Continental O-520
| Teledyne Continental Motors | |
|---|---|
 Continental IO-520 |
|
| Continental O-520 | |
| Production period: | since 1964 |
| Manufacturer: | Teledyne Continental Motors |
| Developing country: |
 United States
|
| First run: | 1963 |
| Working principle: | Otto |
| Motor design: | Boxer engine |
| Cylinder: | 6th |
| Displacement: | 8514 cm 3 |
| Mixture preparation: | Carburetor / manifold injection |
| Engine charging: | none / turbocharger |
| Cooling system: | Air cooling |
| Power: | 213 - 280 kW |
| Dimensions: | ? kg |
| Previous model: | none |
| Successor: | IO-550 |
Continental O-520 is the name of a piston engine family from the US manufacturer Teledyne Continental Motors .
All engines in this series are air-cooled 4-stroke boxer engines (O for opposite , opposite), have six cylinders with a bore of 133.35 mm and a stroke of 101.6 mm. The displacement is, as the number indicates, 520 cubic inches , corresponding to 8514 cm³. The engine was first introduced in 1963 and is the six-cylinder version of the O-346 . Different versions have additional features that can be recognized by letters in front of the designation, such as: B. I ( injection ) for fuel injection , G ( geared ) for reduction gears, S ( supercharger ) for a supercharger driven by the engine, T ( turbo supercharger ) for turbocharging and V for the possibility of vertical installation in helicopters. The engine was the basis of the subsequent O-550 engine.
The engine is used in the Beech 35 Bonanza, Bellanca 17 -30 Viking, Piper Malibu , Cessna 185 , Cessna 210 E Centurion, Cessna 206 Super Skywagon, Cessna 340 and Cessna 402 .
variants
- O-520-A: Original engine with 213 kW power
- IO-520-B:
- IO-520-BA, -BB, -C, -CB: Version with direct injection and 213 to 223 kW
- IO-520-D: version with direct injection and 224 kW
- IO-520-E: Version with 209 kW (2750 / min) continuous output and 221 kW (2850 / min) maximum output during max. 5 minutes
- IO-520-F:
- IO-520-J:
- IO-520-K:
- IO-520-L:
- IO-520-M: version with direct injection and 213 kW
- IO-520-MB:
- GTSIO-520-C: version with direct injection and 254 kW
- GTSIO-520-D:
- GTSIO-520-H:
- GTSIO-520-K:
- GTSIO-520-L:
- GTSIO-520-M: version with direct injection and 280 kW
- GTSIO-520-N:
- LIO-520-P:
- LTSIO-520-AE: Version with 186 kW
- TSIO-520-AE: Version with 186 kW
- TSIO-520-AF:
- TSIO-520-B:
- TSIO-520 BE / SER: version with direct injection, turbocharger and 230 kW
- TSIO-520-C:
- TSIO-520-CE:
- TSIO-520-E:
- TSIO-520-EB:
- TSIO-520-G:
- TSIO-520-H:
- TSIO-520-J:
- TSIO-520-K.
- TSIO-520-L: version with direct injection, turbocharger and 242 kW
- TSIO-520-LB:
- TSIO-520-M:
- TSIO-520-NB, N: version with direct injection, turbocharger and 250 kW
- TSIO-520-P:
- TSIO-520-R:
- TSIO-520-T:
- TSIO-520-UB: version with direct injection, turbocharger and 224 kW
- TSIO-520-VB, -WB: version with direct injection, turbocharger and 242 kW
- TNIO-520-B, BA, -BB: Version with direct injection and regulated turbocharging (Turbo Normalizer), 213 kW, conversion according to FAA STC SE5222NM
Web links
- Luftfahrt-Bundesamt: registration data
- FAA: TYPE CERTIFICATE DATA SHEET NO. E8CE (PDF; 51 kB)
Individual evidence
- ↑ LBA: Propeller driven airplanes ( page no longer available , search in web archives ) Info: The link was automatically marked as defective. Please check the link according to the instructions and then remove this notice.
