The NWT Spruce Coupe is an American homebuilt aircraft that was designed and produced by NWT Co of Charleston, Maine. When it was available the aircraft was supplied as a kit and also in the form of plans for amateur construction.
The Spruce Coupe features a strut-braced low-wing, a single-seat enclosed cockpit, fixed conventional landing gear and a single engine in tractor configuration.
The aircraft is made from a combination of spruce or pine, and fir, birch, mahogany plywood with its flying surfaces covered in doped aircraft fabric. Its span wing has a wing area of , mounts Junkers ailerons and is braced with "V" struts to the landing gear. The cabin width is . The acceptable power range is and the standard engine used is the Zenoah G-50 twin-cylinder, horizontally opposed, two stroke, carburetted aircraft engine.
The Spruce Coupe has a typical empty weight of and a gross weight of , giving a useful load of . With full fuel of the payload for the pilot, passengers and baggage is .
The aircraft is noted for its STOL capabilities and the standard day, sea level, no wind, take off with a engine is and the landing roll is .
The manufacturer estimates the construction time from the supplied kit as 500 hours.
By 1998 the company reported that one aircraft had been completed and was flying.