P-51 MUSTANG (SAL-51), 2/3 SCALE (66%)
Built in 1988, all wood construction covered with fiberglass. Powered by Ranger Aircraft Engine 6-440C-5, 200Hp straight 6 cylinder in line WWII engine, fully documented with overhaul manuals & parts list. Stressed +/- 10 G. Fully, hydraulically, retractable main and tail wheels WITH BACKUP SYSTEM. Hydraulically operated flaps. Gerdes/Cleveland wheels and brakes. Harzell Propeller variable pitch model HC-82X20-1B, range 600 rpm. Total time engine and prop 325 hr.
Firewall-forward fiberglass cowling. Wing span - 24' - 10"Height - 7' - 0". Aspect ratio - 5.6. Wing area 110 sq. ft. Length - 22' - 6".
Empty weight - 1420 lb. Gross weight max - 2180 lb. Gross weight aerobatics - 1800 lb. Wing loading aerobatics - 16.4 lb/sq. ft.Wing loading max gross - 19.8 lb/sq. ft. Power loading aerobatics - 8.9 lb/Hp. Power loading max gross - 9.9 lb/Hp Max cruise @ 1800 lb @7000' 25' MP, 2300 rpm - 180Kt or 207 mph, Vne - 258 mph.
Cruise 75% power 23' MP, 2100 rpm - 176 mph, 21' MP, 2040 rpm - 162 mph.
Vs no flaps - 67 mph, Vs1 full flaps - 60 mph.
Fuel - 26 US Gallons / 98 Liters.
Average T.O. run @ 1800 lb - 700' Fuel consumption @ cruise 10 US Gal./hr.
Rate of climb 1800'/min.
Bendix-King KX-165 with yellow tag, KI-209 Loc/GS with yellow tag, King KT 78 Mode C transponder with yellow tag, ACK encoder, Shadin Miniflo fuel totalizer, Navworx ADS-600 EXP.
Condition in and out 8. Mechanically perfect 10. The aircraft flies hands free in level flight.
Parachute included.

Engines:
325 SNEW