Attribute | Martin 4-0-4 × | Grumman HU-16 Albatross × |
---|---|---|
General | ||
Manufacturer | Glenn L. Martin Company | Grumman |
Model | Martin 4-0-4 | Grumman HU-16 Albatross |
Country | United States | United States |
Manufactured from (year) | 1951 | 1949 |
Manufactured to (year) | 1953 | 1961 |
Type | Passenger Turbo Props | Amphibious |
Icao | M404 | U16 |
Performance | ||
Engine | 2x Pratt & Whitney R-2800-CB16 | 2x Wright R-1820-76 Cyclone 9 |
Power, hp (hp) | 2,400 | 1,425 |
Max cruise speed (km/h) | 502 | 380 |
Approach speed (km/h) | 130 | 130 |
Travel range (km) | 4,260 | 4,593 |
Fuel economy (km/l) | - | 0.724 |
Service ceiling (m) | 8,839 | 6,553 |
Rate of climb (m/sec) | 9.68 | 7.37 |
Take off distance (m) | 600 | 762 |
Landing distance (m) | 530 | 410 |
Weights | ||
Max take off weight (kg) | 20,366 | 17,010 |
Max landing weight (kg) | 18,231 | 14,965 |
Max payload (kg) | 4,050 | 4,535 |
Fuel tank capacity (l) | 7,571 | 6,469 |
Dimensions | ||
Seats | 4 | 3 |
Cabin height (m) | - | 1.93 |
Cabin width (m) | - | 2.28 |
Cabin length (m) | - | 7.98 |
Exterior length (m) | 22.7 | 19.16 |
Tail height (m) | 8.6 | 7.87 |
Fuselage diameter (m) | 2.9 | 2.4 |
Wing span (m) | 28.42 | 29.46 |
Wing tips | No Winglets | No Winglets |