Mooney M20M Owner's manual

PILOT'S OPERATINGHANDBOOK
AND
FAAAPPROVED
AIRPLANE FLIGHT MANUAL
MOONEY
M20M
MOONEYAIRCRAFT CORPORATION
LOUIS SCHREINER
KERRVILLE, TEXAS
78028
SERIAL NUMBER:
REGISTRATIONNUMBER:
FAA APPROVED: 3- 16- ?a
Henry A Arrnstrong
Manager,Airplane CertificationOftice
FEDERALAMATION ADMINISTRATION
FortWith,Texas
76193-0150
FAAAPPROVED in NormalCategory based on CAR PART 3 and applicable
<
portionsof FAR PART23; applicableto Model M20MSIN listed above only.
ORIGINAL ISSUE 3 - 90
RevisionA
1 - 96
POHIAFMNUMBER - 3501
27-0062
N1091A

INTRODUCTION MOONEY
M20M
/
WLCOMETO MOONEY'S NWSTDIMENSIONINSPEED, QUALIlYAND ECONOMY.
YOUR DECISION TO SELECT
A MOONEY AIRCRAFT HAS PLACED YOU IN AN ELITE
AND DISTINCTIM.CLASS OF ARCRAFTOWNERS. V1E HOPEYOU FINDYOUR MOONEY
A UNIQUE RMNG EXPERIENCE, VU-IrnER FOR BUSINESS OR PLEASUfE, THE MOST
PROFITABLE
EVER
- NOTICE -
This manualis providedas an operatingguidefor the MooneyModelM20M. It isimportant
that you --regardless of your previousexperience
- carefully read the handbook from
coverto coverand reviewitfrequently.
All information and illustrations in the manualare based on the latest product information
available at the time of publication approval and all sections including attached supple-
ments are mandatory for proper operation ofthe aircraft. The right is reserved to make
changesat any time without notice. Every effort has been madeto presentthe material in
a clear and convenient manner to enable you to use the manual as a reference. Your
cooperation in reporting presentationand contentrecommendationsissolicited.
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
outlined portion, is a boxwhich denotesthe manual number and issueor revisionof the
manual. It will be advanced one letter, alphabetically, per revision. Wth each revision to
the manuala new
List of EffectivePages showing all applicapablereyisionswith dateof
approval and a "Log of Revisions" page($ ,with only the latest Revlsion shown, will be
provrded to replacethe previous ones. It IS theoperatorsresponsiblllty to ensurethat this
manualiscurrentthroughthe latest published revision.
This handbook
will be kept current by MooneyAircraft Corporationwhen the yellow infoma-
tion card in front of this handbook has been completed and mailed to the Service Parts
Department, MooneyAircratlCorporation,Louis SchreinerField, Kenville,
TX, 78028.
ISSUED
3 - 90

INTRODUCTION
MOONEY
M20M
LIST OF EFFECTIVE PAGES I
....................
ORIGINAL 3 - 90
....................
RevisionA I - 96
Alwaysdestroysuperseded pageswhen inserting revised pages.
.................
CONGRATULATIONS A
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! POHIAFM NUMBER - 3501 [ A ]]
ISSUED 3 - 90
This POHIAFM effectivebeginning with M20M SIN 27-0053
i

INTRODUCTION MOONEY
M20M
~UST OF EFFECIVE PAGES Icont.) I
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6-1 thru 65 Original
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IPOHIAFM NUMBER - 3501 [ A ] I
ISSUED 3 - 90

INTRODUCTION
ISSUED 3 - 90
MOUNEY AIRCRAFT CORPORATION
LOUIS SCHREINER FIELD
KERRVILLE, TEXAS
78028
LOG OF REVISIONS
POHIAFM No. 3501
RN. A
iii
Date
Agfi49$
vertical
black l~nesin the narptn.
FAA
Approved
Description
of Revisions
Revision
Number
Revision
Pages
A T.P., Congrat.,
i thnr iv, 1-5,
2-3,2-4,245,2-11,2-12,2-14,
3-1,3-10,4-8,
4-10,7-8,7-9,
7-16,7-17
1-3, 1-7,2-5,
2-6,3-63-9,
4-14,6-13,7-1
1-6.3-17,3-18,
53,7-20,7-32
3-15,3-16,4-5,
4-9,7-23
54.7-18,7-19,
7-21,7-22,7-31
6-6,6-7
The revised
Revised Data
Added Data
Relocated Data
Revised
& Added Data
Revised
& Relocated Data
Revised Graphs
portions of affected pages are indicated
by

