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Mooney M20f
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Aircraft Type: |
1967 Mooney
M20f Executive 21 |
|
Registration
Number: |
N9576M |
|
Current Hourly
(wet) Rate: |
$102 |
|
Engine: |
200 HP Lyc.
10-360-A1A |
|
Maximum Gross
Weight: |
2,740 Lb |
|
Maximum Useful
Load: |
1067 Lb |
|
Maximum Usable
Fuel: |
64 Gallons
(384 Lb) |
|
Fuel Type: |
100 LL |
|
Normal Rotation
Speed: |
70 Mph
(15º flaps) |
|
Best Angle of
Climb Speed,
Vx |
94 Mph
(15º flaps) |
|
Best Rate of
Climb Speed,
Vy |
113 Mph |
|
Maneuvering Speed:
(@ Gross Weight) |
135 Mph |
|
Normal Landing
Speed: |
80 Mph |
|
Stall Speed:
(@ Max Gr Wt /
Full Flaps) |
62 Mph IAS |
|
Best Glide
Speed: |
104 Mph |
|
Glide Ratio:
(Prop Windmilling,
Gear & Flaps Up) |
10.3:1
1.7 NM / 1000' |
|
Altitude |
RPM |
Mn. Pressure |
Power |
TAS |
GPH |
Endurance |
|
2,500 |
2400 |
22" |
64% |
134 Knots |
9.3 |
6 Hours
53 Min. |
|
5,000 |
2400 |
22" |
66% |
148 Knots |
9.7 |
6 Hours
36 Min. |
|
7,500 |
2400 |
21" |
64% |
149 Knots |
9.4 |
6 Hours
49 Min. |
|
10,000 |
2400 |
21" |
66% |
153 Knots |
9.7 |
6 Hours
36 Min. |
|
12,500 |
2600 |
17.5" |
60% |
152 Knots |
9.3 |
6 Hours
53 Min. |
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All information
provided with no warranty as to its accuarcy. Endurance figures based
on theoretical optimum with no allowance for taxi, take off,
condition of airframe, etc. Consult the Operating Handbook for this
or any aircraft you intend to fly. |
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