Weight 7,615 lbs (3,454 kg)
CAUTION Refer to General notes and correction factors at the beginning of
this subsection.
Table 5.9.7 - Takeoff Distances (ft) – 7,615 lbs (3,454 kg)
At 50 ft = 99 KIAS – 114 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% 1,450 2,065 100% 1,575 2,215 100% 1,675 2,380
2,000 100% 1,570 2,210 100% 1,740 2,465 100% 1,890 2,645
4,000 100% 1,735 2,455 100% 1,955 2,730 100% 2,105 2,915
6,000 100% 1,950 2,720 100% 2,185 3,020 100% 2,370 3,230
8,000 100% 2,175 3,010 100% 2,465 3,340 100% 2,650 3,570
Pressure
altitude
(ft)
ISA ISA + 10 °C ISA + 20 °C
TRQ * GR
D
50
TRQ * GR
D
50
TRQ * GR
D
50
0 100% 1,805 2,535 100% 1,925 2,695 100% 2,055 2,855
2,000 100% 2,015 2,805 100% 2,155 2,985 100% 2,295 3,160
4,000 100% 2,255 3,110 100% 2,425 3,300 100% 2,590 3,495
6,000 100% 2,540 3,435 100% 2,715 3,645 100% 2,890 3,860
8,000 100% 2,835 3,795 100% 3,030 4,025 100% 3,225 4,260
Pressure
altitude
(ft)
ISA + 30 °C ISA + 37 °C
Associated conditions:
- INERT SEP
ON CAS
message OFF,
- Rotation speed:
V
R
= 90 KIAS,
- 12.5° attitude after
rotation.
TRQ * GR
D
50
TRQ *
GR
D
50
0 100% 2,180 3,020 100% 2,275 3,135
2,000 100% 2,460 3,345 100% 2,565 3,470
4,000 100% 2,750 3,695 100% 2,870 3,840
6,000 100% 3,075 4,080 100% 3,205 4,235
8,000 100% 3,455 4,500 100% 3,595 4,670
* TRQ at brake release
Pilot's Information Manual
Section 5
Performance
PIM TBM 960 - Edition 0
Rev. 01
Page 5.9.9
PIM - DO NOT USE FOR FLIGHT OPERATIONS