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United States' North American AT-6 trainer1
North American AT-6G and SNJ-7B Texans:
Design
The North American AT-6 Texan became the most produced trainer.1
Prototype
The NA-16, with a fixed undercarriage, first flew in April 1935.1
The NA-26, with retractable undercarriage, first flew in 1937.1
Production
- Produced by:
- North American: 15,1091
- Noorduyn (Canada): 2,6101
Variants
- NA-16: Prototype.1
- NA-26: Prototype.1 Had Pratt & Whitney R-1340 radial engine.1
- BC-1 / Harvard I: First flew in February 1938.1
- BC-1A / Harvard II: Metal skin covering.1 Rudder was straight edged.1
- Harvard IIA: Wood replaced alluminum.1
- Harvard IIB: Canadian produced AT-6A.1
- Harvard III: Electronics upgraded.1 All metal construction.1
- SNJ-1: US Navy trainer.1
- SNJ-2: US Navy trainer.1
- SNJ-3: US Navy trainer.1 Instrument panel was modified.1 Had R-1340-AN engine.1
- SNJ-3C: US Navy trainer.1 Had tailhook.1
- SNJ-4: Wood replaced alluminum.1
- SNJ-5: Electronics upgraded.1 All metal construction.1
- SNJ-6: Canopy was clear.1
- AT-6: Was renamed in 1940 from BC-1A.1
- AT-6A: Instrument panel was modified.1
- AT-6B: Had R-1340-AN engine.1
- AT-6C: Wood replaced alluminum.1
- AT-6D: Electronics upgraded.1 All metal construction.1
- AT-6F: Rear canopy was clear.1
- XAT-6E: Modified AT-6D with Ranger V-770-9 inverted V 12 engine (575 HP).1
Usage
Countries that used the AT-6: Britain, Canada, France, Italy, Japan, Netherlands, New Zealand, South Africa, Southern Rhodesia, Soviet Union, Sweden, and the United States.1
| North American AT-6 Texan1 | North American AT-6C Texan1 | |
|---|---|---|
| Type | Trainer1 | |
| Crew | 21 | |
| Engine (Type) | Pratt & Whitney R-13401 | |
| Cylinders | Radial 91 | |
| Cooling | ||
| HP | 6001 | |
| Propeller blades | 21 | |
| Dimensions | ||
| Span | 42' 0.25"1 12.8 m1 |
|
| Length | 29' 6"1 8.99 m1 |
|
| Height | 11' 8.5"1 3.57 m1 |
|
| Wing area | ||
| Weight | ||
| Empty | 4,158 lb1 1,886 kg1 |
|
| Loaded | 5,300 lb1 2,404 kg1 |
|
| Performance | ||
| Speed | 208 mph1 335 kph1 |
|
| Cruising speed | ||
| Climb | 1,640'/minute1 500 m/minute1 |
|
| Climb to 10,000' / 3,048 m |
7.4 minutes1 | |
| Service ceiling | 21,500'1 6,553 m1 |
|
| Range | 750 miles1 1,207 km1 |
|
| Armament | ||
| Wing roots | 1 or 2: 0.3" MG1 | |
| Rear cockpit | 1: 0.3" MG1 |
Sources:
- Aircraft of WWII, Stewart Wilson, 1998
