Douglas C-133
Technical Specifications
| First Flight: |
1957 |
| Number Built: |
50 for USAF Operations |
| Length: |
157 feet 6 inches |
| Wing Span: |
179 feet 8 inches |
| Height: |
48 feet 3 inches |
| Max Take-Off Wt.: |
286,000 lbs. |
| Max Landing Wt.: |
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| Empty Wt.: |
120,262 lbs. |
| Max Cruising Speed: |
359 mph 312 kts |
| Normal Cruising Speed: |
323 mph 281 kts |
| Approach Speed: |
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| Landing Speed: |
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| Stall Speed: |
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| Service Ceiling: |
29,950 feet |
| Fuel Capacity: |
1550 US gallons |
| Range: |
4027 miles with 52,000 lb. payload |
| Fuel Type: |
Jet |
| Fuel Consumption: |
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| Engines: |
4 Pratt & Whitney T-34-P-9W rated at
7500 SHP each |
| Maximum Payload: |
110,000 lbs. or 200 Troops |
| Crew: |
2 Pilots and 1 Flight Engineer/Crew Chief |
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Engine Specifications
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Pratt & Whitney T-34-P-9W
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| Type: |
Turbo-Prop |
| Diameter: |
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| Length: |
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| Bore: |
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| Stroke: |
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| Displacement: |
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| Compression Ratio: |
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| Dry Weight: |
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| Ignition: |
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| Fuel Grade: |
Jet |
| Carburation: |
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