RCR – ISA + 20 °C
NOTE Conditions:
- ISA + 20 °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 5.11.37 - RCR Performance – ISA + 20 °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 36 92 85.9 215 228 221 234 229 242 231 244
5,000 26 93 79.6 211 240 217 247 225 256 227 258
10,000 16 95 74.6 211 259 217 266 221 271 223 273
15,000 6 97 72.3 209 277 213 282 217 288 217 288
18,000 0 96 69.5 205 286 211 294 213 296 215 299
20,000 -4 96 68.4 205 295 209 300 211 303 211 303
21,000 -6 95 67.2 205 300 207 303 209 305 211 308
22,000 -8 94 66.1 205 305 205 305 207 308 209 310
23,000 -10 93 65.1 203 307 205 310 205 310 207 313
24,000 -12 92 64.1 199 306 201 309 203 312 203 312
25,000 -14 89 61.8 197 308 197 308 199 311 199 311
26,000 -16 86 59.7 193 308 193 308 195 311 195 311
27,000 -17 83 57.7 189 307 189 307 191 310 191 310
28,000 -19 80 55.7 186 306 186 306 187 309 187 309
29,000 -21 76 52.8 182 305 182 305 182 305 184 308
30,000 -23 73 51.0 178 304 178 304 178 304 178 304
31,000 -25 71 49.3 174 303 174 303 174 303 174 303
Section 5
Performance
Pilot's Information Manual
PIM TBM 960 - Edition 0
Rev. 01
Page 5.11.39
PIM - DO NOT USE FOR FLIGHT OPERATIONS