Mooney M20K - Page 291

MOONEY
AIRCRAFT
CORPORATION
M20K
SERVICE
AND
MAINTENANCE
MANUAL
CRITICAL
ALTITUIIE
VARIATICM
WlfH
AMBIENT
TEMPERATURE
41
t~P/
a
a
a
a
4)
a
3)
a,
a
MT
DECBES
C
1.Aircraft
in
climb
configuration
96
KIAS,
2600
RPM
(+0/-50)
Record
below:
Pressure
Altitude,
OAT,
and
Fuel Flow
when MAP
decreases
below
38"
Hg.
at
full
throttle.
.Enter
point
on
chart
at
Pressure
Altitude
and
OAT. If
point
is
within
the
depicted
altitude
band,
critical
altitude
is
within
tolerance.
If
outside
the
altitude
band,
the
engine
will have
to
be
retrimmed.
CRITICAL
ALTITUDE
REPORT
FLT
1
FLT
2
FLT 3
FLT
4
FLT 5
Altitude
(Feet)
Air
Temp
(C)
Flow
(GPH)
Date
Aircraft
Serial
Number
Aircraft
Registration
Number
CRITICAL
ALTITUDE
CHART
CTSIO-360-SB
ENGINE)
FIGURE
71
4D
71-00-50
15
OLDWILLWAYNE