SECTION 5
PERFORMANCE
T B M
700 PILOT’S INFORMATION MANUAL
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Page 5.10.5
Rev. 9
CRUISE PERFORMANCE
Maximum cruise
Conditions : ISA
Landing gear and flaps UP
2000 RPM (*) – BLEED LO
NOTE :
Use preferably recommended cruise power
AIRSPEEDS (kt)
Pressure
altitude
IOAT
(°C)
TRQ
(%)
Fuel flow
4850 lbs
(2200 kg)
5512 lbs
(2500 kg)
6173 lbs
(2800 kg)
(feet)
( C) (%)
l / h kg / h
us
gal / h
IAS TAS IAS TAS IAS TAS
0 +22 100 312 245 82.3 228 231 227 230 226 229
5000
+13
100 282 221 74.5 223 243 221 241 220 240
10000 +3 100 257 201 67.8 217 255 216 253 215 252
15000 – 6 100 237 186 62.5 212 269 211 267 209 265
18000 – 12 100 228 179 60.2 209 278 208 275 206 273
20000 – 15 100 223 175 58.9 207 284 205 281 204 279
21000 – 17 100 221 174 58.5 206 287 204 285 203 282
22000 – 19 100 220 172 58.0 205 290 203 288 202 285
23000 – 21 100 218 171 57.5 204 293 202 291 201 289
24000 – 22 100 216 170 57.1 203 297 201 294 199 292
25000 – 24 100 215 169 56.8 202 300 200 298 198 295
26000 – 26 99 209 164 55.2 200 303 198 300 197 298
27000 – 28 95 202 159 53.5 196 302 194 298 193 297
28000 – 30 91 195 153 51.6 192 301 189 297 188 295
29000 – 32 88 188 148 49.8 188 299 186 296 184 293
30000 – 34 84 181 142 47.9 184 298 182 294 178 288
Figure 5.10.5 – CRUISE PERFORMANCE –
Maximum cruise / ISA
(*) Propeller RPM utilization between 1600 and 2000 RPM is possible without changing
performance. Display the TRQ indicated in table with Np = 2000 RPM, then reduce Np
without resetting power lever (within limits permitted by torque limiter).
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