SOCATA TBM 700 - Page 320

T B M
PILOT’S INFORMATION MANUAL 700
SECTION 5
PERFORMANCE
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Contents
Page 5.7.2
Rev. 9
ENGINE OPERATION
Conditions : Maximum climb power (FL ≤ 200) ISA
Landing gear and flaps UP
IAS = 130 KIAS – Np = 2000 RPM – BLEED LO
NOTE :
Add 1 % of TRQ for each additional 10 KCAS on climb airspeed
T° (°C)
FLIGHT LEVEL (FL)
SAT IOAT 100 110 120 130 140 150 160 170 180 190 200
– 25 – 19
– 23 – 17
– 21 – 15
– 19 – 13
TRQ = 100 %
100
– 17 – 11
TRQ = 100 %
99
– 15 – 09 97
– 13 – 07 100 95
– 11 – 05 98 93
– 09 – 03 100 96 91
– 07 – 01 99 94 89
– 05 + 01 100 97 92 87
– 03 + 03 99 95 90 85
– 01 + 05 97 93 87 82
+ 01 + 07 100 95 90 85 80
+ 03 + 09 98 93 88 82 78
+ 05 + 11 100 95 91 86 80 75
+ 07 + 13 98 93 88 83 78 72
+ 09 + 15 100 95 90 86 81 74 69
+ 11 + 17 100 97 93 88 83 78 71 66
+ 13 + 19 99 95 90 85 80 74 69
+ 15 + 21 100 97 92 88 82 77 71
+ 17 + 23 99 94 90 84 79 67
+ 19 + 25 100 96 92 86 81 67
+ 21 + 27 98 94 88 83 68
+ 23 + 29 100 96 90 76 67
+ 25 + 31 97 84 76 67
+ 27 + 33 84 75 67
+ 29 + 35 74 68
+ 31 + 37 69
CAUTION
THE TRQ SETTING MUST NEVER EXCEED 100 % FOR Np = 2000 RPM
Figure 5.7.1A – ENGINE OPERATION
[Maximum climb power (FL v
200)]