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