The 685 was certified on September 17, 1971 per CAR 3. The 685 has a gross weight of 9000 pounds and is basically the same as the 690 with the following exceptions: Continental engines GTSIO520-K, Slight change in wing structure at the engine attach area, the picture window was divided into two individual windows in the pressure cabin and structural changes to the fuselage. The 685 was the final iteration of piston powered Twin Commander designs.
Specification Performance Kit FinderSpan | 46.66′ | 14.22m |
Length | 42.11′ | 12.83m |
Height | 14.11′ | 4.30m |
Tread | 15.50′ | 4.72m |
Cabin Entry Door | 3. 91’ x 2.21’ | 1.19 x 0.67m |
Cabin Height (Inside Interior) | 4.55' | 1.38m |
Cabin Length | 14.41′ | 4.39m |
Cabin Width (Inside Interior) | 4.33′ | 1.31m |
Cabin Volume (incl cockpit) | 224 ft³ | 68.27m³ |
Baggage compartment height | 3′ | 0.91m |
Baggage compartment width | 3.83′ | 1.16m |
Baggage compartment length | 4.83′ | 1.47m |
Baggage compartment volume | 43 ft³ | 13.10 m³ |
Baggage door height | 2.60′ | 0.79m |
Baggage door width | 1.64′ | 0.49m |
Baggage compartment load limit | xxx lbs | xxx kg |
xx
Continental engines GTSIO520-K
Ramp Weight: | xx,xxx lbs/x,xxx kg |
Take-off Weight: | xx,xxx lbs/x,xxx kg |
Landing Weight: | x,xxx lbs/x,xxx kg |
Standard Empty Weight: | x,xxx lbs/x,xxx kg |
Useful Load: | x,xxx lbs/x,xxx kg |
Zero Fuel Weight: | x,xxx lbs/x,xxx kg |
Baggage: | xxx lbs/xxx kg |
Maximum Cruise | |
(100% 12,000 ft.TAS@ 10,325 lbs/4,683 kg) | xxxmph/xxxkts |
Normal Cruise Speed | |
(96%20,000 ft.TAS@ 10,325 lbs/4,683 kg): | xxxmph/xxxkts |
Twin Engine Best Rate of Climb Speed (CAS): | xxxmph/xxxkts |
Twin Engine Best Angle of Climb Speed (CAS): | xxxmph/xxxkts |
Single Engine Best Rate of Climb Speed (CAS): | xxxmph/xxxkts |
Single Engine Best Angle of Climb Speed (CAS): | xxxmph/xxxkts |
Minimum Control Speed (CAS): | xxmph/xxkts |
Stall Speed, Clean (CAS): | xxmph/xxkts |
Stall Speed, Gear and Flaps Down (CAS): | xxmph/xxkts |
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