Daher TBM 850, Руководство пилота

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SECTION 5
PERFORMANCE
T B M
850 PILOT’S OPERATING HANDBOOK
Page 5.11.17
Edition 1 -- June 22, 2007
Rev. 14
PRE--GARMIN SOFTWARE VERSION 9.14
Long Range Cruise (5500 lbs -- 2495 kg)
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
15000 45
-- 33
42.2
125
156
190
-- 23
42.6
127
154
192
-- 13
43.2
128
152
194
-- 3
43.7
130
150
195
+ 7
44.2
131
148
196
18000 45
-- 39
39.7
118
152
194
-- 29
40.2
120
150
196
-- 19
40.8
121
148
197
-- 9
41.2
122
146
199
+ 1
41.7
124
145
202
19000 45
-- 41
39.0
116
150
195
-- 31
39.4
117
148
197
-- 21
39.9
119
147
199
-- 11
40.4
120
145
201
-- 1
40.9
121
144
203
20000 45
-- 43
38.2
113
149
197
-- 33
38.7
115
147
199
-- 23
39.1
116
146
201
-- 13
39.6
118
144
203
-- 3
40.1
119
143
205
21000 45
-- 45
37.4
111
148
198
-- 35
37.9
112
146
201
-- 25
38.4
114
145
203
-- 15
38.8
115
143
205
-- 5
39.3
117
142
207
22000 45
-- 46
36.7
109
147
200
-- 36
37.1
110
145
202
-- 26
37.5
112
144
205
-- 16
38.1
113
142
207
-- 6
38.6
115
140
208
23000 45
-- 48
35.9
107
146
202
-- 38
36.4
108
144
205
-- 28
36.8
109
142
206
-- 18
37.3
111
141
208
-- 8
37.8
112
139
210
24000 45
-- 50
35.3
105
145
204
-- 40
35.7
106
143
206
-- 30
36.1
107
141
208
-- 20
36.6
109
139
210
-- 10
37.0
110
138
212
Figure 5.11.17 (1/2) -- 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