Mooney Executiv 21 Bedienungsanleitung
MODEL
M20F
OWNERS
MANUAL
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
MOONEY
AlRCRAF7:
lNC.
YEAR
P
1967
OWNERS
MANUAL
MODEL
SERIAL
NUMBERS
M20F 660003
&
660004
670001
TWRU
670539
Issued
September
1966
Revised
March
1967
aboard your new Executive
21.
Enjoy the greater utility
of the long, rooiny cabin. The far-ranging fuel capacity
of the Executive
21
now makes possible one-stop trans-
continental flights.
The same high perforinance and low operating cost which
make its sister ships, the Mark
21
and Super
21,
the
world's leading sellers
in
the retractable-geared class,
arebred into the Executive
21.
Read this manual carefully, it is prepared to help you en-
joy fully the remarkable perfor~nanceand econorn)r charac-
teristics the Executive
2
1
is prepared to deliver.
MBONEY
AIRCRAFT,
INC.
XERRVIL 1
E
TEXAS
This manual contains Federal AviationAgency- DelegarionOption
Authority approved li~nitarionsand
nus st
be carried in the
Execu-
tive
21
at all times.
EXECUTIVE
21
OWNER'S
MANUAL
TABLEOFCONTENTS
PART
I
DESCRIPTION AND OPERATION
OF
COMPONENTS
Page
General
Propeller
Engine
Power Boost
Engine Ignition
Fuel System
Electrical System
Airframe
Landing
Gear
Flight Controls
Moaney Positive Control Systen.
Trim System
Flaps
Vacuum System
Brakes
Heating and Ventilation Systems
PART
II
FLIGHT
PROCEDURES
General
Weight and Balance
Pre-Flight Inspection
Entering the Airplane
Starting the Engine
Cold Weather ond Manual Starting
Taxiing and Ground Operation
Pre Take-Off Check
Take-Off and Climb
Power Changes
Cruise Procedures
Indicated Airspeed
Fuel Management
Let-Down Procedures
Land
ing Procedures
Normal Landing
Stopping the Engine
PART I!! SERVICE AND MAINTENANCE
Page
General
Ground Handling
Propeller
Engine
Battery
Care
of
Interior
Care of Exterior
Windows
Landing Gear
Vacuum Operated Step
Required Data
Service Bulletins and Instructions
PART IV PERFORMANCE
DATA
Take-Off and Climb Data
Climb Performance
Cruise and Range (2500')
(5000')
(7500')
(1
0,000')
(15,000')
Stall Speed
vs.
Sank Angle
Maximum Range
&
Glide Range
Landing Data
(Fig.
1)
(Fig.
2)
(Fig. 3)
(Fig. 3A)
(Fig. 38)
(Fig. 3C)
(Fig. 3D)
(Fig.
4)
(Fig. 5)
(Fig. 6)
Page
PART
V
OPERATING
LIMITAT
IONS
FAA/BOAAPPROVED MOONEY
M20F
Page
Power Plant Instruments
Airspeed Limitations
Flight Load Factors
Maximum Weight
&
CG Range
Aircraft Instrumentation Markings and
their Significance
Types of Operation
Power Boost
Placards
Instrument Marking (Except Power Plant)
Maximum Altitude Loss in Stalls at Gross Weight
Revised
March
1967
PART
I
DESCRIPTION AND OPERATION OF COMPONENTS
GENERAL
The Executive 21 is a single engine four-place low wing, re-
tractable tricycle landing gear airplane. The design and opera-
tion of this aircraft are conventional with few exceptions. This
section will describe some of the components of the aircraft
and operating details.
PROPELLER
The Executive 21 uses an alunlinu~nalloy constant speed pro-
peller of
74
inch diameter. The pitch of the blades is controlled
by engine oil pressure which acts to increase blade angle of
attack and thereby control engine speed. The propeller control
in the cabin operates the propeller governor which controls the
oil pressure provided to the propeller hub. The governor
ser-
ting functions to maintain the engine at a constant speed by
actuating blade angle of attack. In essence then, the function
of the propeller control in the cabin is to regulate and maintain
the rotational speed of the engine at a desired setting.
ENGINE
The Executive 21 is powered by the Lyconling
200
hp
10-360-A
1A
four cylinder engine. This engine uses 100/130 octane fuel.
Four rubber bushings on the aft side of the engine provide
mounting and vibration isolation. Engine ~iianifoldpressure
is
regulated by the push-pull throttle control on the panel.
POWER
BOOST
A
unique Power Boost feature of the Executive 21 provides in-
creased manifold
p
re
ss
u re when operating at full throttle.
This is
a
c co
111
p
1
is
h ed by pulling the Power Roost control
out, which causes induction air to by-pass the engine air filter
to perinit the engine to operate
on
direct ram air. Because
the engine will be operating on unfiltered air when the Power
Boost is used, it should be operated only in clean, dust free
Revised
March
1967
air at altitude, and turned off for take-off and landing. Because
the Power Boost is effective only when the throttle is in the
fully opened position, its advantages generally will be realized
at altitudes above
5,000
feet where flight is often with full throt-
tle.
A
light is provided on the panel by the Power Boost control
to remind the pilot to push the control in (to filtered air) before
landing. This light will come on when the gear
is
lowered
while Power Boost is on.
I
WARNING
Do not
fly
this aircraft in icing conditions.
Turn Power Boost off when icing conditions are
inadvertently encountered. Icing conditions prevail
any time the temperature and inoisture conditions
coixbine to produce the possibility of impact ice.
Using unfiltered induction air when flying in snow
or other
IFR
conditions can be hazardous. Snow
can accumulate in the fuel injector impact tubes or
inoisture can freeze in the passages under icing
conditions and cause loss of power. Therefore it
is imperative that the Power Boost not be used when
flying in sleet, snow, rain, or i~~oisture-ladenair
near freezing teii~peratures. Under these condi-
tions ice can for~liin the inlet duct or fuel injector
unit even though no visible moisture
is
apparent on
the airframe.
POWER
BOOST
ON
FUEL-AIR
MIXTURE
The fuel injector unit of the
10-360
engine has provisions for
adjusting the fuel-to-air ratio as required at,different altitudes.
The fuel-to-air ratio (mixture) is regulated by the hexagon
shaped push-pull control located between the throttle and pro-
peller controls in the cabin. This control has a vernier adjust-
nlent feature for obtaining precise mixture settings. An exhaust
gas temperature gage is provided to indicate the optiinurn mix-
ture setting.
ENGINE
COOLING
The engine baffling directs air flow over the cylinders for cool-
ing in flight. Cowl flaps are provided on the lower cowling to
allow more free air flow on the ground and during low speed,
high power conditions (i.e., climb conditions). Cowl flaps
should always be open on the ground, and prolonged engine
operation on the ground should be avoided to prevent engine
overheating.
A
push-pull cofitro'i is provided below the in-
strument panel and to the right of the pilot for operation of th'e
cowl flaps.
Dieses Handbuch passt für folgende Modelle
1
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