TBM-700 Cruise Performance Data

This information is non-official - copied from a generic TBM-700 Pilot's Information Manual and may ONLY be used for general information purposes. This information MAY NOT, CAN NOT, and MUST NOT be used for flight planning purposes. Only the approved Pilot's Information Manual for the specific aircraft may be used for flight planning.



Normal (Recommended) Cruise
Pressure Altitude (Feet)  IOAT Deg. C TRQ (%) Fuel Flow AIRSPEEDS (kts)
4,850 lbs (2,200 kg) 5,512 lbs (2,500 kg) 6,173 lbs (2,800 kg)
l/hr (1) kg/hr US gal/hr IAS TAS IAS TAS IAS TAS
0 +22 100 312 245 82.3 228 231 227 230 226 229
5,000 +13 100 282 221 74.5 223 243 221 241 220 240
10,000 +3 100 257 201 67.8 217 255 216 253 215 252
15,000 -6 100 237 186 62.5 212 269 211 267 209 265
18,000 -12 100 228 179 60.2 209 278 208 275 206 273
20,000 -15 100 223 175 58.9 207 284 205 281 204 279
21,000 -17 100 221 174 58.5 206 287 204 285 203 282
22,000 -19 100 220 172 58.0 205 290 203 288 202 285
23,000 -21 100 218 171 57.5 204 293 202 291 201 289
**24,000 -22 100 216 170 57.1 203 297 201 294 199 292
**25,000 -24 97 209 164 55.3 199 296 197 294 195 291
**26,000 -26 94 203 159 53.6 195 295 194 293 191 290
27,000 -28 90 196 154 51.9 192 295 190 292 187 287
28,000 -31 86 190 149 50.1 188 294 186 291 183 286
29,000 -33 83 183 144 48.3 184 293 182 289 178 284
30,000 -35 78 176 138 46.5 180 291 177 287 174 282
** Apparent most efficient operating altitudes/temperatures
(1)   l/hr = Liters per hour
Conditions:

• ISA
• Landing gear and flaps UP
• 2,000 RPM (*)
• BLEED LO

(*) Propeller RPM utilization between 1,600 and 2,000 RPM is possible without changing performance. Display the TRQ indicated in table with Np = 2,000 RPM, then reduce Np without resetting power lever (within limits permitted by torque limiter)

Note:

• Power recommended by PRATT & WHITNEY CANADA



Maximum Cruise
Pressure Altitude (Feet)  IOAT Deg. C TRQ (%) Fuel Flow AIRSPEEDS (kts)
4,850 lbs (2,200 kg) 5,512 lbs (2,500 kg) 6,173 lbs (2,800 kg)
l/hr (1) kg/hr US gal/hr IAS TAS IAS TAS IAS TAS
0 +22 100 312 245 82.3 228 231 227 230 226 229
5,000 +13 100 282 221 74.5 223 243 221 241 220 240
10,000 +3 100 257 201 67.8 217 255 216 253 215 252
15,000 -6 100 237 186 62.5 212 269 211 267 209 265
18,000 -12 100 228 179 60.2 209 278 208 275 206 273
20,000 -15 100 223 175 58.9 207 284 205 281 204 279
21,000 -17 100 221 174 58.5 206 287 204 285 203 282
22,000 -19 100 220 172 58.0 205 290 203 288 202 285
23,000 -21 100 218 171 57.5 204 293 202 291 201 289
 24,000 -22 100 216 170 57.1 203 297 201 294 199 292
 25,000 -24 100 215 169 56.8 202 300 200 298 198 295
 26,000 -26 99 209 164 55.2 200 303 198 300 197 298
27,000 -28 95 202 159 53.5 196 302 194 298 193 297
28,000 -30 91 195 153 51.6 192 301 189 297 188 295
29,000 -32 88 188 148 49.8 188 299 186 296 184 293
30,000 -34 84 181 142 47.9 184 298 182 294 178 288
(1)   l/hr = Liters per hour
Conditions:

• ISA
• Landing gear and flaps UP
• 2,000 RPM (*)
• BLEED LO

(*) Propeller RPM utilization between 1,600 and 2,000 RPM is possible without changing performance. Display the TRQ indicated in table with Np = 2,000 RPM, then reduce Np without resetting power lever (within limits permitted by torque limiter)

Note:
• Use recommended cruise power • Power recommended by PRATT & WHITNEY CANADA


