Mooney M20R - Ovation Technical specifications

MOONEY
PILOT'S OPERATING HANDBOOK
AND
FAA APPROVED
AIRPLANE FLIGHT MANUAL
M20R -OVATION
ORIGINAL ISSUE- 06-1994
REVISION G - 03-2000
Copyright 2013- All Rights Reserved
PIN: POH-003600
MOONEY AVIATION COMPANY, INC. Louis Schreiner Field, Kerrville, Texas 78028 tel: [phone]
www.mooney.com

29-0045
OE-KGG
Section VI, page 6-5 Revised Weight and Balance sheet dated 10/4/12 inserted
by Erik Rosdol on 15-Nov-2014

INTRODUCTION
CONGRATULATIONS
MOONEY
M20R
'JI.ELCOME TO MOONEY'S NBI\ESTDI MENSION IN SPEED, QUALI1Y AND ECONOMY.
YOUR DECISION TO SELECT A MOONEY AIRCRAFT HAS PLACED YOU IN AN EliTE
AND DISTINCTIVE CLASS OF AIRCRAFT O'MIIERS. 11\.E HOPE YOU FIND YOUR
MOONEY A UNIQUE FLYING EXPERIENCE. IM-IETHER FOR BUSINESS OR PLEASURE ,
THE MOST PROFITABLE EVER
-NOTICE -
This manual is provided as an operating guide for the Mooney Model M20R. It is important
that you --4"egardless ofyour previous experience -carefully
read the handbook from
coverto cover
and review it frequently .
All infonnation and illustrations in the manual are based on the latest product infonnation
available at the time of publicalion approval
and all sections including attac hed supple-
ments are mandatory for proper operation of the aircraft. The right is reserved to make
changes
at any time without notice. Every effort has been made to present the material in
a clear and convenient manner to enable you to use the manual as a reference . Your
cooperation
In reporting presentation and content recommendations is solicited.
REVISING THE MANUAL
The "i" pages of this manual contain a "list of Effective Pages " containing a complete
current listing of all pages i.e ., Original or Revised . Also, in the lower right comer of the
outl
ined portion, is a box which denotes the manual number and issue or revision of the
manual. It will be
advanced one letter, alphabetically, per revision . IMth each revision to
the manual a new Ust of Effective Pages showing all applicapable revisions with dates of
approval and a " Log of Revisions" page(s) ,with only the latest Revision shown, will be
provided to replace the
previous ones . It is the operators responslblilty to ensure that this
manual
is current through the latest published revision .
This harodbook will be kept current by Mooney Aircraft Corporation when the yellow
infonnation card
in front of this handbook has been completed and mailed to :
Mooney Aircraft Corporation
Service Parts Department
Louis Schreiner Field,
Kerrville,
TX., 78028.
ISSUED 6-94

INTRODUCTION
ORIGINAL .
Revision A.
Revision B.
Revision C
Revision D.
Revision E.
Revision F.
Revision G
ILIST OF EFFECTIVE PAGES I
MOONEY
M20R
6-94
7-94
8-94
9-94
1-95
9-95
9-96
3-00
Always destroy suuperseded pages when inserting revised pages.
TITLE PAGE . . . . . . . . . . . . . . . .
CONGRATULATIONS .
i thru iv
v, vi
1-1,
1-2.
1-3
1-4
1-5 . .
1-6 thru 1-8
1-9, 1-10
2-1
2-2 .
2-3, 2-4
2-5 .
2-6,2-7
2-8 . .
2-9, 2-10 .
2-11,2-12
2-13 .
2-14, 2-15
2-16,2-17 .
2-18
3-1 thru 3-4
3-5 . .
3-6 thru 3-7
3-8 .
3-9, 3-10
3-11
3-12
3-13 . .
3-14,3-15.
3-16
4-1 . .
·4-2 th ru 4-4
4-5
4-6 .
4-7, 4-8
ISS USED 6-94
G
ORIGINAL
.. G
ORIGINAL
ORIGINAL
F
.. c
ORIGINAL
.. G
ORIGINAL
G
B
G
. . F
ORIG INAL
G
E
G
D
G
.. A
OR IGINAL
ORIGINAL
G
. E
. A
. . E
ORIGINAL
E
F
.. E
ORIGINAL
. . F
ORIGINAL
F
c
E
POH(AFM NUMBER 3600 (G)
This POH(AFM effective beginning with M20R S/N 29-0001

