Αποτελέσματα Αναζήτησης
1976 - 1978 COMMANDER 114. Single engine piston aircraft with retractable landing gear. The 114 seats up to 3 passengers plus 1 pilot.
On the outside, the 114B looks much like its 114A and 114 cousins built in the mid- to late 1970s by Rockwell International. In fact, only the practiced eye can tell the difference between the 200- and 210- horsepower 112s and 112TCs of the '70s and the equivalent-era 260-hp 114s.
1 Ιουλ 2009 · PERFORMANCE: Cruise 160 kts. Stall mph 54 kts. Initial climb rate 1,160. Range 705. Ceiling 16,800'. Takeoff distance 1,145'. Landing distance 720'. The first examples of this airframe came from aerospace giant Rockwell Aircraft. Their model 112 first flew in late 1970 and continued to evolve through a number of engine changes.
Commander 114 Performance Specifications** Engine – 6-cylinder Lycoming IO-540-T4B5D, 260 HP @ 2700 RPM Prop – Hartzell HC-C2YR-1BF, Constant Speed, 2 -Blade Weights - Empty – 1,905 lbs.; Gross – 3,140 lbs. Fuel – 70 Gals. Total, 68 Gals. Usable Oil – 8 qts. Total Capacity Wing Area – 393.10” / 152 ft.²
First introduced in the 1970s, the Commander 114B is known for its sleek design, excellent performance, and spacious cabin. It is powered by a single Lycoming IO-540 engine and can accommodate up to four passengers, making it a popular choice for personal and business travel.
28 Οκτ 2024 · This 1978 Commander 114 has 639 hours on the airframe, its 260 hp Lycoming IO-540 engine, and two-blade Hartzell propeller. In the cabin, the panel was refurbished in 2022 and upgraded with Aspen ...
The Rockwell Commander 112 and Commander 114 are single-engine four-seat light touring aircraft with retractable landing gear produced by the US-American manufacturer North American Rockwell, later Rockwell International and later by Commander Aircraft Corporation.
