| Type | Aircraft | |
| Company | Groupe Latécoère | |
| Scheme | Monoplane High wing | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
15.0
88.7
|
|
| Height (m) |
0.6
3.6
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
74.8
925
|
|
| Wingspan (Beam) (m) |
0.1
22.4
95
|
|
| Weights | ||
| Empty weight (kg) |
8
4,400
276,800
|
|
| Loaded weight (kg) |
5
6,500
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
3
112
|
|
| Capacity passengers (per.) |
1
10
400
|
|
| Speeds | ||
| Ground Speed (km/h) |
96.6
238.5
1,500
|
|
| Сruise Speed (km/h) |
52
200
3,087
|
|
| Stall Speed (km/h) |
40
114
257.7
|
|
| Power | ||
| Total Power (hp) |
0.4
1,200
60,000
|
3 powerplants 400 hp each |
| Performance | ||
| Service ceiling (m) |
0.6
6,250
161,544
|
|
| Range (Ferry range) (km) |
4
800
40,700
|
|
| Stat | ||
| Number built (qt) |
0
1
43,000
|
|
| Introduction | 1931 | |
| First flight | 02.02.1931 | |
