Specifications

Engines

Gnôme-Rhône 14 N-38/39
Gnôme-Rhône 14 N-48/49

Dimensions

Wing span: 22.52 m
Length: 17.17 m
Height: 5.24 m
Landing gear width: 5.49 m
Propellers diameter: 3.20 m

Aerodynamic data

Wing surface 68 m2

Airfoils:

Weights and loads

Total fuel capacity: 3225 l (in 6 tanks and one reserve(?))
Main fuel tanks located between wing roots and engine nacelles
Auxiliary fuel tanks in wings outside of engine nacelles
Oil capacity: 154 l (in 2 tanks)
Empty weight (equipped): 7,820 kg
Loaded weight: 11,400 kg

Detailed weights for LeO.450 with Hispano-Suiza 14AA engines:
airframe
3,700 kg
powerplants
2,150 kg
tanks
109 kg
fixed equipment
330 kg
total empty weight
6,390 kg
mobile equipment
1,050 kg
crew
354 kg
useful load:
fuel between 1,260 to 2,360 kg
payload between 500 to 2,000 kg
2,876 kg
total useful load
4,280 kg
normal total weight
10,650 kg
maximum total weight (with 5,330 kg useful load)
11,700 kg
wing loading
157 kg / m2
power loading
4.70 kg / hp

Performance

Max speed: 495 km/h at 4,800 m
Cruise speed: 360 km/h at 1,600 m
Range with 500 kg bombload: 2,300 km
Climb to 5,000 m: 14'
Ceiling: 9,000 m

Speed-vs-alt and climb rate curves


Reception test requirements (before weapons were fitted):

Armament

Offensive armament

One bomb bay in each wing root, one bomb bay in fuselage (port side).
Total theoretical bomb load was 2,100 kg.

One Bronzavia B 30 main bomb sight, with target heading displayed to the pilot's type 11 indicator
One D 40 emergency bomb sight (not fitted on all aircraft?)

Defensive armament