Mooney Aircraft MARK 21 Manuel utilisateur
MARK
21
MODEL
M
20
C
OPERATE THIS AIRCRAFT
ONLY
-
after reading
owners manual
@
with owners manual on board
@
after you are fully qualified
&
understand all of
the aircraft operating characteristics& limitations
OWNERS
MANUAL
DATA
INCLUDED
MOONEY
AIRCRAFT. /NC.
NOTE:
Information in the
1965
MARK
21
owner's manual
also applies
to
the
1962
through
1964
models with the
ex-
1852, 1940
thru
2207, 2209
thru
2255, 2257
thru
2296
2208,2256,2297
thru
2622
ment
to
the
1965
MARK
21
owrrers
manual
PAR"1" DESCRIPTION AND OPERATION
OF COMPONENTS
FUEL
SYSTEM
(Reference page 3)
The fuel tank capacity of the 1962 and 1963Mark 21 is 24
gallons per wing tank or 48 gallons total fuel. The '62 and
'63 models do not have a pull ring to drain the fuel selector
sump from the cabin. In these models the selector sump is
drained from outside using the sameprocedure recommended
for draining the wing tanks. 1962 and 1963 models have a
gascolator in the nose wheel well which can be inspected and
drained from outside the aircraft.
LANDING
GEAR:
(Reference page 6)
The thumb operated safety latch for the landing gear retrac-
tion lever has not been factory installed on serial numbers
1852, 1940 through 2050.
POSITWE CONTROL SYSTEM: (Reference page 8)
The Positive Control section does not apply to 1962, 1963
or 1964 models unless retrofit installation of the PC system
has been made.
TRIM SYSTEM: (Referencepage 9)
The friction adjsstment for the trim control wheel does not
apply to 1962 models.
FLAPS: (Referencepage 9)
The 1962 and I965 model fiaps are retracted by pulling the
release knob adjacent to the flap handle.
VACUUM
SYSTEM: (Reference page 10)
1962,
'63
and '64 models do not have a vacuum operated
cabin entry seep. These models have a manually operated
step retraction system activated
by
a hand crank on the left
side panel near the pilot's knee. Turning the crank clockwise
raises the step; counter clockw
is,
lowers the step.
The vacuum regulator will maintain vacuum between
3.5
and
5.0
inches of mercury on 1962, 1963 and 1964 models. The
vacuum warning lights for these airplanes are
see
accord-
ingly.
HEATING
AND VENTILATION SYSTEMS: (Reference pages 10
and 11)
1962 models do not have rear heat outlets. There
Ls
no left
side air scoop on 1962, 1963 or 1964 production aircraft.
Serial numbers 1852 and 1940 through 2693 do not have a
firewall-mounted radio cooling grill.
PART
II
FLIGHT
PROCEDURES
WEIGHT AND BALANCE: (Reference page 14)
1962 models are not equipped with the utility shelf aft of the
main baggage compartment. Therefore, related weight limita-
tion does not apply.
ENTERING THE AIRCRAFT: (Reference page
15)
Drain the fuel selector valve sump from outside the air-
craft on 1962 and 1963 models.
STARTING THE ENGINE: (Reference page
15)
-
--
"Push to Stare" feature was installed on the ignition switch
beginning with 1963 models. On earlier aircraft, turning the
ignition switch to "start" engages the starter and the
"shower of sparks" ignition.
COLD
WEATHER AND MANUALSTARTI* (Referencepage 16
To manually start aircraft with serial numbers 1852 and 1940
through 2342 use
the
following procedures:
(1)
Turn off the "starter disconnect switch" located on the
upper center section of the firewall under the instrument
panel. The switch disconnects the starter so that only
the starter vibrator operates when the magneto switch is
turned to the start position.
(2)
As the engine is "propped", hold the magneto switch in
the "start" position. This operates the starter vibrator
and furnishes retarded spark to the engine.
(3) When the engine starts, release the switch to the "both"
position and place the starter disconnect switch in the
"on" position.
Aircraft serial numbers from 2343 may be manually started
as described on page
16.
PART
ill
SERVICE
AND
MAINTENANCE
VACUUM
STEP: (Reference page 27)
The maintenance check of the step retraction does not apply
to 1962, 1963 or 1964 models.
REQUIRED DATA
:
(Reference page
28)
The F.A .A. approved flight manual is part
of
the requird
data for 1962 and 1963 models. Placards in the aircraft and
data in the owner's manual supercede the flight manual data
for later models.
PART
IV
PERFORMANCE
DATA
(Reference pages 29-37)
Perforrnance data shown applies to all 1962, '63, '64 and '65
models except for endurance and range on '62 and '63 planes
which carry
48
gallons of fuel. Following are
the
'62-'63 cruise
and range tables:
CRUISE
AND
RANGE DATA
AWRGGE
CROSS
WEIGHT
-
2200
POUNDS
BEST
POWER
MIXTURE
-
48
GALLONS USABLE FUEL
ALTITUDE
5000'
K3&
AETIPUDE
10,000'
MSL
I
I
I
I
I
I
J
(1)
TRUE AIR SPEED
?
3
PERCENT
(2)
MAXIMUM
RANGE
EACH
100
LB.CHANGE IN AIRPLANE WEIGHT
#ILL
REDUCE OR iNCREASE
TAS
BY
1.2
MPH
PART
V
OPERATION
LlMlTATlONS
The information in
PART
V
of this manual does not apply
to
1962
and
1963
models but does apply to
1964
aircraft. Refer to the
airplane flight manual and instrument markings for
1962
and
1963
airplanes.
OPERATE
THIS
AIRCRAFT
ONLY
-
@
after
reading
owners
manual
@
with
owners
manual
on
board
@
after
you
are
fully
qualified
81
understand
all
of
the
aircraft
operating
characteristics&
limitations
MARK
2
OWNERS
MANUAL
Thank you for choosing a hlooney
The wisdom of
your
selection of
a
Mooney Mark
21
will
be
proved many times as your hours in this exceptional
airplane increase.
It
takes a
long
time
and a lot
of
flying to appreciate
all of the mauy outstanding features built into the
Mark
21.
This
owners manual
will
help you know
your
airplane
better and will make your experience with the Mark
21
more enjoyable.
Welcome
to
the rapidly growing family of blooney own-
ers.
M001VE
B8
AIRCRAFI,
INC.
LOUIS
SCHREINER
FIELD
.
XERRVILLE.
TEXAS
1965
MARK
21
PART
I
DESCRlPTlON
AND
OPERATBa
OF
COMPONENTS
Page
Genera
I
Propeller
Engine
Engine ignition
Fuel System
E
lectrical System
Airframe
Landing Gear
Flight Controls
Mooney Positive Control System
Trim System
Flaps
Vacuum System
Brakes
Heating and Ventilation Systems
Pictures
Ce manuel convient aux modèles suivants
4
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