambient temperature and altitude

Dimensions and Weight

Bore x Stroke: 84.0 mm x 61.0 mm (3.31 in x 2.4 in)
Displacement: 1352 cm³ (82.6 cu in)
Engine Weight: 82.2 kg (181.2 lb) including gearbox, turbocharger, intercooler, and exhaust system
Additional Components: Engine suspension frame (2.0 kg), external alternator (3.0 kg), air guide hood (0.4 kg), fuel pumps assembly (1.6 kg)

Fuel Requirements

Minimum MON 85, RON 95, AKI 91
Compatible with leaded, unleaded, AVGAS 100LL, and Ethanol 10 fuels

Compliance
The engine is ASTM compliant, ensuring it meets industry standards for safety and performance.

Catalog excerpts

POWER MEETS RELIABILITY. The ultimate flight experience with the best power-to-weight ratio and reliability.

Open the catalog to page 1

915 iS A Dynamic, turbocharged iS engine with best power-to-weight ratio, full take-off power and a service ceiling up to 23.000 feet. DESCRIPTION • 4-cylinder • 4-stroke liquid-/air-cooled engine with opposed cylinders • Dry sump forced lubrication with separate oil tank, automatic adjustment by hydraulic valve tappets • Redundant electronic fuel injection and ignition • Engine management system • Electric starter (12 or 24 volt) • Propeller speed reduction gearbox • Air intake system / intercooler • Turbocharger / stainless steel exhaust • TBO 1,200 hrs • Maximum operating altitude 23.000 feet...

Open the catalog to page 2

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