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NORTH AMERICAN T28

  NORTH AMERICAN T28 "TANGO"
 
Reg G-TROY

The North American Aviation T-28 was a basic trainer that was ordered in three advanced versions, the T-28A for the U.S Air Force and T-28B and T-28C, by the U.S. Navy, with the latter version designed for carrier operation. It was the first trainer designed to transition pilots to using jet aircraft.

Originally, it was powered by a Wright R-1300 engine with a rating of 800 horsepower, a top speed of 285 mph (459 kph) and a service ceiling of 29,000 feet (8839 meters). New versions carried a Wright R-1820 engine with a rating of 1,425 horsepower, a top speed of more than 345 mph (555 kph) and a 37,000-foot (11,278-meter) ceiling.

The T-28B and T-28C could handle accessory kits providing for bombs, rockets and machine guns.

1,194 T-28As were delivered to the U.S. Air Force and the Navy ordered 792 T-28s, 299 of which were T-28Cs that included an arrester hook for carrier landings. Some versions of the T-28 were adapted to more extensive military operations by other countries.

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Technical
Specifications

Surface ceiling

Range

Fuel consumption

Empty weight

MTOW

Seats

Take-off distance

Engine type

35,500 ft

320 nm

50 GPH

2914 kg

3856 kg

1 pilot / 1 passenger

400m

9-cylinder Radial

Registration

Manufacturer

Year of construction

Serial number

Power plant

Power

Engine displacement

Cruising Speed

Max speed

G-TROY

NORTH AMERICAN

1951

51-7692

WRIGHT 1820

1425 HP

29.9L

230 knts

300 knts

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