MOONEY
M20R
4-9 thru 4-12
4-13, 4-14
4-5, 4-16 .
5-1
5-2
5-3 . . .
5-4 thru 5-12 .
5-13 . .
5-14 thru 5-18
5-19 . . .
5-20 thru 5-30
6-1 thru 6-6 .
6-7, 6-8
6-9
6-10 .
6-11
6-12 . .
6-13, 6-14.
6-15 .
6-16 . .
6-17 .
6-18, 6-19. .
6-20 thru 6-22
6-23 . .
6-24 . . .
6-25 thru 6-29
6-30 . .
7-1,7-2 . .
7-3 thru 7-4 .
7-5 thru 7-30
8-1
8-2 . .
8-3 thru 8-6 .
8-7 .
8-8 thru 8-10 .
I LIST OF EFFECTIVE PAGES (con't.}l
INTRODUCTION
. .. F
. E
ORIGINAL
. .. c
ORIGINAL
. .. A
ORIGINAL
G
. c
. E
. c
ORIGINAL
. F
ORIGINAL
... E
ORIGINAL
F
ORIGINAL
. .. G
ORIGINAL
. . G
ORIGINAL
.. G
... F
ORIGINAL
... G
ORIGINAL
. G
ORIGINAL
. G
ORIGINAL
. G
ORIGINAL
. A
ORIGINAL
9-1 through 9-4 . . . . . . .
(plus Applicable Supplements inserted) ORIGINAL
ii
10-1 . . .
10-2 thru 10-10 .
10-11
10-12 .
D
ORIGINAL
D
ORIGINAL
POH/AFM NUMBER- 3600
(G)
This POH/AFM effective beginning with M20R S/N 29-0001
ISSUED 6-94

INTRODUCTION
~FVISION
REVISED
UMBER PAGES
G
Title
Page,
LOEP, Log of
Revisions, 1-6,
1-7, 1-8,2-1,
2-3, 2-8, 3-5,
7-1, 7-2, 7-5
thru 7-3, 8-2
2-4
5-13,
6-15,
6-16,6-17,
6-20, 6-21,
6-22,6-25thru
6-29
2-11thru 2-15
I LOG OF. REVISIONS I
DESCRIPTION FAA
OF REVISIONS APPROVED
I
Revised Data
Added Data
Revised Chart
Added Placard
, 1·1;~
MOONEY
M20R
DATE
¥~1P
..
The reVJsed portions of affected pages are and1 .cated by vert1cal black lines 10 the margm.
POH/AFM NUMBER- 3600
(G)
ISSUED 6-94 iii

MOONEY
M20R
REVISION
NUMBER
INTRODUCTION
I LOG OF REVISIONS (con'tll
REVISE[ DESCRIPTION FAA DATE
PAGES OF REVISIONS I APPROVED
The revised portions
of affected pages are indicted by vertical black lines in :he margin.
iv
POH/AFM NUMBER 3600 (G)
ISSUED6-94

MOONEY
M20R
I TABLE OF CONTENTS I
TITLE ....... .. . . .•.•
GENERAL
LIMITATIONS
EMERGENCY PROCEDURES
NORMAL PROCEDURES.
PERFORMANCE
WEIGHT & BALANCE. ·
AIRPLANE &SYSTEM DESCRIPTIONS
HANDLING, SERVICE & MAINTENANCE.
SUPPLEMENTAL DATA .
SAFETY & OPERATIONAL TIPS.
ISSUED 6-94
INTRODUCTION
. . . SECTION
II
Ill
IV
v
VI
VII
VIII
IX
X
v

