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AC68
Integrator1 (talk | contribs) (New page: {{Infobox General |source = SKYbrary |source_image = skybrary |source_caption = skybrary |control = EUROCONTROL |control_image = Eurocontrol |control_capti...) |
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| − | {{ | + | {{Aircraft |
| − | | | + | |Name=Commander 680F |
| − | | | + | |Manufacturer=AERO COMMANDER |
| − | | | + | |WTC=L |
| − | | | + | |APC=A |
| − | | | + | |Body=Narrow |
| − | | | + | |Wing=Fixed Wing |
| + | |Engine=Piston | ||
| + | |Engine_Amount=Multi | ||
| + | |Type_Code=L2P | ||
| + | |Description=Light utility corporate aircraft. In widespread service from 1958 in a range of versions. Developed from 1958 to 1967 on the basis of the 520/560 series. | ||
| + | |Wing_Span=13.4 | ||
| + | |Length=13.1 | ||
| + | |Heigth=4.6 | ||
| + | |Wing_position=High wing | ||
| + | |Engine_position=(Front) Wing leading mounted | ||
| + | |Tail_configuration=Regular tail, low set | ||
| + | |Landing_gear=Tricycle retractable | ||
| + | |Powerplant=2 x 340 HP Lycoming GSO-480-A1A-6 or 2 x 380 HP Lycoming IGSO-540-B1A piston engines with 3 blade propellers. | ||
| + | |Engine_Model=Lycoming O-480, Lycoming O-540 | ||
}} | }} | ||
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Latest revision as of 17:31, 7 September 2020
| Aircraft | ||||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Name | Commander 680F | |||||||||||
| Manufacturer | AERO COMMANDER | |||||||||||
| Body | Narrow | |||||||||||
| Wing | Fixed Wing | |||||||||||
| Position | High wing | |||||||||||
| Tail | Regular tail, low set | |||||||||||
| WTC | Light | |||||||||||
| APC | A | |||||||||||
| Type code | L2P | |||||||||||
| Engine | Piston | |||||||||||
| Engine count | Multi | |||||||||||
| Position | (Front) Wing leading mounted | |||||||||||
| Landing gear | Tricycle retractable | |||||||||||
| Mass group | 2 | |||||||||||
|
| ||||||||||||
AERO COMMANDER Commander 680F
Description
Light utility corporate aircraft. In widespread service from 1958 in a range of versions. Developed from 1958 to 1967 on the basis of the 520/560 series.
Technical Data
| Wing span | 13.4 m43.963 ft <br /> |
|---|---|
| Length | 13.1 m42.979 ft <br /> |
| Height | 4.6 m15.092 ft <br /> |
| Powerplant | 2 x 340 HP Lycoming GSO-480-A1A-6 or 2 x 380 HP Lycoming IGSO-540-B1A piston engines with 3 blade propellers. |
| Engine model | Lycoming O-480, Lycoming O-540 |
Performance Data
| Take-Off | Initial Climb (to 5000 ft) |
Initial Climb (to FL150) |
Initial Climb (to FL240) |
MACH Climb | Cruise | Initial Descent (to FL240) |
Descent (to FL100) |
Descent (FL100 & below) |
Approach | ||||||||||
| V2 (IAS) | kts | IAS | 180 kts | IAS | kts | IAS | kts | MACH | TAS | 180 kts | MACH | IAS | kts | IAS | 180 kts | Vapp (IAS) | kts | ||
| Distance | 457 m | ROC | 1000 ft/min | ROC | ft/min | ROC | ft/min | ROC | ft/min | MACH | ROD | ft/min | ROD | ft/min | MCS | kts | Distance | 490 m | |
| MTOW | 40004,000 kg <br />4 tonnes <br /> kg | Ceiling | FL240 | ROD | 1000 ft/min | APC | A | ||||||||||||
| WTC | L | Range | 13701,370 nm <br />2,537,240 m <br />2,537.24 km <br />8,324,278.221 ft <br /> NM | ||||||||||||||||
Accidents & Serious Incidents involving AC68
None on SKYbrary