Mooney M20M - Page 32

SERVICE
AND
MAINTENANCE
MANUAL M20M
MOONEY
AIRCRAFT
CORPORATION
AIRFRAME
STANDARD
M
ETRI
C10 PT/M
I SC
WEIGHTS 8
LOADINGS:
A.
Approximate
Empty Weight
2100
Ib.
953
Kg.
B.
GrossWeight
(27-0001
thru
27-0052)*
3200
Ib.*
1452
KS.X
(27-0053
thru
27-TEA)
3368
Ib. 1528
Kg.
C.
Average
Useful Load
1100
Ib.
521.63
Kg.
D.
Wing
Loading.
18.3
Lbs./Sq.Ft.
E.
Power
Loading
11.85
Ib/hp.
5.4
Kgkp
Retrofit of these
A/C
to
3368
Gross
Weight
is
allowed
when
compliance
with SE
M20-248
is
accomplished.
WINGS:
A.
Airfoil
AtWing
Root
632215
B.
Airfoil
At
Wing
Tip
641412
C. Mean
Aerodynamic
dhord
At
Wing
Sta.94.85
61
in.
241
cm
D.
Center-of-Gravity
Range.
41.0
to51.0
E.
Geometric
Twist
(DEG)
1.5"
F.
Incidence
Angle
(DEG)
From
Sta
20.
to
Wing
Tip
2.50
G.
Dihedral
angle
(DEG)
5.50
H.
Aspect
Ratio
7.448
i.
Taper
Ratio
(CS/CT)
2.271
FUSELAGE:
A.
Cabin Dimensions:
(1)
Height
44.5"
113
cm
(2)
Width
43.5"
110.5
cm
(3)
Length
126".
315 cm
(4)
Cabin Door Width
29".
73.4
cm
(5)
Cabin Door
Height.
35".
88.9
cm
B.
Baggage
Campartment:
(1)
MAX.Loading
120
\bs
54.4
kg
(2)
Baggage
Space
22.6
Cu.
Ft. 0.678
Cu. M.
(3)
Baggage
Door Width
17"
43.2 cm
(4)
Baggage
Door
Height
20.5"
52.1
cm
(5)
Hat Rack
Capacity
10
Ibs.
4.5
kg
C.
Landing
Gear:
(1) Type
Tricycle,
Retractable
(2)0peration
Electrical
(3)
Wheel
Track
9’
2" 279.4
cm
(4)
Wheel
Base
6’7
9/16"
202.08
cm
(5)
Tire Size-Nose
(6-Ply
Rating)
5.00x5
(6)
Tire
Size--Main
(6-Ply
Rating)
6.00x6
(7)
Tire Pressure--Nose
49
Ibs/sq.
in.
(8)
Tire Pressure--Main
42
Ibs/sq.
in.
6-00-02
AIRCRAFT
DIMENSIONS
DIEIIENSIONS:
A.
Wing Span
36’1"
10.998
meters
B.
Fuselage
Length
26’9"
8.153 meters
C.
Tail
Height.
8’4"
2.54
meters
D.
Stabilizer
Span
11’9"
3.581
meters
AREAS:
A.
Wing
174.786
so.
ft.
16.24
so.
meters
B.
Ailerons
11.4
so.
ft. 1.06
so.
meters
C.
Flaps
17.9sq.ft.
1.66
so.
meters
D.
Vertical Fin
7.8
so.
ft.
0.73
so.
meters
E.
Rudder
6.25
so.
ft.
0.52
so.
meters
F.
Horizontal
Stabili;er
21.42
so.
ft.
1.90
so.
meters
G. Elevators
13.0sq.ft.
1.21
so.
meters
6-00-02
4-99
OLDWILLWAYNE