Weight 6,579 lbs (2,984 kg) – INERT SEP
CAUTION Refer to General notes and correction factors at the beginning of
this subsection.
Table 5.9.4 - Takeoff Distances (ft) – 6,579 lbs (2,984 kg) – INERT SEP
At 50 ft = 94 KIAS – 108 MPH IAS
Pressure
altitude
(ft)
ISA - 35 °C ISA - 20 °C ISA - 10 °C
TRQ * GR
D
50
TRQ * GR
D
50
TRQ * GR
D
50
0 100% 1,035 1,500 100% 1,110 1,605 100% 1,180 1,710
2,000 100% 1,110 1,605 100% 1,225 1,770 100% 1,320 1,895
4,000 100% 1,220 1,765 100% 1,365 1,955 100% 1,475 2,090
6,000 100% 1,360 1,950 100% 1,535 2,165 100% 1,650 2,310
8,000 100% 1,525 2,155 100% 1,715 2,390 100% 1,840 2,550
Pressure
altitude
(ft)
ISA ISA + 10 °C ISA + 20 °C
TRQ * GR
D
50
TRQ * GR
D
50
TRQ * GR
D
50
0 100% 1,260 1,820 100% 1,345 1,930 100% 1,440 2,045
2,000 100% 1,415 2,010 100% 1,510 2,135 100% 1,610 2,260
4,000 100% 1,580 2,225 100% 1,685 2,360 96% 1,820 2,535
6,000 100% 1,765 2,460 100% 1,885 2,610 91% 2,110 2,890
8,000 100% 1,990 2,715 97% 2,145 2,905 86% 2,445 3,305
Pressure
altitude
(ft)
ISA + 30 °C ISA + 37 °C
Associated conditions:
- INERT SEP
ON CAS
message ON,
- Rotation speed:
V
R
= 85 KIAS,
- 15° attitude after
rotation.
TRQ * GR
D
50
TRQ * GR
D
50
0
89% 1,605 2,275 68% 2,105 2,905
2,000 84% 1,850 2,590 67% 2,370 3,250
4,000 80% 2,145 2,970 65% 2,675 3,640
6,000 75% 2,505 3,435 63% 3,045 4,115
8,000 71% 2,965 4,020 61% 3,490 4,685
* TRQ at brake release
Pilot's Information Manual
Section 5
Performance
PIM TBM 960 - Edition 0
Rev. 01
Page 5.9.6
PIM - DO NOT USE FOR FLIGHT OPERATIONS