T B M
PILOT’S INFORMATION MANUAL 700
SECTION 5
PERFORMANCE
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Page 5.10.4
Rev. 9
CRUISE PERFORMANCE
Maximum cruise
Conditions : ISA – 55C
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 +17 100 310 243 81.8 228 230 227 229 226 228
5000 +8 100 280 220 74.1 223 241 222 240 221 238
10000 – 2 100 255 200 67.4 218 254 217 252 216 250
15000 – 11 100 235 185 62.2 213 267 212 265 210 263
18000 – 17 100 226 178 59.8 210 276 208 274 207 272
20000 – 20 100 222 174 58.6 208 282 206 280 205 278
21000 – 22 100 220 173 58.1 207 285 205 283 204 281
22000 – 24 100 218 171 57.5 206 289 204 286 203 284
23000 – 26 100 216 170 57.1 205 292 203 289 202 287
24000 – 28 100 215 168 56.7 204 295 202 293 200 290
25000 – 29 100 213 167 56.3 203 298 201 296 199 293
26000 – 31 100 212 166 56.0 202 302 200 299 198 296
27000 – 33 99 210 165 55.5 200 304 198 301 196 299
28000 – 35 96 202 159 53.5 197 304 194 301 193 298
29000 – 37 92 195 153 51.5 193 303 190 300 188 296
30000 – 39 88 188 147 49.6 188 302 186 298 183 294
Figure 5.10.4 – CRUISE PERFORMANCE –
Maximum cruise / ISA – 5°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).
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