|J-4 Cub Coupe|
|Piper J-4A Cub Coupe displayed at the Pima Air Museum, Tucson, Arizona in 2005|
|Role||Trainer and private owner aircraft|
|First flight||May 1938|
|Status||many still flying as of 2014|
The Piper J-4 Cub Coupe is a two place side-by-side version of the Piper J-3 that was built between 1938 and 1942 by Piper Aircraft. It was Piper's first model with side-by-side seating; combined with docile low-speed handling, this made it a good trainer.
The fuselage of the J-4 was wider than the J-3 and the aircraft had a fully enclosed rear decking to the fuselage top. The first J-4s had a Continental 50 hp A50 engine, with up[clarification needed] exhaust, an open cowl, oil and spring landing gear, a modified tail wheel system and many other changes. The early J-4 had a comfortable cockpit but was slower than most side by side aircraft of the day.
The 1940 J-4A gained a fully enclosed cowling, a Continental 65 hp A65 engine, and aft auxiliary fuel. The J-4B was fitted with a 60 hp Franklin_4AC-171 engine. The final version was the 1941 J-4E which sported a 75 hp Continental engine and redesigned interior. The main fuel tank was moved to the wing along with a header tank. Performance was now on par with similar contemporary types, but the attack on Pearl Harbor sealed its fate as all civilian aircraft manufacture came to a stop with the entry of the United States into World War II.
Some J-4s had another unique feature in the tail construction: the stabilizer was made of stainless steel tubing, riveted together with gussets.
- powered by a 50-hp (37-kW) Continental A50-1 piston engine.
- powered by a 65-hp (48-kW) Continental A65-1 or -8 piston engine.
- powered by a 60-hp (45-kW) Franklin 4AC-171 or 65-hp (48-kW) 4AC-176-B2 piston engine.
- powered by a 75-hp (56-kW) Continental A75-9 piston engine.
- powered by a 55-hp (41-kW) Avco Lycoming 0-145-A1, -A2 or 65-hp (48-kW) 0-145-B1 piston engine.
Data from Simpson, 2001, p. 430.
- Length: 22 ft 6 in (6.86 m)
- Wingspan: 36 ft 2 in (11.02 m)
- Height: 6 ft 10 in (2.08 m)
- Gross weight: 1300 lb (589.67 kg)
- Powerplant: 1 × Continental A65-1 piston engine, 65 hp ( kW) each
- Maximum speed: 100 mph (160.93 km/h)
- Cruise speed: 92 mph (148.06 km/h)
- Range: 360 miles (579.36 km)
- Service ceiling: 15,000 ft (4572 m)
- Rate of climb: 600 ft/min (3.04 m/s)
- Related development
- Related lists
- Simpson, 2001, p.429
- Simpson, 2001, p.429
- "Cub Coupe". www.pimaair.org. Pima Air & Space Museum. Retrieved 5 July 2014.
The J-4 remained an excellent selling product for Piper until December 1941 when all civilian aircraft manufacture came to a stop with the entry of the United States into World War II.
Media related to Piper J-4 at Wikimedia Commons