3. TAKEOFF PERFORMANCE | Main page | Previous | Next |
Lockheed 1049G/C121G Super Constellation
Operations Manual Synopsis
Takeoff Performance, Distance in Feet Standard Day Takeoff Distances and Performance Factor values |
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Gross Wt. Lbs. |
Kts IAS |
Sea Level |
1,000 Ft. |
2,000 Ft. |
3,000 Ft. |
4,000 Ft. |
5,000 Ft. |
6,000 Ft. |
90,000 | 98 | 1,400 | 1,400 | 1,400 | 1,600 | 1,800 | 1,900 | 2,100 |
100,000 | 103 | 1,700 | 1,700 | 1,700 | 2,100 | 2,300 | 2,400 | 2,600 |
110,000 | 108 | 2,200 | 2,200 | 2,200 | 2,600 | 2,800 | 3,000 | 3,300 |
120,000 | 113 | 2,700 | 2,700 | 2,700 | 3,200 | 3,500 | 3,800 | 4,100 |
130,000 | 118 | 3,300 | 3,300 | 3,300 | 3,900 | 4,200 | 4,600 | 5,000 |
140,000 | 122 | 4,200 | 4,200 | 4,200 | 4,900 | 5,300 | 5,700 | 6,300 |
T.O. Factor |
2 | 2 | 2 | 3.8 | 4.8 | 5.9 | 7.0 | |
Thrust Factor |
52 | 51.8 | 51.4 | 52.6 | 53.6 | 55.4 | 55 | |
* T.O. Factor for standard day power, Low Blower, 2900 RPM,
Max. BMEP, (page A3-14, figure A-3-5). Used in flight performance graphs. * Thrust Factor for standard day power, Low Blower, (A-3-15, figure A3-6). Used in flight performance graph calculations. * Climb Performance Factor graph A3-32, figure A3-20 (Sheet 1 of 3) uses Thrust Factor to obtain Climb Performance Factor. Factor values are use other in flight performance graphs to calculate additional performance parameters under all possible conditions. * Ground Run distance is for a standard day, no wind, level runway, and no obstacles (page A-30, figure A-3-18). To clear a 50-foot obstacle, add the appropriate distance from Obstacle Clearance Table 5 to the distance from the above table. * Ground Run Acceleration, Distance, and Time can be calculated (page A-31, figure A3-19). |
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