Cessna 208B - Page 202

CESSNA
MODEL
2088 (675 SHP)
SECTION
5
PERFORMANCE
CARGO POD INSTALLED
CRUISE PERFORMANCE
PRESSURE ALTITUDE 10,000 FEET
CONDITIONS:
8750 POUNDS
INERTIAL SEPARATOR
- NORMAL
NOTE
-1
Figure 5-17. Cruse Performance (Sheet 6 of 13)
-, 1 Revision 23 U.S. 5-39
-
1. Do not exceed maximum cruise torque or 740°C ITT.
T!Fp
25
20
10
0
-10
-20
-30
40
-50
-54
2. Refer to Sheet 1 for
1900 RPM
TORQUE FUEL KTAS
FT-LBS FLOW
PPH
1176
298 150
1259 310
155
1420
334 163
1295 314
156
1580
364 170
1400
329 161
1265 307
153
1738
394 175
1600
366 169
1400
327 159
1235 300
149
1865 417 178
1700 384 171
1500
344 162
1300 308
152
1235 297
148
1865 414 176
1700 382 169
1500 343 160
1300
306 150
1215 292 145
1865 412 174
1700 380 167
1500
341 158
1300 304 148
1210 289
143
1865 411 172
1700 378
165
1500 340 156
1300 302 146
1200 286 141
1865 411 171
1700 378 164
1500 339
156
1300 301 146
1205 286 140
appropriate notes
1750 RPM
TORQUE FUEL KTAS
FT-LBS FLOW
PPH
1254
298 148
1342 310
154
1320
307 152
1510
334 161
1400
317 156
1305
302 150
1678
364 168
1500
330 159
1295 298 148
1847
394 173
1700
366 167
1500
328 158
1295 295 147
1970 414 176
1800 382 169
1600 344 161
1400
308 151
1285
291 145
1970
412 174
1800
380 167
1600
342 159
1400
306 150
1290
289
144
1970 409 172
1800 377
166
1600 339 157
1400
303 148
1270 283
141
1970 407 170
1800 374 164
1600 337 156
1400 301 147
1245 277 138
1970
406 169
1800 373 163
1600 336 155
1400 300 146
1250 277 138
applicable to this chart.
1600 RPM
TORQUE FUEL KTAS
FT-LBS FLOW
PPH
1335 298 145
1426 310 150
1395 306
149
1600 334
158
1395 302
148
1775 363
165
1600 331
157
1400 300 147
1385 298 146
1949 394 170
1800 365 164
1600 328 155
1400 298
146
1365 292 144
1970 394 169
1800 362
162
1600 325 154
1400 295 144
1345 287 142
1970
390 167
1800 358 161
1600 322 152
1400 292 143
1320 280 139
1970 386 165
1800 355 159
1600 320 151
1400 289 142
1305 275 137
1970 382 163
1800 353 157
1600 317 149
1400 286 140
1300 271 135
1970
381 162
1800 352 156
1600 316 149
1400 285 140
1285 268 134