SOCATA TBM 700 - Page 313

SECTION 5
PERFORMANCE
T B M
700 PILOT’S INFORMATION MANUAL
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Contents
Page 5.4.1
Rev. 2
5.4 – SAT – IOAT CONVERSIONS
NOTE :
These indicated temperatures are available for stabilized cruise at normal
operating power.
Pressure
ISA – 20°C ISA – 10°C ISA ISA + 10°C ISA + 20°C
altitude
(feet)
SAT IOAT SAT IOAT SAT IOAT SAT IOAT SAT IOAT
SL – 05 02 05 12 15 22 25 32 35 42
2000 – 09 – 02 01 08 11 18 21 28 31 38
4000 – 13 – 06 – 03 04 07 14 17 25 27 35
6000 – 17 – 10 – 07 00 03 11 13 21 23 31
8000 – 21 – 13 – 11 – 03 – 01 07 09 17 19 27
10000 – 25 – 17 – 15 – 07 – 05 03 05 13 15 23
12000 – 29 – 21 – 19 – 11 – 09 – 01 01 10 11 20
14000 – 33 – 25 – 23 – 14 – 13 – 04 – 03 06 07 16
16000 – 37 – 28 – 27 – 18 – 17 – 08 – 07 02 03 12
18000 – 41 – 32 – 31 – 22 – 21 – 12 – 11 – 01 – 01 08
20000 – 45 – 36 – 35 – 26 – 25 – 15 – 15 – 05 – 05 04
22000 – 48 – 39 – 38 – 29 – 28 – 19 – 18 – 09 – 08 00
24000 – 52 – 43 – 42 – 33 – 32 – 23 – 22 – 13 – 12 – 04
26000 – 56 – 47 – 46 – 36 – 36 – 27 – 26 – 17 – 16 – 08
28000 – 60 – 50 – 50 – 40 – 40 – 31 – 30 – 21 – 20 – 12
30000 – 64 – 54 – 54 – 45 – 44 – 35 – 34 – 26 – 24 – 16
Figure 5.4.1 – SAT – IOAT CONVERSIONS