Weight 7,394 lbs (3,354 kg)
CAUTION Refer to General notes and correction factors at the beginning of
this subsection.
Table 5.9.5 - Takeoff Distances (ft) – 7,394 lbs (3,354 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% 1,395 1,990 100% 1,500 2,135 100% 1,610 2,290
2,000 100% 1,495 2,130 100% 1,670 2,375 100% 1,800 2,545
4,000 100% 1,665 2,365 100% 1,865 2,625 100% 2,020 2,805
6,000 100% 1,855 2,615 100% 2,100 2,905 100% 2,255 3,105
8,000 100% 2,090 2,890 100% 2,345 3,210 100% 2,520 3,430
Pressure
altitude
(ft)
ISA ISA + 10 °C ISA + 20 °C
TRQ * GR
D
50
TRQ * GR
D
50
TRQ * GR
D
50
0 100% 1,720 2,440 100% 1,835 2,590 100% 1,955 2,745
2,000 100% 1,920 2,700 100% 2,065 2,870 100% 2,205 3,040
4,000 100% 2,165 2,990 100% 2,310 3,175 100% 2,465 3,360
6,000 100% 2,415 3,305 100% 2,580 3,505 100% 2,750 3,710
8,000 100% 2,700 3,645 100% 2,880 3,865 100% 3,095 4,090
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% 2,095 2,905 100% 2,185 3,015
2,000 100% 2,345 3,215 100% 2,440 3,335
4,000 100% 2,620 3,550 100% 2,730 3,690
6,000 100% 2,950 3,920 100% 3,075 4,070
8,000 100% 3,285 4,320 100% 3,425 4,485
* TRQ at brake release
Pilot's Information Manual
Section 5
Performance
PIM TBM 960 - Edition 0
Rev. 01
Page 5.9.7
PIM - DO NOT USE FOR FLIGHT OPERATIONS