INTRODUCTION
LOG OF REVISIONS
(con't.)
MOONEY
M20M
REV. A
MOONEY AIRCRAFT CORPORATION
LOUIS SCHREINER FIELD
KERRVILLE, TEXAS 78028
LOG OF REVISIONS
ISSUED 3 - 90
Date
black lines in the narsin.
POHIAPM NO. 3501
FAA
Approved
indicated
by vertical
Description
of Revisions
portions
of affected pages are
Revision
Uunber
Revision
Pages
The revised

MOONEY
MODEL M20M INTRODUCTION
....
TITLE
, ................. " ........,
CONTENTS
..............................
.......... SECTION
GENERAL
.......
LIMITATIONS .......
EMERGENCY PROCEDURES ...
NORMALPROCEDURES .....
PERFORMANCE .......
WElGHT&BALANCE ......
AIRPLANE & SYSTEM DESCRIPTIONS
HANDLING, SERVICE
& MAINTENANCE
SUPPLEMENTALDATA
......
SAFETY & OPERATIONALTIPS ...
ISSUED 3 - 90

INTRODUCTION MOONEY
MODEL
M20M
BLANK
ISSUED 3 - 90

MOONEY
MODEL
M20M
SECTION I
GENERAL
TITLE ................ PAGE
THREE VIEW
................. 1.2
INTRODUCTION ................. 1.3
.................
DESCRIPTIVE DATA 1.3
.................
ENGINE 13
............. Accessories 1.3
...............
Ratings 13
................
PROPELLER 1.4
.................
FUEL 1.4
.................
OIL 1.4
LANDING GEAR ............... 1.4
MAXIMUMCERTIFICATEDWEIGHTS ........ 1.5
STANDARDAIRPLANE WEIGHTS ......... 1.5
CABIN & ENTRY DIMENSIONS .......... 1.5
BAGGAGE SPACE AND ENTRY DIMENSIONS ..... 1.5
............. SPECIFICLOADINGS 16
............ IDENTIFICATIONPLATE 1.5
SYMBOLS. ABBREVIATIONS & TERMINOLOGY
....... 1.6
GENERALAIRSPEED TERMINOLOGY & SYMBOLS
... 1.6
ENGINE POWER TERMINOLOGY ......... 1.7
AIRPLANE PERFORMANCE & FLIGHT PLANNING
TERMINOLOGY
............... 1.7
ENGINECONTROLS & INSTRUMENTSTERMINOLOGY . . 1.7
METEOROLOGICALTERMINOLOGY ........ 1.7
WEIGHT & BALANCE TERMINOLOGY ........ 1.8
MEASUREMENTCONVERSION TABLES .......... 1.9
ISSUED 3 . 90

