SOCATA TBM 700 - Page 341

SECTION 5
PERFORMANCE
T B M
700 PILOT’S INFORMATION MANUAL
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Contents
Page 5.10.3
Rev. 9
CRUISE PERFORMANCE
Maximum cruise
Conditions : ISA – 105C
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 +12 100 308 242 81.4 229 228 228 227 227 226
5000
+2
100 279 219 73.6 224 240 223 238 222 237
10000 – 7 100 254 199 67.0 219 252 218 251 216 249
15000 – 16 100 234 184 61.9 214 266 213 264 211 262
18000 – 22 100 225 177 59.4 211 274 209 272 208 270
20000 – 25 100 220 173 58.2 209 281 207 278 206 276
21000 – 27 100 218 171 57.6 208 284 206 281 205 279
22000 – 29 100 216 170 57.1 207 287 205 285 204 282
23000 – 31 100 215 168 56.7 206 290 204 288 202 285
24000 – 33 100 213 167 56.3 205 293 203 291 201 288
25000 – 34 100 212 166 55.9 204 297 202 294 200 291
26000 – 36 100 210 165 55.6 203 300 201 298 199 295
27000 – 38 100 209 164 55.3 202 304 200 301 198 298
28000 – 40 100 209 164 55.2 201 307 199 305 197 302
29000 – 42 97 201 158 53.2 197 307 195 303 193 300
30000 – 44 93 194 152 51.2 193 306 190 301 188 298
Figure 5.10.3 – CRUISE PERFORMANCE –
Maximum cruise / ISA – 10°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).