Comparison of Airbus A400M and Lockheed L-188 Electra

Attribute	Airbus A400M ×	Lockheed L-188 Electra ×
General
Manufacturer	Airbus	Lockheed Martin Aeronautics
Model	Airbus A400M	Lockheed L-188 Electra
Country	France	United States
Manufactured from (year)	2009	1957
Manufactured to (year)	-	1961
Type	Military Propellor Planes	Passenger Turbo Props
Icao	A400	L188
Performance
Engine	4x 4 × EuroProp International TP400-D6	4x Allison 501-D13
Power, hp (hp)	11,000	3,750
Avionics	-	Bendix Weather Radar, MLS, GPS
Max cruise speed (km/h)	780	648
Approach speed (km/h)	241	222
Travel range (km)	8,890	3,519
Fuel economy (km/l)	0.083	-
Service ceiling (m)	12,192	8,656
Rate of climb (m/sec)	15.24	10.01
Take off distance (m)	980	1,439
Landing distance (m)	770	1,311
Weights
Max take off weight (kg)	141,000	51,256
Max landing weight (kg)	123,000	44,499
Max payload (kg)	37,000	15,300
Fuel tank capacity (l)	62,879	20,895
Baggage volume (m³)	342	15
Dimensions
Seats	116	98
Cabin height (m)	3.85	1.93
Cabin width (m)	4	2.74
Cabin length (m)	17.71	20.02
Exterior length (m)	43.8	31.85
Tail height (m)	14.7	10.01
Fuselage diameter (m)	4.1	3.2
Wing span (m)	42.4	30.18
Wing tips	No Winglets	No Winglets