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SOCATA TBM 700 - Page 321

SOCATA TBM 700
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SECTION 5
PERFORMANCE
T B M
700 PILOTS INFORMATION MANUAL
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Contents
Page 5.7.3
Rev. 9
ENGINE OPERATION
Conditions : Maximum climb power (FL w 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 200 210 220 230 240 250 260 270 280 290 300
65 58 100 94
63 56 97 92
61 54 100 95 90
59 52 99 93 88
57 50 97 91 85
55 48
TRQ = 100 %
100 94 89 84
53 46
TRQ = 100 %
98 92 87 82
51 44 100 95 90 85 80
49 42 99 93 88 83 79
47 40 97 92 87 82 77
45 38 100 95 90 85 80 76
43 36 98 93 88 83 79 75
41 34 97 92 87 82 78 73
39 32 100 95 90 85 81 76 72
37 30 98 94 89 84 79 74 70
35 28 97 92 87 82 77 73 68
33 26 100 95 91 86 81 76 71 66
31 25 99 94 89 84 79 74 69 65
29 23 97 92 87 82 77 72 68 63
27 21 100 95 90 85 80 75 70 66 61
25 19 98 93 88 83 78 73 69 64 59
23 17 100 95 91 86 81 76 71 67 62 58
21 15 98 94 89 84 79 74 70 65 60 57
19 13 100 96 92 87 82 77 73 68 63 59 55
17 11 99 94 90 85 80 75 71 66 61 57 53
15 09 97 92 88 83 78 74 69 64 59 55
13 07 95 90 86 81 76 72 67 62 57 53
11 05 93 88 84 79 74 70 65 60 55
09 03 91 86 82 77 72 68 63 58 53
07 01 89 84 80 75 70 65 60 56
05 + 01 87 82 77 73 68 63 58 54
03 + 03 85 80 75 70 66 60 55
01 + 05 82 78 73 68 63 57 53
+ 01 + 07 80 75 70 65 60 55
+ 03 + 09 78 73 67 62 57
+ 05 + 11 75 70 65 59
+ 07 + 13 72 67 62
+ 09 + 15 69 64
+ 11 + 17 66
CAUTION
THE TRQ SETTING MUST NEVER EXCEED 100 % FOR Np = 2000 RPM
Figure 5.7.1B ENGINE OPERATION
[Maximum climb power (FL
w 200)]
Figure 5.7.2

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