Models	H75 A-1	H75 A-2	H75 A-3	H75 A-4
Prototype	May 4, 1937	August 18, 1938	Deccember 15, 1938
Wingspan	11.36m	11.36m	11.36m	11.36m
Lenght	8.79m	8.79m	8.79m	8.79m
Height	2.70m	2.70m	2.70m	2.70m
Wing Area	21.92m²	21.92m²	21.92m²	21.92m²
Empty Weight	2138 kg	2138 kg	2138 kg	2138 kg
Maximum weight	2680 kg	2716 kg	2716 kg	2716 kg
Maximum speed	490 km/h at 4000m	500 km/h at 4060m	500 km/h at 4000m	520 km/h at 4600m
Climbing speed	650 m /mn	715 m /mn	715 m /mn	715 m /mn
Service ceilling	9700m	10000m	10000m	9980m
Range	1470 km at 5500m	1470 km at 5500m	1470 km at 5500m	1615 km at 5500m
Motorization	Radial Engine Pratt & Withney R1820 Twin Wasp SCG 14 cylinders air-cooled on 2 levels	Radial Engine Pratt & Withney R1830 Twin Wasp SC2 G 14 cylinders air-cooled on 2 levels	Radial Engine Pratt & Withney R1820 Twin Wasp S1C3G 14 cylinders air-cooled on 2 levels	Radial Engine Wright Cyclone R1820-G205A 14 cylinders air-cooled on 2 levelsx
Power	1050ch on take-off 900ch at 4500m	1200ch on take-off 900ch at 4500m	1200ch on take-off 1050ch at 4500m	1200ch on take-off 1200ch at 4500m
Armament	2 Machine-guns FN Browning of 7.5mm in the wings 2 other in the fuselage	2 or 4 Machine-guns FN Browning of 7.5mm in the wings 2 other in the fuselage	4 Machine-guns FN Browning of 7.5mm in the wings 2 other in the fuselage from No142	4 Machine-guns FN Browning of 7.5mm in the wings 2 other in the fuselage