The Globe Swift
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Back in my early days as a Flight Instructor we used to fly our dual cross country training flights to an airport in Ohio because of a great "on airport" restaurant. Across from the restaurant sitting out on the ramp was a Globe Swift. It was bare aluminum and pretty cool looking, I wonder where it is today? |
![]() The Globe Swift was designed by Mr. R.S. "Pop" Johnson in 1940 and is a light, two-seat sport monoplane with retractable main landing gears and usually equipped with a constant speed propeller (although a fixed pitch propeller is also listed in the original May 7, 1946 type certificate number ATC#-766.) |
![]() The Ft. Worth, Texas located Globe Aircraft Company soon became backlogged with orders so they entered a contract with the nearby (newly founded) Grand Prairie, Texas company TEMCO (Texas Engineering & Manufacturing Company) to build GC-1B Swifts under sub-contract. |
| Globe Swift GC-1B | |
| • Manufacturer: Globe Aircraft/TEMCO | |
| • Total Built: 1,521 (including prototypes) | |
| • Original Base Price: $3750-$4000 | |
| • Varients: 3- (GC-1A, GC-1B, T-35 “Buckaroo”) | |
| • First Flight: The prototype GC-1A made its initial test flights in January, 1945 | |
| • Crew: 1 | |
| • Capacity: 2 | |
| • Wingspan: 29 ft 4 in. (8.94 m) | |
| • Wing Area: 132 ft² (12.3 m²) | |
| • Airfoil: Root NACA 23015, Tip NACA 23009 | |
| • Height: 6 ft 2 in. (1.88 m) | |
| • Length: 20 ft 10 in. (6.35 m) | |
| • Empty weight: 1,370 lb. (621 kg) | |
| • Maximum Takeoff Weight: 1,710 lb. (766 kg) | |
| • Total Fuel: 27.8 gals. | |
| • Powerplant: 1 × Continental C125 six cylinder, four-stroke aircraft engine, 125 hp (93 kW) | |
| Performance | |
| • Cruise speed: 122 kts (140 mph; 226 km/h) | |
| • Climb Performance: 700 ft/min (3.6 m/s) | |
| • Never Exceed speed: 161 kts (185 mph; 298 km/h) | |
| • Range: 1,000 nm (1,151 mi; 1,852 km) | |
| • Service Ceiling: 18,000 ft. (5,500 m) | |