Long Range Cruise (5,512 lbs - 2,500kg) LEGEND:
IOAT: Deg. C  IAS: KIAS
ff       : US gal/hr.
ff       : lbs/hr. TAS: KTAS
Pressure Altitude (feet) TRQ (%) ISA -20o C ISA -10o C ISA ISA +10o C ISA +20o C
15,000 60.5 -28 176 -18 174 -8 172 +2 171 +12 169
46.4 47.0 47.6 48.2 48.9
304 214 309 216 311 219 315 221 320 223
18,000 59 -34 171 -24 169 -14 168 -4 166 +6 165
43.2 43.7 44.4 45.0 45.7
282 218 287 221 291 223 295 226 300 228
19,000 58.5 -36 169 -26 167 -16 166 -6 164 +4 163
42.2 42.7 43.4 44.1 44.7
276 220 280 222 284 225 289 227 293 229
20,000 58 -38 168 -28 166 -18 164 -8 163 +2 161
41.2 41.7 42.4 43.1 43.7
269 222 273 224 278 226 282 228 287 231
21,000 57.5 -40 166 -30 164 -20 163 -10 161 0 160
40.4 40.8 41.5 42.1 42.7
265 223 267 225 271 228 276 230 280 232
22,000 57 -42 165 -32 163 -22 161 -12 159 -1 158
39.5 39.9 40.6 41.2 41.7
258 224 262 227 265 229 269 232 273 234
23,000 56.5 -44 163 -34 161 -24 159 -13 158 -3 156
38.7 39.1 39.7 40.3 40.9
254 226 256 228 260 231 265 233 267 235
24,000 56 -46 161 -36 159 -25 158 -15 156 -5 154
37.9 38.3 38.8 39.4 40.0
249 227 251 230 254 232 258 234 262 237
25,000 55.5 -48 159 -38 158 -27 156 -17 154 -7 153
37.2 37.6 38.1 38.6 39.2
243 228 247 231 249 233 254 236 256 238
26,000 55 -50 157 -39 156 -29 154 -19 152 -9 151
36.5 36.9 37.4 37.8 38.3
238 229 243 232 245 235 247 237 251 239
27,000 54.5 -52 156 -41 154 -31 152 -21 151 -11 149
35.8 36.2 36.7 37.1 37.6
234 230 238 233 240 236 243 238 247 240
28,000 54 -53 154 -43 152 -33 151 -23 149 -13 147
35.1 35.5 36.1 36.5 37.0
229 231 234 235 236 237 238 239 243 241
29,000 53.5 -55 152 -45 150 -35 149 -25 147 -15 145
34.6 35.0 35.5 35.9 36.3
227 232 229 236 231 239 236 241 238 242
Conditions:

• ISA
• Landing gear and flaps UP
• 2,000 RPM (*)
• BLEED LO

(*) Propeller RPM utilization between 1,600 and 2,000 RPM is possible without changing performance. Display the TRQ indicated in table with Np = 2,000 RPM, then reduce Np without resetting power lever (within limits permitted by torque limiter)


Long Range Cruise (6,173 lbs - 2,800kg) LEGEND:
IOAT: Deg. C  IAS: KIAS
ff       : US gal/hr.
ff       : lbs/hr. TAS: KTAS
Pressure Altitude (feet) TRQ (%) ISA -20o C ISA -10o C ISA ISA +10o C ISA +20o C
15,000 65.5 -28 179 -18 177 -8 176 +2 174 +12 172
48.1 48.8 49.5 50.1 50.8
315 218 320 220 324 223 328 225 333 227
18,000 64 -34 174 -24 172 -14 171 -4 169 +6 167
45.0 45.7 46.2 47.0 47.6
295 222 300 225 302 227 309 230 311 232
19,000 63.5 -36 172 -26 170 -16 169 -6 167 +4 166
44.1 44.7 45.3 46.0 46.6
289 223 293 226 298 229 302 231 304 233
20,000 63 -38 170 -28 169 -18 167 -8 166 +3 164
43.2 43.7 44.4 45.0 45.6
282 225 287 227 291 230 295 233 298 234
21,000 62.5 -40 169 -30 167 -20 166 -9 164 +1 162
42.3 42.9 43.5 44.1 44.6
278 226 280 229 284 232 289 234 293 236
22,000 62 -42 167 -32 165 -21 164 -11 162 -1 161
41.5 42.0 42.5 43.2 43.7
271 227 276 230 278 233 282 236 287 238
23,000 61.5 -44 165 -34 164 -23 162 -13 161 -3 159
40.6 41.1 41.7 42.3 42.9
267 229 269 232 273 235 278 237 280 239
24,000 61 -46 164 -35 162 -25 161 -15 159 -5 157
39.8 40.3 40.8 41.5 42.0
260 230 265 233 267 236 271 238 276 240
25,000 60.5 -47 162 -37 160 -27 159 -17 157 -7 155
39.0 39.6 40.1 40.7 41.2
256 232 260 235 262 237 267 239 269 241
26,000 60 -49 160 -39 159 -29 157 -19 155 -9 153
38.3 38.8 39.4 39.9 40.4
251 233 254 236 258 239 262 241 265 243
27,000 59.5 -51 159 -41 157 -31 155 -21 153 -11 151
37.6 38.2 38.7 39.2 39.8
247 235 249 237 254 240 258 242 260 244
28,000 59 -53 157 -43 155 -33 153 -23 151 -13 149
37.0 37.5 38.0 38.6 39.1
243 236 245 238 249 241 254 243 256 245
29,000 58.5 -55 155 -45 153 -35 151 -25 149 -15 147
36.5 37.0 37.5 38.0 38.5
238 238 243 239 245 242 249 244 251 246
Conditions:

• ISA
• Landing gear and flaps UP
• 2,000 RPM (*)
• BLEED LO

(*) Propeller RPM utilization between 1,600 and 2,000 RPM is possible without changing performance. Display the TRQ indicated in table with Np = 2,000 RPM, then reduce Np without resetting power lever (within limits permitted by torque limiter)