INTRODUCTION
BLANK
vi
MOONEY
M20R
ISSUED 6-94

MOONEY
M20R
ITABLE OF CONTENTS I
SECTION I
GENERAL
TITLE • •••••• • • •• ••• • • • • •• PAGE
THREE VIEW . . . . . . . . • • . . . . . . • • . 1-2
INTRODUCTION . . . . • • . . . . . . . . . . . . 1-3
DESCRIPTIVE DATA
ENGINE
PROPELLER
FUEL
OIL
LANDING GEAR
MAXIMUM CERTIFICATED WEIGHTS
STANDARD AIRPLANE WEIGHTS
CABIN & ENTRY DIMENSIONS
BAGGAGE SPACE AND ENTRY DIMENSIONS
SPECIFIC LOADINGS
IDENTIFICATION PLATE
SYMBOLS, ABBREVIATIONS &TERMINOLOGY
GENERAL AIRSPEED TERMINOLOGY & SYMBOLS
ENGINE POWER TERMINOLOGY
1-3
1-3
1-3
1-4
1-4
1-4
1-4
1-4
1·5
• . 1-5
1-5
1-5
1-5
1-5
Hi
AIRPLANE PERFORMANCE & FLIGHT PLANNING TERMINOLOGY 1-6
ENGINE CONTROLS &INSTRUMENTS TERMINOLOGY 1-7
METEOROLOGICALTERMINOLOGY 1-7
WEIGHT & BALANCE TERMINOLOGY 1-8
MEASUREMENT CONVERSION TABLES . . . . . . . . . . . 1-8
ISSUED 6 - 94 1 - 1

SECTION I
GENERAL MOONEY
M20R
(1099,8 ,Cl'l)
I
.
-36'-1 ·~ · 1
FIGURE 1 - 1 THREE VIEW -M20R
1 -2 ISSU:OD 6-94

SECTION I
GENERAL
FUEL
Minimum Fuel Grade (Color)
Total capacity . . . .
Usable
MOONEY
M20R
100 LL (Blue) or 100 Octane (Green~
. . . 9S U.S. Gal .. (359 .6 Liters
. . .
89.0 U.S . Gal . (336 .9 Liters
Oil Spec ification . . . . • . . . . . . . . . . . MH5-24()
an d as Approved by TCM . (Reference Engine Maintenance & Operators ManuaO
All Tem peratures 0 • • • • • . • . • • • • • • . • 1511\50 or 20111.60
Above 30:F (- 1
0
C) Amb i ent Air (S . L) . . . . . . • . . . . SAE 50
Be l ow 50 F (1 0 C) Ambient Air (S L ) . . . . . . • . . SAE 30, 1 0\1\GO
I Total 01 Capacity . • • . . . . . . . . . . . 8 Qts. (T.57 liters)
Oil Filter . . . . . . . . . . . . . . . . . . . Full Row
Oil grades, specifications and changing recommendations are contained in ·SEcllON VIII.
LANDING GEAR
TYPE: Bectrically operated, fully retractable tricycle gear with rubber shock discs. The
main wheels have hydraulically operated disc brakes. The nose wheel is fully steerable 11°
left to 13° right of center.
Wleel Base
Wleel Track
lire Size:
Nose .
Main . .
Trre Pressure
Nose .
Main .
Minimum Turning Radius (No brakes applied)
Right . . . . . . . . • . •
Left . . . . . . . . • . .
MAXIMUM CERTIACATED WEIGHTS
Gross IM!ight . . . . . .
Maxim~ landing Weight . .
Baggage
Area • • . • • .
Rear st orage Area . . . . .
Cargo (Rear Seats Folded Down)
STANDARD AIRPLANE WEIGHTS
79 9116 in .. (198.91 em)
. 110 in. (279.4 em)
5.00 X 5 (6 ply)
6.00 X 6 (6 ply)
49PSI
42PSI
40ft. (12.0 m)
48ft. (14.4 m)
3368 Lbs. (1528 Kg!
3200 Lbs . (1452 Kg
120 Lbs . (54.4 Kg
. 10 Lbs . (4.5 Kg
340 Lbs . (154 .2 Kg
Basic Bnpty Weight
Useful Load . . . . . . . . . . . . . . . .
See Page 1-8
. . . . . . . . . Varies with installed equipment.
See SECTION VI for specific airplane weight (pg. 6-5).
1-4
REV.C 9-94
ISSUED 6-94

