Mooney M20M - Page 31

MOONEY
AIRCRAFT CORPORATION M20M
SERVICE
AND MAINTENANCE MANUAL
6-00-00
DIMENSIONS
AND AREAS
6-00-01
AIRCRAFT SPECIFICATIONS
ENGINE
STANDARD
METRIC/OPT/MISC.
Engine
Manufacturer
TEXTRON-Lycoming
Engine
Model
TIO-540-AF1A
or
-AF1B
No.
Cylinders
6
Rated
Horsepower
270
HP
RPM.
2575
Min. Fuel Octane
100
or
100
LL.
Fuel
Capacity
Total
95
U.S.
Gal. 359.6
Liters
Useable
89
U.S.
Gal.
336.9
Liters
Refer to
TCDS
for
engine
configuration
Oil
Specification
MIL-L-22851
Oil
Grade-Above
300
F(-l
C)Ambient
air
SL SAE
40
or
15W-50
Below
300
F(-l"
C)Ambient
air
SL SAE
30
or
20W-30
Oil
Capacity
10
qts.
9.5
Liters
Minimum
for
Flight
Oil’Lev~l
6
qts.
5.7
Liters
*X
Break in oil
for
Lycoming
turbocharged
engines
is
required
to
be
ashless
dispersant
oil
per
Lycoming
SI
1014(M (or
current
revision) corresponding
to
MIL-L-22851
or
SAE J1899.
Max
Operational
Induction
Air
Temperature
2800
F
1380
C.
Max
Continous
Operation
TIT
17500
F
Normal
Operating
TIT
1300
17500
F
Oil
Pressure
Idle,
Minimum-
25
PSI
Normal
Operation
55-95
PSI
Max.
Allowable
(cold
oil)
115
PSI
Oil
Temperature
Max. Allowable
1180_
C
2440
F
Recommended
Takeoff-Min
100U.F
380
C
Recommended
Flight Operation
iCrui’se)
38-1180.C
100
2440
F
Cylinder
Head
Temperature
(CHT)
Max.
Allowable.
5000
F
2600
C
Recommended Cruise
250
to
5Q00
F.
121
to
2600
C
Turbocharger
Turbocharger
Mfg.
Airesearch
Type
Exhaust
Driven
Turbocharger
Model
TA0413
PROPELLER
PropellerMfg.
McCauley
Type
Constant
Speed
Model
B3D32C41
7/GS2NRD-7
Pitch
Angle
30
in.
LOW
15.1
DEG
(-e/-)0.2
DEG.
HIGH
43
DEG
(+/-)0.5
DEG.
Diameter
75.0
Inches.
190.5
cm
Governor
McCauley
4-99
6-00-00
OLDWILLWAYNE