MOONEY
M20V ACCLAIM ULTRA
SECTION V
PERFORMANCE
5
−
24
AIRPLANE FLIGHT MANUAL
ORIGINAL ISSUE
−
03-16-2017
CRUISE POWER SETTINGS & FUEL FLOWS
−
BEST ECONOMY
2500
2400
2300
2200
RPM:
Manifold Pressure (inHg):
30.5
29.0
26.0
22.0
30.5
27.0
24.0
21.0
28.0
25.0
22.0
19.0
21.0
ST
AND
ARD
D
A
Y CRUISE FUEL FL
OW (gal/hr) @ 6.0 lb/gal
Pr
. Alt.
STD OA
T
18.5
17.8
16.2
13.8
17.7
15.6
13.7
11.5
15.5
13.5
11.3
9.7
10.8
18.4
17.7
16.1
13.8
17.6
15.7
13.8
11.8
15.6
13.9
12.0
10.0
10.9
18.4
17.6
16.1
13.7
17.6
15.7
14.0
12.1
15.5
13.9
12.1
10.2
10.9
18.3
17.5
16.0
13.6
17.5
15.7
14.1
12.3
15.5
13.9
12.2
10.3
10.9
18.2
17.5
15.9
13.6
17.5
15.7
14.1
12.4
15.5
13.9
12.2
10.4
10.8
18.1
17.4
15.8
13.5
17.4
15.7
14.2
12.5
15.5
13.9
12.2
10.4
10.8
18.1
17.3
15.7
13.5
17.4
15.7
14.2
12.5
15.5
13.9
12.2
10.5
10.8
18.1
17.3
15.7
13.5
17.4
15.7
14.1
12.5
15.5
13.9
12.2
10.5
10.8
18.1
17.3
15.6
13.5
17.4
15.6
14.1
12.5
15.5
13.9
12.2
10.5
10.8
18.0
17.2
15.6
13.5
17.4
15.6
14.1
12.5
15.5
13.9
12.2
10.6
10.9
18.1
17.2
15.6
13.5
17.5
15.6
14.0
12.5
15.5
13.8
12.3
10.6
11.0
18.1
17.2
15.6
13.5
17.5
15.6
14.0
12.5
15.4
13.8
12.3
10.7
11.1
0
2000
4000
6000
8000
10000
12000
14000
16000
18000
20000
22000
18.1
17.2
15.6
13.5
17.5
15.6
14.0
12.6
15.4
13.8
12.3
10.9
11.1
18.1
17.2
15.6
13.5
17.5
15.6
14.1
12.7
15.4
13.8
12.4
11.0
11.2
24000
25000
Note 1: At altitudes above 22,000 feet, power settings above 2300 rpm must be operated at 1675
5
F TIT or richer
.
Note 2: When operating above 30.5 inHg manifold pressure only FULL RICH mixture is permitted. Note 3: Decrease Fuel Flow 0.5 gal/hr for each 10
5
C above standard temperature.
Note 4: Increase Fuel Flow 0.5 gal/hr for each 10
5
C below standard temperature.
Example: for 2500 RPM, 20000 ft Pr
. Alt.,
−
15
5
C OA
T,
30.5 inHg MAP the fuel flow is: 18.4
−
0.5 = 17.9 gal/hr
15
5
C5
9
5
F
11
5
C5
2
5
F
45
5
F
3
5
C
‐1
5
C3
0
5
F
‐5
5
C2
3
5
F
‐9
5
C1
6
5
F
‐13
5
C9
5
F
‐17
5
C2
5
F
‐21
5
C‐
5
5
F
‐25
5
C
‐12
5
F
‐29
5
C
‐19
5
F
‐33
5
C
‐27
5
F
‐35
5
C
‐30
5
F
7
5
C
38
5
F
BEST ECONOMY 50
5
Lean of P
eak TIT
Filled Speed & Fuel Flow table entries indicate
conditions that may not be attainable without ex-
ceeding engine limitation Note 1 on Power Chart