TBM-700 Takeoff Performance Data
This information is non-official - copied from a generic TBM-700 Pilot's Information Manual and may ONLY be used for general information purposes. This information MAY NOT, CAN NOT, and MUST NOT be used for flight planning purposes. Only the approved Pilot's Information Manual for the specific aircraft may be used for flight planning.
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WEIGHT: 5,512 lbs. (2,500kg) at 50 ft. - 91
KIAS - 105 MPH IAS
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| Pressure Altitude ft. |
ISA -35o C |
ISA -20o C |
ISA -10o C |
ISA |
| GR |
D50 |
GR |
D50 |
GR |
D50 |
GR |
D50 |
| 0 |
787 |
1,280 |
886 |
1,411 |
951 |
1,493 |
1,017 |
1,591 |
| 2,000 |
886 |
1,411 |
984 |
1,558 |
1,066 |
1,657 |
1,132 |
1,772 |
| 4,000 |
984 |
1,558 |
1,099 |
1,722 |
1,181 |
1,837 |
1,280 |
1,968 |
| 6,000 |
1,099 |
1,722 |
1,230 |
1,903 |
1,329 |
2,051 |
1,444 |
2,215 |
| 8,000 |
1,230 |
1,903 |
1,394 |
2,149 |
1,526 |
2,329 |
1,657 |
2,510 |
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| Pressure Altitude ft. |
ISA +10o C |
ISA +20o C |
ISA +30o C |
ISA +37o C |
| GR |
D50 |
GR |
D50 |
GR |
D50 |
GR |
D50 |
| 0 |
1,083 |
1,690 |
1,148 |
1,788 |
1,214 |
1,903 |
1,247 |
1,969 |
| 2,000 |
1,214 |
1,870 |
1,296 |
1,985 |
1,378 |
2,133 |
1,444 |
2,231 |
| 4,000 |
1,363 |
2,100 |
1,476 |
2,247 |
1,575 |
2,411 |
1,640 |
2,526 |
| 6,000 |
1,575 |
2,379 |
1,690 |
2,559 |
1,837 |
2,756 |
1,919 |
2,887 |
| 8,000 |
1,804 |
2,707 |
1,968 |
2,920 |
2,100 |
3,133 |
2,198 |
3,281 |
Associated Conditions:
• Landing Gear DN and flaps TO
• Np = 2,000 RPM - BLEED LO
• Hard, dry and level runway
• GR = Ground roll (in ft.)
• D50 = Takeoff Distance in feet (clear to 50 ft.)
Note:
Between ISA + 30 Deg. C and ISA + 37 deg. C, it may be necessary to cut-off the Bleed in order to set TQ = 100% during takeoff while respecting the engine limitations. In this case, reduce power after takeoff to set the Bleed ON
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Corrections:
• Reduce total distances of 10% every 10 kt. of headwind
• Increase total distances of 30% every 10 kt. of rear wind
• Other runway surfaces require the following correction factors:
Increase by 7% on hard sod
Increase by 10% on short grass
Increase by 15% on wet runway
Increase by 25% on high grass
Increase by 30% on slippery runway
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WEIGHT: 6,579 lbs. (2,984kg) at 50 ft. - 94 KIAS - 108 MPH IAS
|
| Pressure Altitude ft. |
ISA -35o C |
ISA -20o C |
ISA -10o C |
ISA |
| GR |
D50 |
GR |
D50 |
GR |
D50 |
GR |
D50 |
| 0 |
1,083 |
1,673 |
1,214 |
1,870 |
1,280 |
2,001 |
1,378 |
2,133 |
| 2,000 |
1,214 |
1,870 |
1,345 |
2,067 |
1,444 |
2,198 |
1,542 |
2,362 |
| 4,000 |
1,345 |
2,067 |
1,509 |
2,297 |
1,640 |
2,461 |
1,739 |
2,625 |
| 6,000 |
1,509 |
2,297 |
1,706 |
2,559 |
1,837 |
2,723 |
1,968 |
2,920 |
| 8,000 |
1,706 |
2,559 |
1,903 |
2,854 |
2,067 |
3,051 |
2,231 |
3,281 |
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|
| Pressure Altitude ft. |
ISA +10o C |
ISA +20o C |
ISA +30o C |
ISA +37o
C |
| GR |
D50 |
GR |
D50 |
GR |
D50 |
GR |
D50 |
| 0 |
1,476 |
2,264 |
1,575 |
2,395 |
1,690 |
2,559 |
1,755 |
2,657 |
| 2,000 |
1,673 |
2,493 |
1,772 |
2,657 |
1,903 |
2,854 |
1,969 |
2,953 |
| 4,000 |
1,870 |
2,789 |
2,001 |
2,953 |
2,149 |
3,182 |
2,231 |
3,314 |
| 6,000 |
2,100 |
3,117 |
2,297 |
3,346 |
2,461 |
3,609 |
2,543 |
3,740 |
| 8,000 |
2,428 |
3,543 |
2,657 |
3,839 |
2,854 |
4,134 |
2,969 |
4,298 |
Associated Conditions:
• Landing Gear DN and flaps TO
• Np = 2,000 RPM - BLEED LO
• Hard, dry and level runway
• GR = Ground roll (in ft.)
• D50 = Takeoff Distance in feet (clear to 50 ft.)
Note:
Between ISA + 30 Deg. C and ISA + 37 deg. C, it may be necessary to cut-off the Bleed in order to set TQ = 100% during takeoff while respecting the engine limitations. In this case, reduce power after takeoff to set the Bleed ON
|
|
Corrections:
• Reduce total distances of 10% every 10 kt. of headwind
• Increase total distances of 30% every 10 kt. of rear wind
• Other runway surfaces require the following correction factors:
Increase by 7% on hard sod
Increase by 10% on short grass
Increase by 15% on wet runway
Increase by 25% on high grass
Increase by 30% on slippery runway
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