SOCATA TBM 700 - Page 340

T B M
PILOT’S INFORMATION MANUAL 700
SECTION 5
PERFORMANCE
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Page 5.10.2
Rev. 9
CRUISE PERFORMANCE
Maximum cruise
Conditions : ISA – 205C
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 +2 100 304 239 80.3 231 226 230 225 229 224
5000 – 8 100 275 216 72.6 226 237 225 236 223 235
10000 – 17 100 250 196 66.0 221 249 220 248 218 246
15000 – 26 100 232 182 61.2 216 263 214 261 213 259
18000 – 32 100 223 175 58.9 213 271 211 269 210 267
20000 – 36 100 218 171 57.6 211 277 209 275 208 273
21000 – 37 100 216 170 57.1 210 280 208 278 207 276
22000 – 39 100 214 168 56.5 209 283 207 281 206 279
23000 – 41 100 212 166 56.0 208 286 206 284 205 282
24000 – 43 100 210 165 55.6 207 290 205 287 203 285
25000 – 45 100 209 164 55.3 206 293 204 291 202 288
26000 – 46 100 208 163 54.9 205 296 203 294 201 291
27000 – 48 100 207 162 54.7 204 300 202 297 200 294
28000 – 50 100 206 162 54.4 203 303 201 301 199 298
29000 – 52 100 206 161 54.3 202 307 200 304 198 301
30000 – 54 100 205 161 54.2 201 310 199 308 197 305
Figure 5.10.2 – CRUISE PERFORMANCE –
Maximum cruise / ISA – 20°C
(*) 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).