TA-3
Dayton-Wright (Trainer, Air-cooled type 3), 13 built, 80 hp (60 kW) Le Rhone 9C rotary engine, wingspan 30 ft 11 in (9.4 m), Length 22 ft 7 in (6.9 m), gross weight 1,753 lb (795 kg)
TA-5
Single TA-3 with Lawrance J-1 engine used for tests of a single-wheel landing gear arrangement in 1923.

TW-3
Dayton-Wright (Trainer, Water-cooled type 3), two built, 150 hp (112-kW) Wright-Hispano I engine wingspan 34 ft 9 in (10.6 m), Length 25 ft 7 in (7.8 m), gross weight 2,447 lb (1019 kg)
TW-3
Consolidated (Trainer, Water-cooled type 3), 20 built, 180 hp (134 kW) Wright-Hispano E engine wingspan 34 ft 9 in (10.6 m), Length 26 ft 9 in (8.1 m), gross weight 2,407 lb (1,092 kg)
PT-1
Consolidated (Primary Trainer number 1), 221 built, 180 hp (134 kW) Wright-Hispano E (V-720) engine
XPT-2
PT-1 with 225 hp (168 kW) Wright R-790 (J-5) engine, wingspan 34 ft 7 in (10.5 m), Length 28 ft 4 in (8.6 m), gross weight 2,427 lb (1,100 kg)
TA-3
Dayton-Wright (Trainer, Air-cooled type 3), 13 built, 80 hp (60 kW) Le Rhone 9C rotary engine, wingspan 30 ft 11 in (9.4 m), Length 22 ft 7 in (6.9 m), gross weight 1,753 lb (795 kg)
TA-5
Single TA-3 with Lawrance J-1 engine used for tests of a single-wheel landing gear arrangement in 1923.
TW-3
Dayton-Wright (Trainer, Water-cooled type 3), two built, 150 hp (112-kW) Wright-Hispano I engine wingspan 34 ft 9 in (10.6 m), Length 25 ft 7 in (7.8 m), gross weight 2,447 lb (1019 kg)
TW-3
Consolidated (Trainer, Water-cooled type 3), 20 built, 180 hp (134 kW) Wright-Hispano E engine wingspan 34 ft 9 in (10.6 m), Length 26 ft 9 in (8.1 m), gross weight 2,407 lb (1,092 kg)
PT-1
Consolidated (Primary Trainer number 1), 221 built, 180 hp (134 kW) Wright-Hispano E (V-720) engine
XPT-2
PT-1 with 225 hp (168 kW) Wright R-790 (J-5) engine, wingspan 34 ft 7 in (10.5 m), Length 28 ft 4 in (8.6 m), gross weight 2,427 lb (1,100 kg)
Consolidated PT-1 Trusty