Lycoming IO-390

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Lycoming
Lycoming-IO390.jpg
IO-390
Production period: 2009 – current
Manufacturer: Lycoming
Developing country: United StatesUnited States United States
First run: 2002
Working principle: Otto
Motor design: Boxer engine
Cylinder: 4th
Drilling: 135.1 mm
Hub: 111.1 mm
Displacement: 6370 cm 3
Mixture preparation: Injector
Engine charging: -
Power: 157 - 160 kW
Previous model: Lycoming IO-360
Lycoming IO-580
Successor: none

The Lycoming IO-390 is a four-cylinder boxer engine for small aircraft manufactured by the US company Lycoming . Since there is no version with a carburetor that would have the designation O-390, the IO-390 is the basic model.

construction and development

The engine was originally conceived as the IO-400-X in the 1970s, but the project has been discontinued.

The motors of the IO-390 series (factory designation IO-390-X) produce between 200  HP (147  kW ) and 215 HP (158 kW). The IO-390 was developed from the IO-360 by using the larger cylinders of the IO-580 . It has improved air intake, roller tappets and a slick start ignition. The engine has a fuel injection system that measures the amount of fuel in relation to the air flow through the intake system and gasifies the fuel in the intake manifold. The engine capacity is 6390 cm³. The cylinder heads are air-cooled .

The IO-390 was presented for the first time at the EAA AirVenture 2002. The recommended mean time between overhaul is 2000 hours.

Before the engine received its type certification , it was first marketed through Thunderbolt Engines - Lycoming's custom-built subsidiary - and was only available for non-type-certified aircraft during that time. The IO-390 received its FAR Part 33 approval on March 30, 2009.

In January 2009, the base price for the IO-390-EXP was 32,650 US dollars .

In November 2009, Lycoming announced that it is the supplemental type approval of the Federal Aviation Administration had received to the Lycoming O-360 engines in the Mooney M20E, M20F and M20J with new or refurbished IO-390-A3A6 engines replaced. Furthermore, Commander Aircraft received a supplementary type certificate for the Rockwell Commander 112 B with MTV-12-B / 188-59b propellers.

variants

IO-390

IO-390-X
Four cylinders, injection, Boxer, air-cooled, direct drive, 6390 cc, 210 hp (154 kW) at 2700 min -1 , dry weight of 308 lb (140 kg)
IO-390-EXP
Four cylinders, injection, Boxer, air-cooled, direct drive, 6390 cc, 210 hp (154 kW) at 2700 min -1 , dry weight of 308 lb (140 kg), model no pattern approval for DIY aircraft built by Lycomings thunderbolt division.
IO-390-A1A6
First: four-cylinder injection engine, air-cooled boxer,,, cc direct drive 6390, 210 hp (154 kW) at 2,700 min -1 , prepared for variable pitch with one-lever operation, pattern-approved March 30, 2009
IO-390-A1B6
Certified pattern model, four-cylinder injector, Boxer, air-cooled, direct drive, 6390 cc, 210 hp (154 kW) at 2700 min -1 . Identical to the A1A6, but with the propeller tachometer on the front left of the crankcase, type approval on January 21, 2010.
IO-390-A3A6
Certified pattern model, four-cylinder injector, Boxer, air-cooled, direct drive, 6390 cc, 210 hp (154 kW) at 2700 min -1 . Prepared for controllable pitch propellers with single-lever operation, identical to the A1A6, but with newly arranged cylinder liners for the propeller shaft, type approval on August 27, 2009.
IO-390-A3B6
Certified pattern model, four-cylinder injector, Boxer, air-cooled, direct drive, 6390 cc, 210 hp (154 kW) at 2700 min -1 . Identical to the A3A6, but with the propeller tachometer on the front left of the crankcase, type approval on April 5, 2012.
IO-390-C1A6
Certified pattern model, four-cylinder injector, Boxer, air-cooled, direct drive, 6390 cc, 215 hp (158 kW) at 2700 min -1 . Identical to the IO-390-A1A6, but with a lighter oil pan, modified air intake and an RSA-10 injection system, type approval on January 25, 2016.
IO-390-C1B6
Certified pattern model, four-cylinder injector, Boxer, air-cooled, direct drive, 6390 cc, 215 hp (158 kW) at 2700 min -1 . Identical to the C1A6, but with the propeller tachometer on the front left of the crankcase, type approval on January 25, 2016.
IO-390-C3A6
Certified pattern model, four-cylinder injector, Boxer, air-cooled, direct drive, 6390 cc, 215 hp (158 kW) at 2700 min -1 . Identical to the C1A6, but with rearranged cylinder liners for the propeller shaft, type approval on January 25, 2016.
IO-390-C3B6
Approved model, four cylinder, injected, boxer, air cooled, direct drive, 6390 cc, 215 hp (158 kW) at 2,700 rpm, dry weight 296 lb (134 kg). Identical to the C3A6, but with the propeller tachometer on the front left of the crankcase. Used in the Cirrus SR20 G6.

