| Type | Aircraft | |
| Company | Lockheed Corporation | |
| Scheme | Low wing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
8.3
88.7
|
|
| Height (m) |
0.6
2.8
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
27.3
925
|
|
| Weights | ||
| Empty weight (kg) |
8
1,945.5
276,800
|
|
| Loaded weight (kg) |
5
3,220.1
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
2
112
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
298
28,165
|
|
| Сruise Speed (km/h) |
52
241.4
3,087
|
|
| Fuel | ||
| Fuel Capacity (l) |
23
1,574.7
320,000
|
|
| Performance | ||
| Service ceiling (m) |
0.6
7,955
161,544
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
390
36,000
|
|
| Stat | ||
| Introduction | 1929 | |
| First flight | 1929 | |
