N390MF - 2003 SYMPHONY AIRCRAFT SYMPHONY 160

2003

SYMPHONY AIRCRAFT

SYMPHONY 160

Used

N390MF

The Symphony 160 is a single engine, two-seat, high wing, fixed tricycle landing gear, Normal Category, FAA certified VFR/IFR aircraft. Blending traditional concepts with the latest technological and ergonomic developments in light aircraft aviation, the Symphony 160 offers an affordable and easy flying experience for even the most inexperienced student or private pilot. The flying surfaces are of standard aircraft aluminum construction. The fuselage structure is steel tubing with a non-structural fiberglass shell. The robust steel tube fuselage, the aluminum wings and control surfaces along with the non-structural L-285 fiberglass exterior shell bring together the best combination of materials available on the market. This serves to guarantee high performance and durability, making the Symphony a new standard in this category of aircraft. At 2,150 lbs. maximum takeoff weight and up to 700 lbs. carrying capacity, the Symphony 160 offers unique versatility not usually found in general aviation aircraft. Engine Manufacturer Textron Lycoming Model O-320-D2A, 160 horsepower Type 4 cylinder, direct drive, horizontally opposed Maximum RPM 2,700 Induction System Carbureted Oil Capacity 8 quarts -------------------------------------------------------------------------------- Fuel Type 100 LL AVGAS Capacity 32.5 gal.; Usable: 30.2 gal. -------------------------------------------------------------------------------- Propeller - Standard (cruise) Manufacturer MT-Propeller Model 86 R 140-3D P-244-3 Composition Composite with stainless steel leading edge -------------------------------------------------------------------------------- Propeller - Optional (climb) Manufacturer Sensenich Propeller Model 74DM6S11-1-56 Composition Aluminum -------------------------------------------------------------------------------- Performance at 2,150 lbs. Service Ceiling 16,400 ft. Cruise (74% pwr @ 8,000 ft.) 128 KTAS *Rate of Climb (MSL) MT Standard Prop 710 fpm Stall Vs (flaps up) 60 KIAS Stall Vs (flaps 40°) 51 KIAS Landing (MSL-over 50 ft. obstacle) 1827 ft. Landing (ground roll) 715 ft. Take-off (MSL-over 50 ft. obstacle) 1309 ft. Take-off (ground roll) 982 ft. VNE 162 KIAS Exterior noise (take-off) 69 db Limit loads +3.8 to -1.5g (flaps up) Note: *Rate of Climb (MSL) Sensenich Climb Prop 915 fpm Performance data based on International Standard Atmospheric Conditions (ISA) Current PAS Demonstrator, Garmin 430, 420, 340, GTX-327. Price Reduced $10,000.

230.0

Garmin GNS-430 with GI-106A VOR/LOC Glide Slope Indicator Garmin GNC-420 Garmin GMA-340 Audio Panel Garmin GTX-327 Transponder Vision Microsystems VM1000 and EC100 with Fuel level, OAT/CAT, and Chronometer systems