Weight 5,512 lbs (2,500 kg) – INERT SEP
CAUTION Refer to General notes and correction factors at the beginning of
this subsection.
Table 5.9.2 - Takeoff Distances (ft) – 5,512 lbs (2,500 kg) – INERT SEP
At 50 ft = 91 KIAS – 105 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% 705 1,150 100% 755 1,225 100% 800 1,300
2,000 100% 750 1,225 100% 825 1,345 100% 890 1,435
4,000 100% 825 1,340 100% 920 1,480 100% 985 1,575
6,000 100% 915 1,475 100% 1,020 1,630 100% 1,110 1,740
8,000 100% 1,015 1,625 100% 1,155 1,800 100% 1,245 1,920
Pressure
altitude
(ft)
ISA ISA + 10 °C ISA + 20 °C
TRQ * GR
D
50
TRQ * GR
D
50
TRQ * GR
D
50
0 100% 850 1,380 100% 905 1,460 100% 960 1,545
2,000 100% 945 1,520 100% 1,005 1,610 100% 1,085 1,705
4,000 100% 1,065 1,675 100% 1,140 1,775 96% 1,230 1,900
6,000 100% 1,190 1,850 100% 1,275 1,960 91% 1,410 2,160
8,000 100% 1,335 2,040 97% 1,440 2,180 86% 1,640 2,460
Pressure
altitude
(ft)
ISA + 30 °C ISA + 37 °C
Associated conditions:
- INERT SEP
ON CAS
message ON,
- Rotation speed:
V
R
= 77 KIAS,
- 15° attitude after
rotation.
TRQ * GR
D
50
TRQ * GR
D
50
0
89% 1,080 1,710 68% 1,415 2,160
2,000 84% 1,235 1,935 67% 1,595 2,400
4,000 80% 1,430 2,205 65% 1,780 2,670
6,000 75% 1,675 2,530 63% 2,025 3,000
8,000 71% 1,960 2,940 61% 2,290 3,385
* TRQ at brake release
Pilot's Information Manual
Section 5
Performance
PIM TBM 960 - Edition 0
Rev. 01
Page 5.9.4
PIM - DO NOT USE FOR FLIGHT OPERATIONS