title: Piper J-4
text: # Piper J-4
  
  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.
  
  ## J-4 development
  
  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 upward-facing exhaust ports, 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.
  
  ## Variants
  
  ### J-4
  
      powered by a 50-hp (37-kW) Continental A50-1 piston engine.
  
  ### J-4A
  
      powered by a 65-hp (48-kW) Continental A65-1 or -8 piston engine.
  
  ### J-4B
  
      powered by a 60-hp (45-kW) Franklin 4AC-171 or 65-hp (48-kW) 4AC-176-B2 piston engine.
  
  ### J-4E
  
      powered by a 75-hp (56-kW) Continental A75-9 piston engine.
  
  ### J-4F
  
      powered by a 55-hp (41-kW) Avco Lycoming O-145-A1, -A2 or 65-hp (48-kW) O-145-B1 piston engine.
  
  ## Specification (J-4A)
  
  General characteristics Performance
  
  Data from Simpson, 2001, p. 430.
  
  General characteristics
  
  * 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: 1,300 lb (589.67 kg)
  * Powerplant: 1 × Continental A65-1 piston engine , 65 hp (48 kW)
  
  Performance
  
  * Maximum speed: 100 mph (160.93 km/h, 87 kn)
  * Cruise speed: 92 mph (148.06 km/h, 80 kn)
  * Range: 360 mi (579.36 km, 310 nmi)
  * Service ceiling: 15,000 ft (4,572 m)
  * Rate of climb: 600 ft/min (3.04 m/s)
  