Steward-Davis Jet-Packet 1600

The 1956 Steward-Davis Jet-Packet 1600 was a civil conversion of Fairchild C-82A with a jet-pod added to upper fuselage. At least three were converted including N6887C and N6985C,

The Jet-Packet II involved airframe weight reduction to increase cargo weights. With two P&W R-2800CB-16 engines, the application was applied to Jet-Packet 1600 or 3400. At least three were converted, including TWA C-82A Ontos N9701F.

Engines: 2 x 2100hp P&W R-2800-85 and 1 x 1600 lb Westinghouse J30-W jet-pak
Max take-off wt: 54,000 lb

Steward-Davis Inc

1946: Steward-Davis Inc
fdrs: Herb Steward, Stanley Davis
Compton Airport CA.
USA

Under name Steward-Davis/Jet-Packet made and promoted modernized commercial version of Fairchild C-82 with turbojet mounted above fuselage for augmented power.

Gardena CA.

1961: Long Beach CA
Business partner with New Frontier Airlift Corp, Phoenix AZ,

In 1961 adapted C-119 in similar manner as Jet- Pak.

1971: New Frontier bankruptcy.

Steward-Davis Intl
Van Nuys CA

Steward-Davis left the aircraft conversion business, but continued as a company marketing APU technologies.

Stewart S-51D

First flown in March 1994. Designed by Jim D. Stewart, the Stewart S-51D is an all aluminum 2-place scale reproduction of the North American P-51D Mustang. The kit is prefabricated and held together with pop rivets for shipping. Flush aircraft rivets are installed by the builder. A fast build kit was available for US$89,000, ans the basic kit for US$64,000. The kit is included on the FAA 51 % rule list.

The aircraft features dual controls and is fully aerobatic. The S-51D utilizes liquid cooled engines ranging from 300 to 700 hp. The 91” diameter, constant speed four-blade Hartzell propeller is driven through spur gear reduction with a 0.469 (2.13:1) ratio. Using a 400 hp engine, the S-51D duplicates P- 51 performance, except for top speed.

By 1998, 72 kits had been sold in the previous three years, with two finished.

Engine: V8, 400 hp
HP range: 300-600
Height: 9 ft
Length: 22.25 ft
Wing span: 26 ft
Wing area: 123 sq.ft
Fuel cap: 70 USG
Weight empty: 2200 lb
Gross: 3000 lb
Vne: 273 mph
Speed max: 265 mph
Cruise: 240 mph
Range: 700 sm
Stall: 70 mph
ROC: 2700 fpm
Take-off dist: 900 ft
Landing dist: 1300 ft
Service ceiling: 24,000 ft
Seats: 2
Landing gear: retractable tail wheel

Engine: V8
Wing span: 7.92 m
Wing area: 11.32 sq.m
MAUW: 1360 kg
Empty weight: 998 kg
Fuel capacity: 265 lt
Max speed: 426 kph
Cruise speed: 386 kph
Minimum speed: 113 kph
Climb rate: 13 m/s
Seats: 2
Kit price (1998): $64,000

Stewart M-2

Stewart M-2 NR493M

Designed by John Hunt and Lionel Kitchen, the 1931 W F Stewart Co M-2 (ATC 2-349) shoulder wing monoplane was also powered for a short time by a Packard DR-980 Diesel. The one built (X/NR493M) was eventually sold to Abrams Aircraft for photo-survey work and scrapped in 1940.

Stewart M-2 NR493M

Engines: two 300hp Wright J-6
Wingspan: 52’10”
Length: 37’0″
Useful load: 1536 lb
Max speed: 155 mph
Cruise: 130 mph
Stall: 60 mph
Range: 350 mi
Seats: 5