Daher TBM 850, Pilot'S Information Manual

Page: 496 / 1225

T B M
PILOT’S OPERATING HANDBOOK 850
SECTION 5
PERFORMANCE
Page 5.11.18A
Edition 1 -- June 22, 2007
Rev. 14
POST--GARMIN SOFTWARE VERSION 9.14 or ANY LATER
Long Range Cruise (5500 lbs -- 2495 kg) (Cont’d)
Conditions : Landing gear and flaps UP
Np = 2000 RPM (*)
BLEED switch on AUTO and BLEED HI msg OFF
Pressure
altitude
(feet)
TRQ
(%)
ISA
-- 20 ° C
ISA
-- 10 ° C
ISA
ISA
+ 10 ° C
ISA
+ 20 ° C
24000 45
-- 52
35.3
105
145
204
-- 42
35.7
106
143
206
-- 32
36.1
107
141
208
-- 22
36.6
109
139
210
-- 12
37.0
110
138
212
25000 49
-- 54
35.9
107
150
215
-- 44
36.4
108
148
217
-- 34
36.9
110
146
219
-- 24
37.4
111
145
222
-- 14
37.9
113
143
224
26000 52
-- 56
36.6
109
153
223
-- 46
37.1
110
151
226
-- 36
37.6
112
150
229
-- 26
38.0
113
148
231
-- 16
38.5
114
147
233
27000 54
-- 58
36.8
109
155
230
-- 48
37.3
111
153
232
-- 38
37.8
112
152
235
-- 28
38.2
114
150
237
-- 18
38.8
115
148
240
28000 55.5
-- 60
36.9
110
156
235
-- 50
37.4
111
154
238
-- 40
37.9
113
153
241
-- 30
38.3
114
151
243
-- 20
38.8
115
149
245
29000 56
-- 62
36.6
109
156
238
-- 52
37.1
110
154
241
-- 42
37.5
111
152
244
-- 32
38.0
113
150
246
-- 22
38.5
114
148
248
30000 56.5
-- 64
36.4
108
155
242
-- 54
36.9
110
154
245
-- 44
37.3
111
152
247
-- 34
37.8
112
150
250
-- 24
38.3
114
148
252
31000 57
-- 66
36.1
107
155
246
-- 56
36.6
109
153
248
-- 46
37.0
110
151
250
-- 36
37.5
111
149
253
-- 26
38.0
113
147
255
Figure 5.11.17 (2/2) -- CRUISE PERFORMANCE --
Long Range Cruise (5500 lbs -- 2495 kg) (Altitude
≥
24000 ft)
(*) Propeller RPM utilization between 1600 and 2000 RPM is possible without changing
performance. Display the TRQ indicated in table with Np = 2000 RPM, then reduce Np
without exceeding 121.4 % TRQ.
LEGEND : OAT : ° C IAS : KIAS
FF : us gal/h
FF : kg/h TAS : KTAS
PIM - DO NOT USE FOR FLIGHT OPERATIONS