MOONEY
MODEL
M20J
SECTION
IV
NORMAL PROCEDURES
CLIMB
(BEST
ANGLE)
Power
....
FULL THROTTLE and
2700
RPM
Mixture
......
FULL RICH (Lean at higher
....
.altitude for smooth operation)
.............
Cowl Flap FULLOPEN
Airspeed
.
,
.
,
.
,
. .
69
KlAS at sea level increasing
........
approxiinately
1.0
KlAS for each
...........
5000
feet altitude
Ram Air
.....
.ON
after entering clear air
=-----"-
I
MOTE
/
------me
$0
Increase
performance
at
fu61
throttle
pkrll
the
Ram
Air
control
aft
(Ram
Air
QN
position)
allowing
induceion
air
to
bypass
air
s'i!%er
and
irlcrease
manifsid
pressure.
Manifold pressure will drop with increasing altitude at any throttle set-
ring.Power can be restored by gradually opening the throttle.
lllllllllllllllllll
IIIWARNINGIII
ll//llllll/l/ll/ll//
-DO
MOT
FLY
AIRCRAFT
INTO
KNOWN
lCsNG CQNB1TIONS-
CRUISE
Upon reaching cruise altitude, accelerate to cruise airspeed; relrirn aircraft as
necessary for level flight. Set
rnariifold pressure and
RPM
for desired power
setting per Cruise Power
Chart
in
Section
V.
Position cowl flaps as required
to
maintain the oil and cylinder head temperature within their normal operat-
ing ranges.
-----"-.,
I
NDTE
I
--""---"
When
cruising
in
conditions
where
%he
OAT
is
well
above
starsdard,
it
may
be
necessary
to
OPEN
cowl
l!aps
sllghtiy
in
order
to
keep
engine
temperatures in
the
green
arc.
When
cowl
fBape
are
OPEN
during
crteiae,
tho
following
effects
on
cruise
speed
%strill
resuit:
Cowf
Flaps
114
open
(1st
index)
Approximate
loss
in
TAS
..
2
KTAS
Cowl
FIaps
112
open
(2nd
Index)
Approximate
lass
in
$AS
.
4
KTAS
WE!'.
B
6-12-87
ISSUED
6-2-06
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