SECTION I
GENERAL MOONEY MODEL M20M
FIGURE 1 - 1 THREE VIEW
ISSUED 3 - 90

MOONEY
M20M
I INTRODUCTION I
SECTION I
GENERAL
ThisOperatorsManualconformsto GAMA SpecificationNo. 1and includesboth Manufac-
I
ture? material and Fy.APPRObEi? material.requlredto be furnished to the Pilot by the
applicable FederalAviation Regulations. Section IX contains supplemental data supplied
- by MooneyAircraft Corporation.
Section
I containsinformationofgeneral interestto thepilot. It also containsdefinitions of
theterminologyused inthisOperatorsManual.
This Pilot'sOperatingHandbookis not designed as a substitute for adequate and compe-
tent fliaht instruction. knowledaeofcurrent ailworthiness directives, applicablefederal air
reaulafionsor advisorv circulars. It is not intendedto be a~uidefor bdcflight instruction
or-a trainingmanualaiid should not beusedfor operationdpurposesunlegkeptin an up
to datestatus.
All limitations, procedures,safety practices, servicingand maintenancerequirementspub-
lished inthis POHIAFM are considered mandatoryfor the ContinuedAirworthiness of this
airplaneina condlion equalto that ofitsoriginal manufacture.
[ DESCRIPTIVE DATA I
ENGINE
Numberof engines
EngineManufacturer
Model
~ecommended' TBO
TYPe
Numberof'cy1inder.s
Displacement .
Bore ....
Stroke
compression ratio '
1 ...........
.......... ~extr6n-~ycomin?
........... 10-540-AFIA
.......... 2000 Hours
. . ....
. . Reciprocating,air coc&d, fuel injected,Turbocharged
......... 6, Horizontallyopposed
........ 541.5 Cu. In. (8875 cc)
.......... 5.125 In. (13.0 cm)
....... 4.375 In. (11.11 cm)
............ 8.0:l
* Tl0540AFlB WGlNE INSTALLED WN 27-0211 8 ON. OPTIONAL FOR S/N 27-0053 I
THRU 27-0107.
FuelSystem
....... Fuel lniection
Accessories
Magnetos . PressurizedSlick 6260 & 6261 (IMPULSE)
IgnitionHarness
........ . . ShieldedlBraided
.........
Spark Plugs iexiron-iycoming SI 1042) (18 rnlm)
...........
OilCooler Stewart
- Warner Full Row
.............
Alternator (2) 28 Volt DC,
70 AMPS
................
tarter 24voltDC
...............
Intercooler Lycoming
Turbocharger
......... Airsearch - ModelTA0413
....
Turbocharger Controller System ~ensiiyl~ifferentialPressureController
Ratings:
.........
MaximumTakeoff Sea LevelBHPIRPM 27012575
ISSUED 3
- 90 REV. A -1 - 96 1-3

SECTION I
GENERAL
MOONEY
M20M
PROPELLER
Number ................. 1
Manufacturer
............. ~c~auley
............
ModelNumber Bj~3i~417182~RD-7
Numberof Blades .......... 3
..........
Diameter(No cutoffalloweci) 75 in: (19b.5 cm)
Type
.......... ... ConstantSpeed
Governing
. tiydraulically conirolled by engine oil.
BladeAngles
rgj 30:0 in. Sta.:
............
Low 15.1 degrees+/-O.2degrees
............
High 43 degrees +
1- 0.5 degrees
MinimumFuel Grade (Color) . 100 LL (Blue) or 100Octane (Green)
Total Capacity
........... 95 U.S. Gal. (359.6 Liters)
. Usable ........... 89.0 U.S. Gal. (336.9 Liiers)
OIL
-
Oil Specification ....... . MIL-L-22851
and as'Approv& by
~ekron- cornin in^
(Reference EngineOperatorsManual)
Above
30' F(-lo C) Ambient Air (S.L.) . SAE40 or
SAE 15W50
Below 30' F(-lo C) Ambient Air (S.L.) .
SAE 30 or 20W30
Total Oil Capacity ......... I0Qts. (9.5 liters)
(Minimumfor Flight)
......... 6 Qts. (5.7 liters)
011 Filter ................. FullFlow
Oilgrades,specificationsand changing recommendationsarecontainedinSECTION W11.
LANDING GEAR
TYPE: Electrically operated, fully retractable tricycle gear with rubber shock discs. The
mainwheels have hydraulicallyoperateddisc brakes. The nosewheel isfully steerable11'
. .
leftto 13' rightofcenter.
............
MeelBase 79 9/16 in. (198.91 cm)
.............
MeelTrack 11
0 in. (279.4 cm)
Tire Size:
Nose
........... 5.00 x 5 (6 ply)
Main
............ 6.00 x 6 (6 ply)
Tire Pressure
Nose ............... 49 PSI
Main
............... 42 PSI
MinimumTurning Radius (No brakesapplied)
Right
............... 40ft.(12.0m)
Left .............. 48 ft. (14.4 m)
ISSUED 3 - 90

