Daher-Socata TBM 900 Pilot's Information Manual page 576

SUPPLEMENT 58
FIVE--BLADED PROPELLER
WEIGHT : 7394 lbs (3354 kg)
Associated conditions
:
- Landing gear DN and flaps TO
- 12°5 of attitude - TRQ = 100 %
- "BLEED" switch on "AUTO"
- Hard, dry and level runway
- GR = Ground roll (in ft)
- D = Takeoff distance (clear to 50 ft) (in ft)
50
- Rotation speed choice (V
PRESSURE
ALTITUDE ft
0
2000
4000
6000
8000
PRESSURE
ALTITUDE ft
0
2000
4000
6000
8000
Corrections : . Reduce total distances of 10 % every 10 kts of headwind
. Increase total distances of 30 % every 10 kts of rear wind
. Increase by :
NOTE : Between ISA + 30°C and ISA + 37°C, it may be necessary to cut-off the "BLEED" in order to set
TRQ = 100 % during takeoff while respecting the engine limitations. In this case, reduce power
after takeoff to set the "BLEED" switch to AUTO.
NOTE : In SL ISA conditions, nominal Np is of 1985 RPM.
Page 9.58.18
)
R
85
6500
3000
WEIGHT : 7394 lbs (3354 kg) At 50 ft = 99 KIAS - 114 MPH IAS
ISA - 35°C
GR D50
1440 2020 1560
1555 2170 1690
1685 2325 1820
1810 2500 1970
1960 2695 2220
ISA + 10°C
GR D50
1800 2485 1880
1945 2675 2080
2185 3000 2355
2470 3340 2640
2775 3720 2965
Figure 5.9.3 - TAKEOFF DISTANCES - 7394 lbs (3354 kg)
7 % on hard sod
10 % on short grass
15 % on wet runway
PILOT'S OPERATING HANDBOOK
90
7000 7394
3200 3354
ISA - 20°C
GR D50
2175 1645
2335 1770
2505 1910
2710 2130
3045 2410
ISA + 20°C
GR D50
2595 1965
2865 2215
3200 2500
3550 2810
3950 3180
25 % on high grass
30 % on slippery runway
V (KT)
R
7500
WEIGHT
(LBS)
3400
MASSE (KG)
ISA - 10°C
GR D50 GR
2275 1725
2445 1860
2630 2045
2930 2290
3265 2590
ISA + 30°C
GR D50
2705 2060
3040 2325
3385 2610
3765 2935
4185 3315
Edition 0 -- October 31, 2013
ISA
D50
2380
2560
2785
3135
3490
ISA + 37°C
GR D50
2810
3160
3520
3915
4350
Rev. 1