MUUNt:Y
M20R
.:;J~VIIVI' I
GENERAL
IINTRODUCTION I
This OperatoJS Manual confonnsto GAMA Specification No. 1 and includes both Manufac-
tureJS material and FAA APPROVED material required to be furnished to the Pilot by the
appficable
Federal Aviation Regu l ations . section IX contains supplemental data supplied
by MooneyAircraft Corporation.
section Icontains information of general interest to the pilot. It also contains definitions of
thetenninology used in this Operators Manual.
This Pilot's Operating Handbook is not designed as asubstitute for adequate and compe-
tent flight instruction, knowledge of current airworthiness di rectives , applicable federal air
regulations oradvisory circulars. It
is not Intended to be aguide for bas ic flight instruction
oratraining manual
and should not be used for operaUonal purposes unless kept in an up
to date status. · ·
All limitations, procedures, safety practices, servicing and maintenance requirements pub-
lished in this POHIAFM are considered mandatory for the Continued Airworthiness ofthis
airplane
in acondition equal to that of its original manufacture.
IDESCRIPTIVE DATA I
ENGINE
Number of engines
Engine Manufacturer
Molle! ....
Recommended lBO
Type . • . .
Number
of cylinders
Displacement . .
Bore . . . .
stroke. . . .
Compression ratio
Fuel System
~fk~ ....
Fuel-Aviation Gasoline
Accessories
Magnetos . .
!9nition Harness
~ark Plugs .
OIICooler . .
Alternator .
starter .
Ratings:
Maximum Takeoff
Sea Level BHPIRPM
PROPELLER
Number .
Manufacturer .
Model Number .
Number
of Blades . . . .
Diameter
(112 in. cutoffallowed)
Type . . . . . . .
Governor (McCauley) . . .
Blade Angles @ 30.0 in. sta.:
Low .... . . .
High .
. . . . . . . . . 1
Teledyne Continental Motors (TC~ I
. -. . • . . 10-550-G(S)
. . . • • . . 2000 Hours
Reciprocating, air cooled,
fuel injected
. . . . 6, Horizontally opposed
. . . . 550 Cu. ln . ~9014 cc~
. . . . . 5.25 ln. 13.3 em
: : : : . . 4~5 ~n . ~ o:
5
c~ I
. Fuellnjection
.... TCM
100 octane -1 OOLL
Bendix - S6RN - 25
. . . . Shielded/Braided
AC 273 (orequivalent) ( 18 m/m)
• . . . . TCM Full Row
28 Volt DC, 100 AMPS
24vottDC
. 280/2500
. . . . . . . 1
. . . . . McCauterl
3A32C418/(G)-82NRC-9
. . . . . . . . . . 3
. . . . . . 73 in . (185 .4 em)
. . . . . . Constant Speed
Hydraulically controlled by engine oil
16.1 degrees+ 1-0.2 degrees
40 degrees + 1- 0.5 degrees
• Refer to TCOS for engine/propeller configuration required .
ISSUED 6-94
REVF 9-96
1-3

