Αποτελέσματα Αναζήτησης
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.
The airplane is powered by a horizontally opposed, six cylinder, direct drive, normally aspirated, air cooled, fuel injected engine. The engine is a Lycoming IO-540-T4B5 and is rated at 260 horsepower. Fuel is supplied to the engine by two integral fuel tanks, one in the forward section of each wing.
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.
Rockwell Commander 114 Standardization Manual. This manual is to be utilized in conjunction with the manufacturers approved POH/ AFM and the Airplane Flying Handbook (FAA-H-8083-3A). This manual should be used as a reference for approximate power settings and Leading Edge Aviation standard procedures.
This two-door, tricycle gear aircraft sports a high amount of wing dihedral and a cruciform tail configuration, and with numerous updates in both performance and comfort, the 114B has a leg up on its predecessors.
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.
