After ever-bigger Rebels, the JDM – 8 is a genuine ultralight Darryl Murphy’s commitment to small plane design is evident by the fact that during the years when Murphy Aircraft Mfg. exhibited in two locations at various fly-ins, Darryl frequently was seen working his company’s booth in the ultralight area. Other Murphy Aircraft staff members would be working the Rebel/Super Rebel booth. At the Northwest EAA Fly-In in Arlington, Washington, this past summer, that pattern re-emerged; the boss stayed with the JDM-8 in the ultralight exhibit area. In my conversations with him, he seemed pleased to be presenting a genuine ultralight again. Those who know the history of Murphy Aircraft before the first Rebel arrived won’t be surprised to see the company marketing an ultralight. This Canadian manufacturer was an ultralight company that expanded into homebuilts and has achieved success through their Rebel series. The new single-seat JDM-8—especially when contrasted with the huge, radialengine- powered Moose—shows this company has not forgotten its roots in ultralight aircraft.
Murphy Aircraft Returns to Its Roots
The naysayers said an all-metal truly legal ultralight couldn't be built, but Darryl Murphy has proved them wrong. The low-wing JDM-8 ultralight does meet the weight and speed restrictions of FAR Part 103 when powered with the 28 hp Rotax 277 engine. It doesn't offer sprightly performance at that low horsepower, but it does provide pleasurably low-and-slow flight.
For weight and balance purposes, the lightweight Rotax 277 engine was placed far forward in the engine compartment. Obviously, there's plenty of room for the 48 hp Rotax 503 engine should a builder opt to certificate the aircraft in the experimental amateur-built category. Murphy Aircraft hasn't sought official recognition from FAA for 51-percent kit approval, but stated they may do so in the future. Neatly cowled, the JDM-8 has nice, aerodynamic lines.
Again, in an attempt to keep the JDM-8 light and legal, only basic instrumentation was installed in the aircraft. Forming the seat from a metal pan and using a lightweight cushion for comfort saved more weight, as did putting lightening holes in the rudder pedals. Looking down the bulkheads of the fuselage. The seat can be moved aft one bulkhead to accommodate pilots with longer legs.
Heretofore, Darryl Murphy has never been a fan of folding wings, but he agreed to incorporate that feature in this design, recognizing it would make storage easier and less expensive as owners would be able to share hangar space. But, Darryl opted to have the wings fold up a la Navy carrier aircraft instead of back, thinking that would create less of a likelihood for the wings to fold in flight. The beefy hinges holding the wing up will become a primary preflight inspection point as they'll suffer the most wear in this configuration.
This view of the JDM-8 from the back helps visualize what the wing would look like with the outer bay of each wing panel removed-an option that's available for those who wish to power the aircraft with the Rotax 503 engine and would like more speed. Thusly shortened, the wing would end at the outside edge of the ailerons.
Seating | 1 |
Empty weight | 250-254/300-400 pounds |
Gross weight | 485/700 pounds |
Wingspan | 24/20 feet |
Wing area | 120/100 square feet |
Wing loading | 4.0/up to 7.0 pounds per square foot |
Width | (wings folded) 8 feet |
Height | (wings folded) 10.75 feet |
Fuel Capacity | 5/20 gallons |
Standard engine | Rotax 277 |
Power | 25-30/up to 80 hp |
Power loading | 17.3*/8.75 pounds/hp |
Max Speed | 63/110 mph |
Cruise speed | 40-60/45-100 mph |
Stall Speed | 26/34 mph |
Rate of climb at gross | 600/1,000 fpm |
Takeoff distance at gross | 200/100 feet** |
Landing distance at gross | 150/200 feet*** |
Range (powered) | 125/400 miles |
Notes: | *Assuming Rotax 277 engine at 28 horsepower.
**Assuming 28/80 horsepower. ***Assuming 485/700 pounds gross weight. |