MOONEY
M20R
CABIN AND ENTRY DIMENSIONS
Cabin Width (Maximum)
Cabin length (Maximum)
Cabin Helght (Maximum)
Entry Widlh (Minimum)
Entry Height (Minimum)
BAGGAGE SPACE AND ENTRY DIMENSIONS
Compartment Width
Compartrr.ent Length
Compartment Height
Compartment Volume
Cargo Area (with rear seat folded down)
Entry Height (Minimum)
Entry
Wldlh . .
Ground to Bottom of
SUI
SPECIFIC LOADINGS
Wing Loading -@ Maximum Gross Weight
Power Loading -@ Maximum Gross Weight
IDENTIFICATION PLATE
SECTION I
GENERAL
. 43 .51n. (110.5 em
126 ln. (315 em
44.51n. (113 em
29.0 ln. (73.4 em
35.0 ln. (88.9 em
24 ln. (60.9 em~
43ln. (109.2 em
35 ln. (88.9 em
20.9 cu . ft.
(.592 cu. m)
. . 38 .6 cu. ft.
(1 . 09 cu. m)
• 20.5 ln. (52.1 em~
. 17.0 ln. (43.2 em
. 46.0 ln. (116.8 em
19.26lbs./sq . ft .
(94 kg/sq. m)
. 12.02 lbs./HP
(5.46 kg/HP)
All correspondence r*rding your airplane should Include the Serial Number as depicted
on the Identification plate. The identification plate Is located on the left hand side, aft end of
the tall
cone, below the horizontal stabilizer leading edge. The aircraft Serial Number and
type certif.cate are shown.
ISYMBOLS, ABBREVIATIONS & TERMINOLOGY I
GENERAL AIRSPEED TERMINOLOGY & SYMBOLS
GS GROUND SPEED - Speed of an airplane relative to the
ground.
KCAS
KIAS
KNOTS CAUBRATED AIRSPEED -The indicated speed of
an alrcraft,corrected for position and instrument error.
Calibrated airspeed is equal to true airspeed in standard
atmosphere at sea level.
KNOTS INDICATED AIRSPEED - The sp eed of an aircraft
as shown on its airspeed Indicator. lAS values published
in this handbook assume zero instrument error.
KTAS KNOTS TRUE AIRSPEED - The airspeed of an airplane relative to
undisturbed air which
Is the KCAS corrected for altitude and
"temperature.
Va
Vte
ISSUED 6-94
MANEUVERING SPEED -The maximum speed at which
application of
full available aerodynamic control will not
overstress
the airplane.
MAXIMUM FLAP EXTENDED SPEED - The highest speed
permissible with wing flaps in a prescribed extended position.
MAXIMUM LANDING GEAR EXTENDED SPEED -The
maximum speed at which an aircraft can be safely flown
with the landing gear extended.
1 -5

SECTION I
GENERAL MOONEY
M20R
GENERAL AIRSPEED TERMINOLOGY & SYMBOLS (con't.)
Vio
Vne
Vno
Vs
Vso
Vx
Vy
MAXIMUM LANDING GEAR OPERATING SPEED- The
maximum speed at which the landing gear can be safely
extended
or retracted.
NEVER EXCEED SPEED -The speed limit that may not be
exceeded at any time.
MAXIMUM STRUCTURAL CRUISING SPEED -The speed
that should not
be exceeded except in smooth air and then
only with caution.
STALLING SPEED -The minimum steadyflight speed at which
the airplane is controllable.
STALLING
SPEED- The minimum steady flight speed at
which the airplane is controllable
in the landing configuration.
BEST ANGLE-OF-CLIMB SPEED -The airspeed which
delivers the greatest gain
of altitude in the shortest possible
horizontal distance.
BEST RATE-OF-CLIMB SPEED- The airspeed which delivers
the greatest gain
in altitude in the shortest possible time with
gear and flaps
up.
ENGINE POWER TERMINOLOGY
BHP
CHT
EGT
MCP
MP
RPM
BRAKE HORSEPOWER -Power developed by the engine.
CYLINDER HEAD TEMPERATURE- Operating temperature of
engine cylinder(s) being monitored by sensor unit. Expressed in°F .
EXHAUST GAS TEMPERATURE- The exhaust gas temperature
measured in the exhaust pipe manifold: Expressed in °F.
MAXIMUM CONTINUOUS POWER -The maximum power
for takeoff, normal, abnonnal
or emergency operations.
MANIFOLD PRESSURE -Pressure measured in the engine's
induction system and expressed
in inches of mercury (Hg).
REVOLUTIONS PER MINUTE -Engine speed.
AIRPLANE PERFORMANCE AND FLIGHT PLANNING TERMINOLOGY
Demon-
strated
Crosswind
Velocity
g
Service
Ceiling
1 -6
The velocity of the crosswind component for which adequate
control
of the airplane during takeoff and landing test was
actually demonstrated during certification. The value shown
is not considered to be limiting.
Acceleration due to gravity.
The maximum altitude at which aircraft at gross weight has the
capability of climbing at the rate of 100 ft/min.
REV.G ISSUED 6-94

