Grumman G-111 Albatross
Grumman G-111 Albatross Year: 1954 Engine Make/Model: Curtis-Wright R-1820 Cyclone 9HE 9-Cylinder Radial Power (hp): 1475 each Propeller: Hamilton Standard 43D51 3 blade-reversible, feathering Max Takeoff Weight (lbs.): 30,605 on…
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Grumman G-111 Albatross
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| Year: | 1954 | |
| Engine Make/Model: | Curtis-Wright R-1820 Cyclone 9HE 9-Cylinder Radial | |
| Power (hp): | 1475 each | |
| Propeller: | Hamilton Standard 43D51 3 blade-reversible, feathering | |
| Max Takeoff Weight (lbs.): | 30,605 on land; 31,365 on water | |
| Empty Weight (lbs.): | 23,500 | |
| Useful Load, std. (lbs.): | 6,900 (varies by model/equipment) | |
| Fuel Capacity, std. (gals.): | 625 in wing tanks, 400 in floats. Total = 1025 gals. | |
| Wingspan: | 96 ft. 8 in. | |
| Overall Length: | 62 ft. 10 in. | |
| Overall Height: | 25 ft. 10 in. | |
| Wing Area: | 1035 sq. ft. | |
| PERFORMANCE | ||
| Max Speed (KIAS, kts.): | 229 | |
| Cruise Speed (KIAS, kts.): | 145 | |
| Fuel Consumption, Max Cruise (gph): | 110 gph | |
| Rate of Climb, SL (fpm): | 1250 | |
| Vso (kts.): | 64 | |
| Takeoff Distance, Water (ft.): | 2500 | |
| Landing Distance, Water (ft.): | 2000 | |
| Range (Max Payload): | 800 nm | |
| Ferry Range: | 1,450 nm | |
ODEA DeveloperWriter
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