AEIO-390

AEIO-390-A1A6
Certified pattern model aerobatic fed blank, four-cylinder injector, Boxer, air-cooled, direct drive, 6390 cc, 210 hp (154 kW) at 2700 min -1 . Identical to the IO-390-A1A6, but equipped with a lubrication system suitable for aerobatics, type approval on April 5, 2012.
AEIO-390-A1B6
Certified pattern model aerobatic fed blank, four-cylinder injector, Boxer, air-cooled, direct drive, 6390 cc, 210 hp (154 kW) at 2700 min -1 . Identical to the IO-390-A1B6, but equipped with an aerobatic lubrication system, type approval on April 5, 2012.
AEIO-390-A3A6
Certified pattern model aerobatic fed blank, four-cylinder injector, Boxer, air-cooled, direct drive, 6390 cc, 210 hp (154 kW) at 2700 min -1 . Identical to the IO-390-A3A6, but equipped with an aerobatic lubrication system, type approval on April 5, 2012.
AEIO-390-A3B6
Certified pattern model aerobatic fed blank, four-cylinder injector, Boxer, air-cooled, direct drive, 6390 cc, 210 hp (154 kW) at 2700 min -1 . Identical to the IO-390-A3B6, but equipped with an aerobatic lubrication system, type approval on April 5, 2012.

use

Van's Aircraft RV-8s with an IO-390
Kit planes
Mooney M20J with an IO-390-A3A6
Type-approved aircraft
military aircraft

Web links

Commons : Lycoming IO-390  - Collection of pictures, videos and audio files

Individual evidence

  1. a b c d 390 Series. Lycoming , accessed February 1, 2020 .
  2. a b c d e Operation Reference Manual. (pdf) Lycoming , 2007, accessed on February 1, 2020 .
  3. a b c d e f g h i j k l Lycoming's Certified IO-390 Series Engine. Lycoming , 2008, archived from the original ; accessed on January 7, 2009 .
  4. a b Thunderbolt Engine Configurator. Lycoming , January 2009, archived from the original ; accessed on January 6, 2009 .
  5. ^ A b Mary Grady: Lycoming Gets IO-390 STC For Legacy Mooneys. AVweb, November 18, 2009, accessed February 1, 2020 .
  6. Supplemental Type Certificate, STC Number: SA00291BO. Federal Aviation Administration , November 12, 2009, accessed February 1, 2020 .
  7. a b c d e f g h i j k l Type Certificate Data Sheet No. E00006NY. Federal Aviation Administration , accessed February 1, 2020 .
  8. ^ Cirrus Aircraft | SR20. Cirrus Aircraft, accessed January 30, 2017 .
  9. ^ Mary Grady: Cessna News Update: ASTM Compliance For SkyCatcher. AVweb, July 26, 2009, accessed February 1, 2020 .
  10. ^ A b Joseph E. (Jeb) Burnside: Lycoming: Bringing More Technology To An Airplane Near You. AVweb, July 26, 2009, accessed February 1, 2020 .
  11. ^ Cirrus G6 announcement. Cirrus Aircraft, January 2017, accessed February 1, 2020 .
  12. ^ Mary Grady: Cirrus Updates SR22 And SR20. AVweb, January 4, 2017, accessed February 1, 2020 .
  13. P2010 P Twenty-Ten. Tecnam , accessed February 1, 2020 .
  14. ^ Lancair To Provide Colombian Air Force With Training Aircraft. Aero News Network, February 4, 2009, accessed February 1, 2020 .