MOONEY
M20R SECTION I
GENERAL
ENGINE CONTROLS & INSTRUMENTS TERMINOLOGY
Propeller
Control
Throttle
Control
Mixture
Control
CHTGauge
Tachometer
Propeller
Governor
The control used to select engine speed.
The control used to select engine power by controlling MP.
Provides a mechanical linkage to the fuel injector mixture control
to control the size
of the fuel feed aperture, and therefore the air/fuel
mixture. It is the primary method to shut the engine down.
Cylinder
head temperature indicator used to detennine that engine
operating temperature is within manufacturers specifications.
An instrument that indicates rotational speed
of the engine.
The speed· is shown as propeller revolutions per minute (RPM).
The device that regulates RPM
of the engine/propeller by
increasing or decreasing the propeller pitch, through a pitch
change mechanism in the propeller hub.
METEOROLOGICAL TERMINOLOGY
AGL
Density
Altitude
Indicated
Altitude
ISA
OAT
Pressure
Altitude
Station
Pressure
Above ground level.
Altitude as detennined by pressure altitude and existing ambient
temperature.
In standard atmosphere (ISA) density and pressure
altitude are equal.
For a given pressure altitude, the higher the
the temperature, the higher the density altitude.
The altitude actually
read from an altimeter when, and only when
barometric subscale (Kollsman window) has been set
to
Station Pressure.
INTERNATIONAL STANDARD ATMOSPHERE assumes that
(1) The
air is a dry perfect gas; (2) The temperature at sea level is
15 degrees Celsius (59°F); (3) The pressure at sea level is 29 .92
inches Hg (1013.2 mb); (4) The temperature gradient from sea level
to the altitude at which the temperature is -56.5°C (-69.7°F) is
-0.00198°C (-0.003564°F) per root.
OUTSIDE AIR TEMPERATURE- The free air static temperature,
obtained either from inflight temperature indications
or ground
meteorological sources. It is expressed
in °C.
The indicated altitude when Kollsman window is setto 29.92 ln. Hg.
or 1013.2 MB. In this handbook, altimeter instrument errors are
assumed to
be zero.
Actual atmospheric pressure at field elevation.
WEIGHT AND BALANCE TERMINOLOGY
Ann
Basic
Empty
Weight
Center
of
Gravity
(C.G.)
ISSUED 6-94
The horizontal distance from the reference datum to the center of
gravity (C.G.) of an item.
The actual weight
of the airplane and includes all operating
equipment (including optional equipment) that has a fixed
location and is actually installed
in the aircraft.
It includes the weight of unusable fuel and full oil.
The point at which an airplane would balance if suspended.
Its distance from the reference datum is found by dividing the
total moment by the total weight
of the airplane.
REV . G 1 - 7

SECTION I
GENERAL MOONEY
M20R
WEIGHT AND BALANCE TERMINOLOGY (can't.)
C.G. Arm
e. G. in
%MAC
C.G.
Umits
MAC
Maximum
Weight
Maximum
Landing Weight
Moment
lions
Reference
Datum
Station
Tare
Unusable
Fuel
Usable
Fuel
Useful
Load
The arm obtained by adding the airplane's individual moments
and dividing the sum by the total weight.
Center of Gravity expressed in percent of mean aerodynamic
chord (MAC).
The extreme center of gravity locations within which the airplane
must be operated at a given weight.
Mean Aerodynamic Chord.
The maximum authorized weight of the aircraft and its contents as
listed
in the aircraft specifications.
The maximum authorized weight
of the aircraft and its contents
when a normal landing
is to be made.
The product of the weight of an item multiplied by its arm;
(Moment divided by a constant
is used to simplify balance calcula-
by reducing the number
of digits.)
An imaginary vertical plane from which all horizontal distances are
are measured for balance purposes.
A location along the airplane fuselage usually given in terms
of
distance from the reference datum.
The weight
of chocks, blocks, stands, etc. used when weighing an
airplane, and
is included in the scale readings. Tare is deducted
from the scale reading to obtain the actual (net) airplane weight.
Fuel remaining after a runout test has been completed
in
accordance with governmental regulations.
Fuel available for aircraft engine combustion.
The basic empty weight subtracted from the maximum weight
of
the aircraft. This load consists of the pilot, crew Qf applicable),
useable fuel, passengers, and baggage.
IMEASUREMENT CONVERSION TABLES I
LENGTH
U. S.
Customary Unit
1 inch
Metric Equi•1alents
2.54 centimeters
0.3048 meter
0.9144 meter
1, 609 meters
1, 852 meters
1 foot
1 yard . .
1 mile (statute, land)
1 mile (nautical,
international)
U. S.
Customary Unit
1 square inch
1 square foot
1 square yard
1 -8
AREA
REV.G
Metric Equivalents
6.4516 sq. centimeters
929 sq. centimeters
0.836 sq. meter
ISSUED 6-94

