COMMANDER AIRCRAFT 114/115
STANDARD DATA: (114) Seats 4. Gross wt. 3,260. Empty wt. 2,102. Fuel capacity 68. Engine 260-hp Lycoming IO-540-T4B5. 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 […]
