Daher TBM 850, Руководство пилота

Страница: 498 / 1225

T B M
PILOT’S OPERATING HANDBOOK 850
SECTION 5
PERFORMANCE
Page 5.11.20A
Edition 1 -- June 22, 2007
Rev. 14
POST--GARMIN SOFTWARE VERSION 9.14 or ANY LATER
Long Range Cruise (6300 lbs -- 2858 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 50
-- 52
37.3
111
147
207
-- 42
37.8
112
145
209
-- 32
38.2
113
143
210
-- 22
38.6
115
141
212
-- 12
39.1
116
139
214
25000 53
-- 54
37.6
112
151
216
-- 44
38.0
113
149
218
-- 34
38.5
114
147
220
-- 24
39.0
116
145
221
-- 14
39.5
117
143
223
26000 56
-- 56
38.2
114
154
224
-- 46
38.6
115
152
227
-- 36
39.2
116
150
229
-- 26
39.7
118
148
231
-- 16
40.2
119
146
232
27000 58.5
-- 58
38.7
115
157
232
-- 48
39.1
116
155
234
-- 38
39.6
118
153
236
-- 28
40.1
119
151
238
-- 18
40.6
121
148
240
28000 60.5
-- 60
39.0
116
158
238
-- 50
39.5
117
156
241
-- 40
40.0
119
154
243
-- 30
40.5
120
152
244
-- 20
41.0
122
150
246
29000 61
-- 62
38.7
115
157
241
-- 52
39.1
116
155
243
-- 42
39.7
118
153
245
-- 32
40.1
119
151
247
-- 22
40.7
121
149
249
30000 61.5
-- 64
38.5
114
157
244
-- 54
39.0
116
155
247
-- 44
39.4
117
153
249
-- 34
39.9
119
150
251
-- 24
40.4
120
148
253
31000 62
-- 66
38.2
114
156
247
-- 56
38.7
115
154
250
-- 46
39.2
116
152
252
-- 36
39.7
118
150
254
-- 26
40.2
119
147
256
Figure 5.11.18 (2/2) -- CRUISE PERFORMANCE --
Long Range Cruise (6300 lbs -- 2858 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