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ryan_3
Specifications (PT-22)Additional specifications of interest to the pilot include:
Fuel Capacity: 24 US Gal (19.99 IMP. Gal)[3]
Oil Capacity: 3 US Gal (2.5 IMP. Gal)[4]
Best Climb Speed: 79 mph (127 km/h)[5]
Best Glide Speed: 85 mph (137 km/h)[6]
Max Flap Extension Speed: 100 mph (160 km/h)[7]
Best Approach Speed: 85 mph (137 km/h) [8]
The PT-22 fuel system consists of a single tank mounted forward of the front cockpit. Fuel is gravity fed to the carburetor through a fuel strainer. A fuel selector valve, located on the left side of each cockpit has three positions: "main", "reserve", and "off". The "reserve" section feeds fuel from the reserve portion at the bottom of the aircraft's only fuel tank. The fuel gauge consists of a sight gauge above the tank, visible to both pilots out the front of the aircraft. The oil system is a dry-stump type, with all oil stored in a tank located on the front side of the firewall in the upper section of the fuselage. Oil Pressure and temperature gauges are provided in each cockpit. Normal oil pressures range from 40 PSI (at idle) to a max of 125 PSI, with 100 PSI being ideal. Normal oil temperatures range from a minimum of 35 degrees C to a max of 75 degrees C, with 60-75 degrees C being ideal. The wing flaps are mechanically operated from a lever located on the left side of each cockpit. Adjustable elevator trim is provided via an elevator trim tab controllable from a handwheel mounted on the left side of each cockpit. In its original configuration, the aircraft was not equipped with an electrical system. Hydraulic brakes are provided for each wheel, controllable via the rudder pedals in each cockpit[9].
General characteristics
Crew: two (student and instructor)
Length: 22 ft 5 in (6.90 m)
Wingspan: 30 ft 1 in (9.17 m)
Height: 7 ft 2 in (2.18 m)
Wing area: 134.25 sq ft[10] (12.5 sq m)
Airfoil: NACA 2412[11]
Empty weight: 1308 lb [12] (593 kg)
Loaded weight: 1860 lb [13] (844 kg)
Useful load: 552 lb [14] (250 kg)
Max takeoff weight: 1,860 lb [15] (844 kg)
Powerplant: 1× Kinner R-540, 160 hp [16] (120 kW)
Performance
Never exceed speed: 190 mph [17] (305 km/h)
Maximum speed: 125 mph (200 km/h)
Cruise speed: 100 mph [18] (160 km/h)
Stall speed: 62 mph, flaps down; 64 mph, flaps up [19] (100 km/h, flaps down; 103 km/h, flaps up)
Range: 231 miles @1560 RPM [20] (371 km @1560 RPM)
Service ceiling: 15,400 ft (4,700 m)
Rate of climb: 710 fpm @ max TO weight [21] (216 m/min @ max TO weight)
Wing loading: 13.6 lb/sq ft[22] ()
Armament
None [23]
Fuel Capacity: 24 US Gal (19.99 IMP. Gal)[3]
Oil Capacity: 3 US Gal (2.5 IMP. Gal)[4]
Best Climb Speed: 79 mph (127 km/h)[5]
Best Glide Speed: 85 mph (137 km/h)[6]
Max Flap Extension Speed: 100 mph (160 km/h)[7]
Best Approach Speed: 85 mph (137 km/h) [8]
The PT-22 fuel system consists of a single tank mounted forward of the front cockpit. Fuel is gravity fed to the carburetor through a fuel strainer. A fuel selector valve, located on the left side of each cockpit has three positions: "main", "reserve", and "off". The "reserve" section feeds fuel from the reserve portion at the bottom of the aircraft's only fuel tank. The fuel gauge consists of a sight gauge above the tank, visible to both pilots out the front of the aircraft. The oil system is a dry-stump type, with all oil stored in a tank located on the front side of the firewall in the upper section of the fuselage. Oil Pressure and temperature gauges are provided in each cockpit. Normal oil pressures range from 40 PSI (at idle) to a max of 125 PSI, with 100 PSI being ideal. Normal oil temperatures range from a minimum of 35 degrees C to a max of 75 degrees C, with 60-75 degrees C being ideal. The wing flaps are mechanically operated from a lever located on the left side of each cockpit. Adjustable elevator trim is provided via an elevator trim tab controllable from a handwheel mounted on the left side of each cockpit. In its original configuration, the aircraft was not equipped with an electrical system. Hydraulic brakes are provided for each wheel, controllable via the rudder pedals in each cockpit[9].
General characteristics
Crew: two (student and instructor)
Length: 22 ft 5 in (6.90 m)
Wingspan: 30 ft 1 in (9.17 m)
Height: 7 ft 2 in (2.18 m)
Wing area: 134.25 sq ft[10] (12.5 sq m)
Airfoil: NACA 2412[11]
Empty weight: 1308 lb [12] (593 kg)
Loaded weight: 1860 lb [13] (844 kg)
Useful load: 552 lb [14] (250 kg)
Max takeoff weight: 1,860 lb [15] (844 kg)
Powerplant: 1× Kinner R-540, 160 hp [16] (120 kW)
Performance
Never exceed speed: 190 mph [17] (305 km/h)
Maximum speed: 125 mph (200 km/h)
Cruise speed: 100 mph [18] (160 km/h)
Stall speed: 62 mph, flaps down; 64 mph, flaps up [19] (100 km/h, flaps down; 103 km/h, flaps up)
Range: 231 miles @1560 RPM [20] (371 km @1560 RPM)
Service ceiling: 15,400 ft (4,700 m)
Rate of climb: 710 fpm @ max TO weight [21] (216 m/min @ max TO weight)
Wing loading: 13.6 lb/sq ft[22] ()
Armament
None [23]