This is an extremely rare Anderson Greenwood AG 14 manufactured in Texas after World War II in 1950..



Item specifics
Condition: Used
This is an extremely rare Anderson Greenwood AG-14 manufactured in Texas after World War II in 1950. It is one of two known to exist. This one, serial number 3, is a standard category aircraft, fully restored with a fresh annual and a full set of logs. This is a full factory built aircraft, not rebuilt from parts. See the video below to learn more about this exceptional historical aircraft that is not only fun to fly, but will attract attention everywhere you land!
Click or paste the link below into your browser to view the video on a mobile device: here Specs: Airframe: 1,496 Hours TTSNEW Engine: Continental 0-200-B
570 Hours TT, 40 Hours SMOH by Pacific Continental (New Cylinders) Propeller: Hartzell HA-12UF-1 Push Propeller
Overhauled in 2004 Exterior: Overall White with Dark Blue and Red Stripes – Excellent Condition Interior: Light Gray Interior, Leather Seats- Excellent Condition AVIONICS:
King KY-96A Comm
King KT-76A Transponder

EQUIPMENT:
3” Gyros
ELT
ATD-300 Traffic-Watch
Parking Brake
Landing Light and Position Lights MISCELLANEOUS:
 Annual Inspection Completed March 2011
All AD’s Complied With
This aircraft was kept at the EAA Museum from 1986-2003
Aircraft was Completely Restored in 2009
1st Standard Certified Pusher Airplane
Completed Logbooks Since New
Original Manufacturer"s Specifications Powerplant Recommended TBO Continental C-90-12FP, 90 hp 1,800 hr Propeller Hartzell 72-in dia, ground-adjustable Length 22 ft Height 6 ft 5 in Wingspan 34 ft Wing area 120 sq ft Wing loading 11.7 lb/sq ft Power loading 15.6 lb/hp Seats 2 Cabin width 44 in Standard empty weight 861 lb Max takeoff weight 1,400 lb Max useful load 539 lb Max payload w/full fuel 395 lb Max landing weight 1,400 lb Fuel capacity, std 24 gal Oil capacity 4.8 qt Baggage capacity 250 lb, 8 cu ft Performance Takeoff distance over 50-ft obstacle 1,887 ft Rate of climb, sea level 630 fpm Max level speed, sea level 120 mph Cruise speed/endurance w/45-min rsv, std fuel (fuel consumption) @ 70% power 110 mph/4.1 hr (30 pph/5 gph) Absolute ceiling 19,000 ft Landing distance over 50-ft obstacle 1,451 fpm Limiting and Recommended Airspeeds V X (best angle of climb) 68 mph V Y (best rate of climb) 75 mph V NO (max structural cruising) 132 mph V NE (never exceed) 148 mph V A (design maneuvering) 109 mph V FE (max flap extended) 94 mph V S1 (stall, clean) 61 mph V S0 (stall, in landing configuration) 57 mph All specifications are based on manufacturer"s calculations. All performance figures are based on standard day, standard atmosphere, sea level, gross weight conditions, ground-adjustable propeller in high pitch unless otherwise noted. Current date: 2016-05-16