RCR – ISA + 10 °C
NOTE Conditions:
- ISA + 10 °C,
- Landing gear and flaps UP,
- BLEED switch
on AUTO, and
P2.5 HI and P3 messages OFF.
Table valid only if INERT SEP ON CAS message is OFF.
Power recommended by Daher for better fuel efficiency.
Table 5.11.36 - RCR Performance – ISA + 10 °C
Pressure
altitude
(ft)
OAT
(°C)
TRQ
(%)
Fuel
flow
(USG/h)
Airspeeds (kt)
5,500 lbs
(2,495 kg)
6,300 lbs
(2,858 kg)
7,100 lbs
(3,220 kg)
7,300 lbs
(3,311 kg)
IAS TAS
IAS TAS IAS TAS IAS TAS
SL 26 100 89.1 231 240 235 244 238 247 238 247
5,000 16 89 76.9 215 241 219 245 223 249 225 251
10,000 6 84 68.6 203 245 209 252 213 257 217 262
15,000 -4 86 65.9 201 262 205 267 209 272 211 275
18,000 -10 87 64.2 199 272 205 280 207 283 209 285
20,000 -14 88 63.0 199 281 203 287 205 289 205 289
21,000 -16 89 63.0 199 286 203 291 205 294 205 294
22,000 -18 90 63.0 199 291 203 296 205 299 205 299
23,000 -20 91 63.2 199 295 201 298 205 304 205 304
24,000 -22 90 62.2 199 300 201 303 203 306 203 306
25,000 -24 92 62.5 199 305 201 308 203 311 203 311
26,000 -26 89 60.4 197 307 197 307 199 310 199 310
27,000 -27 85 58.3 193 307 193 307 195 310 195 310
28,000 -29 82 56.4 189 306 189 306 191 309 191 309
29,000 -31 80 54.5 186 305 186 305 187 308 187 308
30,000 -33 77 52.7 182 304 182 304 184 307 184 307
31,000 -35 72 49.9 178 303 178 303 178 303 178 303
Section 5
Performance
Pilot's Information Manual
PIM TBM 960 - Edition 0
Rev. 01
Page 5.11.38
PIM - DO NOT USE FOR FLIGHT OPERATIONS