MOONEY
M20V ACCLAIM ULTRA
SECTION V
PERFORMANCE
5
−
32
AIRPLANE FLIGHT MANUAL
ORIGINAL ISSUE
−
03-16-2017
Conditions:
Example:
Mixture:
Pressure Altitude:
12000 ft
Best Economy (50
F Lean of Peak TIT)
Propeller Speed:
2300 RPM
Manifold Pressure:
28.0 in HG
Cruise Weight:
3100 LB
Outside Air Temp:
−
8
C
Altimeter:
Set to 29.92
True Airspeed:
196 KTAS
Configuration:
Clean
Fuel Flow:
15.6 GPH
SPEED and POWER SETTINGS vs ALTITUDE
−
(BEST ECONOMY)
D
ISA:
−
30
(
−
59)
5
C
0
(
−
28)
5
C
30
(2)
5
C
25000 Ft. Pressure Altitude
D
ISA:
−
30
(
−
55)
5
C
0
(
−
24)
5
C
30
(6)
5
C
24000 Ft. Pressure Altitude
Some (low) power settings may not be attainable
due to low cylinder or oil temperatures depending
on ambient conditions
Filled Speed & Fuel Flow table entries indicate
conditions that may not be attainable without ex-
ceeding engine limitation Note 1 on Power Chart
(OAT)
−
54
(
−
84)
5
F
0
(
−
30)
5
F
54
(24)
5
F
RPM
MAP
KTAS
GPH
KTAS
GPH
KTAS
GPH
2500
30.5
235
19.4
236
18.3
234
17.0
2500
29.0
231
18.4
232
17.4
229
16.2
2500
26.0
222
16.7
222
15.7
219
14.6
2500
22.0
208
14.6
208
13.7
204
12.7
2400
30.5
232
18.8
233
17.7
230
16.5
2400
27.0
222
16.7
223
15.7
220
14.7
2400
24.0
213
15.1
213
14.2
209
13.2
2400
21.0
203
13.6
202
12.8
197
11.9
2300
28.0
221
16.5
221
15.6
218
14.5
2300
25.0
212
14.9
212
14.0
208
13.0
2300
22.0
201
13.3
200
12.5
196
11.6
2300
19.0
189
11.8
188
11.1
182
10.3
2200
21.0
192
12.0
190
11.3
185
10.5
(OAT)
−
54
(
−
81)
5
F
0
(
−
27)
5
F
54
(27)
5
F
RPM
MAP
KTAS
GPH
KTAS
GPH
KTAS
GPH
2500
30.5
234
19.4
234
18.3
232
17.0
2500
29.0
229
18.4
230
17.4
228
16.2
2500
26.0
220
16.7
221
15.7
217
14.6
2500
22.0
207
14.5
206
13.7
203
12.7
2400
30.5
231
18.8
231
17.7
228
16.5
2400
27.0
220
16.7
221
15.7
218
14.6
2400
24.0
211
15.1
211
14.2
207
13.2
2400
21.0
200
13.5
200
12.7
196
11.8
2300
28.0
220
16.6
219
15.6
216
14.5
2300
25.0
210
14.9
210
14.0
206
13.0
2300
22.0
200
13.3
198
12.5
194
11.6
2300
19.0
187
11.7
185
11.0
180
10.2
2200
21.0
191
12.0
189
11.3
184
10.5
