Two 1928 Alexander Eaglerock A-7 conversions were built; NX4570 and NX4753.
NX4570 was destroyed in a hangar fire, and ATC 2-1 Group 2 approval was cancelled.
Engine: 125hp Ryan-Siemens
Wingspan: 36’8″
Seats: 3
Two 1928 Alexander Eaglerock A-7 conversions were built; NX4570 and NX4753.
NX4570 was destroyed in a hangar fire, and ATC 2-1 Group 2 approval was cancelled.
Engine: 125hp Ryan-Siemens
Wingspan: 36’8″
Seats: 3

Two or three of the 1928 Alexander Eaglerock A-5 were built. One as entry in the 1929 National Air Tour piloted by Ben O Howard.
Eaglerock A-5
Engine: 260hp Menasco-Salmson B-2
Wingspan: 36’8″
Length: 23’10”
Seats: 2

The 1928 Eaglerock A-3 (ATC 59) was powered by a 150hp Hisso A or 180hp Hisso E. they were priced at $3,250.
The 1928 Eaglerock A-4 (ATC 59) was the same as the A-3, but with a 180hp Hisso E, and a nose radiator. A total of ninety-three A-3 and -4 were built.
Eaglerock A-3
Engine: 150hp Hisso A
Length: 24’10”
Useful load: 741 lb
Max speed: 114 mph
Cruise: 97 mph
Stall: 40 mph
Range: 475 mi
Seats: 3
Eaglerock A-3
Engine: 180hp Hisso E
Max speed: 120 mph
Cruise: 103 mph
Stall: 40 mph
Range: 570 mi
Seats: 3

The 1926 Alexander Eaglerock A-2 (ATC 58) was priced at $2,475, rising to $2,000 in 1929. They were also available with 100hp Curtiss OXX-6 engines.

Engine: 90hp Curtiss OX-5 with a chin radiator
Wingspan: 36’8″
Length: 24’11”
Useful load: 983 lb
Max speed: 99 mph
Cruise: 85 mph
Stall: 34 mph
Range: 450 mi
Seats: 3
The 1918 Carolina Corp F Boat was a wood-veneer version of Curtiss F with major design changes, for USN evaluation. It was a two-place open cockpit biplane floatplane powered by a 100hp Curtiss OXX-6.
Although it was overweight to the extreme and incapable of flight, several design changes produced one attractive version that finally did fly, although only a distance of about 25′.
Unfortunately, the Navy demanded longer and higher.
Of three USN s/ns assigned; A4344 to 4346, all were cancelled except A4343.
The 1913 Boland biplane was designed by F. and J. Boland and built by Boland Aeroplane Co. in the USA
Span: 35’6″
Length: 21’2″
Speed: 60 mph

The 1911 Atwood-Wright was a single-place Wright pusher type used for exhibitions.
Possibly it was modified as a wheel version but with flotation tubes under the wing.
The 1913 Atwood appears to be a single-place twin-float blending of Wright and Curtiss design elements, powered by a Roberts pusher.


The 1913 Karpeka-3 biplane was designed and built by A. D. Karpeka in Russia
Span: 36’1″
Length: 24’8″
Loaded Weight: 970 lb

The 1913 Kaishiki No. 5 and 6 biplane was designed and built by the Japanese Army
Span: 50’10”
Length: 36’1″
Empty weight: 1096 lb
Speed: 59 mph
The 1913 Kaishiki No. 3 and No. 4 biplane were scaled-down versions of Kai 2. They were redesigned and built by the Japanese Army, similar but lighter than 1912 Kaishiki No. 2.
Weight: 992 lb