Weight 5,512 lbs (2,500 kg)
CAUTION Refer to General notes and correction factors at the beginning of
this subsection.
Table 5.9.1 - Takeoff Distances (ft) – 5,512 lbs (2,500 kg)
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 1,775 100% 1,215 1,880
6,000 100% 1,190 1,850 100% 1,275 1,960 100% 1,360 2,075
8,000 100% 1,335 2,040 100% 1,425 2,160 100% 1,520 2,285
Pressure
altitude
(ft)
ISA + 30 °C ISA + 37 °C
Associated conditions:
- INERT SEP
ON CAS
message OFF,
- Rotation speed:
V
R
= 77 KIAS,
- 15° attitude after
rotation.
TRQ * GR
D
50
TRQ *
GR
D
50
0 100% 1,020 1,630 100% 1,075 1,690
2,000 100% 1,155 1,800 100% 1,205 1,865
4,000 100% 1,290 1,985 100% 1,350 2,060
6,000 100% 1,450 2,190 100% 1,510 2,275
8,000 100% 1,620 2,415 100% 1,695 2,505
* TRQ at brake release
Pilot's Information Manual
Section 5
Performance
PIM TBM 960 - Edition 0
Rev. 01
Page 5.9.3
PIM - DO NOT USE FOR FLIGHT OPERATIONS