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होम / उत्पाद / Lycoming Aircraft Engine

Lycoming IO-390-C3B6 Aircraft Engine 210 HP 2700 RPM

Lycoming IO-390-C3B6 Aircraft Engine 210 HP 2700 RPM
Lycoming IO-390-C3B6 Aircraft Engine 210 HP 2700 RPM
Lycoming IO-390-C3B6 Aircraft Engine 210 HP 2700 RPM Lycoming IO-390-C3B6 Aircraft Engine 210 HP 2700 RPM Lycoming IO-390-C3B6 Aircraft Engine 210 HP 2700 RPM Lycoming IO-390-C3B6 Aircraft Engine 210 HP 2700 RPM Lycoming IO-390-C3B6 Aircraft Engine 210 HP 2700 RPM Lycoming IO-390-C3B6 Aircraft Engine 210 HP 2700 RPM Lycoming IO-390-C3B6 Aircraft Engine 210 HP 2700 RPM Lycoming IO-390-C3B6 Aircraft Engine 210 HP 2700 RPM Lycoming IO-390-C3B6 Aircraft Engine 210 HP 2700 RPM Lycoming IO-390-C3B6 Aircraft Engine 210 HP 2700 RPM Lycoming IO-390-C3B6 Aircraft Engine 210 HP 2700 RPM Lycoming IO-390-C3B6 Aircraft Engine 210 HP 2700 RPM Lycoming IO-390-C3B6 Aircraft Engine 210 HP 2700 RPM
बुनियादी जानकारी
उत्पत्ति के प्लेस: अमेरिका
ब्रांड नाम: Lycoming
प्रमाणन: FAA 8130-3
मॉडल संख्या: आगामी IO-390-C3B6 इंजन
न्यूनतम आदेश मात्रा: 1 ईए
भुगतान शर्तें: , टी/टी
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  • विस्तार जानकारी
  • उत्पाद विवरण
मूल्यांकित शक्ति: 210 हॉर्सपावर मूल्याँकन की गति: 2700 आरपीएम
सिलिंडर व्यास: 5.319 इंच आघात: 4.375 इंच
विस्थापन: 389 घन इंच संक्षिप्तीकरण अनुपात: 8.9: 1
बाहर निकालने के आदेश: 1-3-2-4 वाल्व रॉकर आर्म क्लीयरेंस: 0.028-0.080 इंच
संचरण अनुपात: 1: 1 रोटेशन दिशा: दक्षिणावर्त
शुद्ध वजन: 315 पाउंड निष्क्रियता के पल: एक्स-एक्सिस (रोटेशन अक्ष क्रैंकशाफ्ट के केंद्र के समानांतर) 59.3in · lb · s the है; Y- अक्ष (सिलेंडर
प्रमुखता देना:

C3B6 Lycoming IO-390 Engine

,

IO-390-C3B6 Lycoming Engine

,

Lycoming IO-390-C3B6 Engine

Lycoming IO-390-C3B6 Engine
Technical Specifications
Attribute Value
Rated power 210 horsepower
Rated speed 2700 rpm
Cylinder diameter 5.319 inches
Stroke 4.375 inches
Displacement 389 cubic inches
Compression ratio 8.9:1
Firing order 1-3-2-4
Valve rocker arm clearance 0.028-0.080 inches
Transmission ratio 1:1
Rotation direction clockwise
Net weight 315 pounds
Moment of inertia X-axis (rotation axis parallel to the centerline of the crankshaft) is 59.3in·lb·s²; Y-axis (rotation axis parallel to the centerline of the cylinder) is 86.7in·lb·s²; Z-axis (vertical direction) is 45.2in·lb·s²
Product Description

The IO-390-C3B6 is a popular choice for builders and pilots looking for a reliable, high-performance engine for light aircraft.

Part Numbers
New Rebuilt Overhaul
ENPL-RT11143 RENPL-RT11143 HENPL-RT11143
Detailed Specifications
  • Engine Type: 6-cylinder, horizontally opposed (flat-six)
  • Displacement: 541.5 cubic inches (8.87 liters)
  • Power Output: 300 horsepower (224 kW) at 2,700 RPM
  • Compression Ratio: 8.7:1
  • Fuel System: Fuel injection (Continental Bendix RSA-5AD1 fuel injector)
  • Cooling System: Air-cooled
  • Weight: Approximately 390 lbs (177 kg) dry
  • Fuel Type: 100LL aviation gasoline (avgas)
  • Oil Capacity: 12 quarts (11.4 liters)
Key Features
  • Fuel Injection: Provides better fuel efficiency and performance compared to carbureted engines.
  • Air-Cooled Design: Simplifies maintenance and reduces weight.
  • High Power-to-Weight Ratio: Makes it suitable for a variety of aircraft, including high-performance singles and light twins.
  • Reliability: Known for its durability and long service life with proper maintenance.
Applications

The IO-540-AE1A5 is commonly found in aircraft such as:

  • Cessna 206 Stationair
  • Piper PA-32 Cherokee Six
  • Mooney M20K
  • Aerostar 600
Maintenance and TBO
  • TBO (Time Between Overhauls): Typically 2,000 hours, depending on operating conditions and maintenance practices.
  • Maintenance: Regular inspections, oil changes, and adherence to Lycoming's service bulletins are critical for longevity.
Contact us for prices.

टैग:

Lycoming Electronic Ignition System,

Lycoming Aircraft Piston Engine,

Piper Aircraft Engine

सम्पर्क करने का विवरण
Enzo

फ़ोन नंबर : +86 18523837266

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