SECTION 5
PERFORMANCE
T B M
700 PILOT’S 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 –