MOONEY
SECTION I
M20R GENERAL
VOLUME OR CAPACITY
U. S. Customary Unit Metric Equivalents
1 cubic Inch 16.39 cubic centimeters
1 cubic foot . 0.028 cubic meter
1 cubic
yard
. 0. 765 cubic meter
U.S. Customary
Liquid Measure Metric Equivalents
1 fluid ounce 29.573 miiiHiters
1 pint 0.4731iter
1 quart 0.946 liter
1 gallon 3.7851iters
U.S. Customary
Dry Measure Metric Equivalents
1 pint 0.
551 liter
1 quart
1.101 liters
British Imperial .u.s.
Metric
Liquid and Dry Measure •Equivalents Equivalents
1 fluid ounce .0.961
u.s. 28.412 milliliters
fluid ounce,
1.734 cubic
Inches
1 pint . 1.032 u.
s. 568.26 miiiUiters
dry pints.
1.201 u.s.
liquid pts.,
34.678 cubic
Inches
1 quart .1.032 u. s.
1.1361iters
dry quarts
1. 201 u.s.
liquid qts.,
69.354 cubic
Inches
1 gallon .1.201 u. s. 4.54611ters
277.420
cubic inches
WEIGHT
U. S. Customary Unit
(Avoirdupois)
Metric Equivalents
1 grain .64.
79891 milligrams
1dram
1.772 grams
1 ounce . 28.350 grams
1 pound 453.6 grams
PRESSURE
U.S. Customary Unit
Metric Equivalents
1
PSIG
6.895 KPA
1 Inch Hg
1 Inch Hg 3.388KPA
: 25.40
mm Hg
ISSUED 6-94
1 -9

SECTION I
GENERAL
1 pound/square foot
1
pound /sq. Inch
1 Pound/HP
1 -10
COMMON CONVERSIONS
MOONEY
M20R
0.488 kg/ meiersquare
. .2.036 Inch t:Jg .
. • 0.4538 kg{HP
ISSUED 6-94

MOONEY
M20R SECTION
II
LIMITATIONS
ITABLE OF CONTENTS I
TITLE .. . •
INTRODUCTION
NOISE LIMITS .
AIRSPEED LIMITATIONS .
AIRSPEED INDICATOR MARKINGS .
POWER PLANT LIMITATIONS
POWER PLANT INSTRUMENT MARKINGS .
FUEL LIMITATIONS
WEIGHT LIMITS
CENTER OF GRAVITY (GEAR DOWN)
MANEUVER LIMITS
FLIGHT LOAD FACTOR LIMITS
FLIGHT
CREW .
OPERATING LIMITATIONS
OXYGEN SYSTEM LIMITATIONS.
KINDS OF OPERATION LIMITS
KINDS OF OPERATION EQUIPMENT LIST .
DECALS & PLACARDS
CABIN INTERIOR
FUSELAGE INTF,RIOR .
EXTERIOR
FAA APPROVED
ISSUED
6-94
REV. G
PAGE
2-2
2-2
2-3
2-4
2-5
2-6
2-7
2-7
2-7
2-8
2-8
2-8
2-8
2-8
2-8
2-8
2-11
2-11
2-15
2-16
AIRPLANE FLIGHT MANUAL
2-1