MOONEY
M20M SECTION
I
GENERAL
MAXIMUM CERTIFICATED WEIGHTS
.........
Gross Wiht 3368 Lbs. (1528 Kg)
I MaximumLandingkight .......... 3200 Lbs. (1452 Kg)
............
BaggageArea 120 Lbs. (54.4 Kg)
..........
Rear Storage Area 10 Lbs. (4.5 Kg)
........
Cargo (Rear Seats ~oldedbwn)
340 Lbs. (154.2 Kg)
STANDARD AIRPLANEWEIGHTS
.............
Basic Empty Wight See Page1-8
UsefulLoad ...... Varies with installed equipment.
See
SECTION Vi for'specificairplane weight (pg. 6-6).
'CABINAND ENTRY DIMENSIONS
...........
Cabin With(Maximum) 43.5 In. (110.5 cm)
...........
Cabjn Length(Mymum) 126 In. (315 cm)
...........
Cab~nHe~ght(M~mum) 44.5 In. (113cm)
...........
Entry Wdth (Min~mum) 29.0 In. (73.4 cm)
...........
Entry Height (Minimum) 35.0 In. (88.9 cm)
BAGGAGE SPACEAND ENTRY DIMENSIONS
............
Compartment Wdth 24 In. (60.9 cm)
............
CompartmentLength 43 In. (109.2 cm)
............
Compartment Height 35 In. (88.9 cm)
Compartment Volume
.......... 20.9 Cu. Ft.
(.&2 cubic meters)
Cargo Area (with rearseat folded down) ...... 38.6 Cu. Ft.
il.09 cubic meters) I
..........
Entry Height (Minimum)
: 20.5 In. (52.1 cm)
...........
Entry Wdth 17.01n.(43.2cm)
..........
Ground to ~oiomof siil 46.0 In. (I16.8 cm)
SPECIFIC LOADINGS
Wng Loading
- @ MaximumGross Wight
....
Power Loading - @ MaximumGross Wight
....
. 19.26Lbs./Sq. Ft.
. "l?$qib!)IHP
(5.66 KgIHP)
IDENTlFlCATlON PLATE
All correspondenceregardingyour airplaneshould includethe Serial Numberas depicted
onthe identificationplate.The identificationplateis locatedonthe leflhandside, aflend of
thetail cone, below the horizontalstabilizer leading edge. The aircrafl Serial Number and
type certificateare shown.
ISSUED 3
- 90

SECTION I
GENERAL
MOONEY
M20M
F~L, ABBREVIATIONS & TERMINOLOGY I
GENERAL AIRSPEED TERMINOLOGY & SYMBOLS
GS GROUND SPEED
- Speed ofan airplane relativeto the
ground.
KCAS KNOTSCALIBRATEDAIRSPEED
- The indicatedspeed of
an aircrafl,corrected for post~onand Instrumenterror.
Calibratedairspeed is equal to true airspeed instandard
atmosphereat sea level.
WAS KNOTS INDICATEDAIRSPEED
- The speed ofan aircrait
as shown on itsairspeed indicator. IASvalues published
inthis handbook assume zero instrument error.
KTAS KNOTSTRUEAIRSPEED
- The airspeed.ofan airplane relativeto
undistubed airwhich isthe KCAS correctedfor altiiude and
temperature.
Va
MANEUVERINGSPEED-The maxjmum speed at which
application
of full available aerodynamic controlwill not
overstresstheairplane.
vfe
MAXIMUM FLAP EXTENDEDSPEED - The highest speed.
permissiblewith wing flaps in a prescribed extended posilon.
We
MAXIMUM LANDING GEAR EXTENDED SPEED -The
maximumspeed at which an aircraflcan besafely flown
with thelandinggear extended.
'40
MAXIMUM IANDINGGEAR OPERATING SPEED - The
maximum speed at whichthe landing gear can besafely
extended or retracted.
Vne
NEVER EXCEED SPEED - The speed limitthat may not be
exceeded at any tlme.
Vno
MAXIMUM STRUCTURAL CRUISING SPEED - The speed
that should not beexceeded except in smooth air and then
only with caution.
VS
STALLINGSPEED -The minimumsteadytlightspeed at which
the airplaneiscontrollable.
VSO
STALLING SPEED - The minimumsteady fiight speed at
which the airplane iscontrollableInthe landing configuration.
VX
BESTANGLE-OF-CLIMBSPEED - The airspeedwhich
deliversthegreatest gain of altitudeinthe shortest possible
horizontaldistance.
VY
BEST RATE-OF-CLIMBSPEED - The airspeedwhich delivers
thegreatestgain in altiiude intheshortest possibletimewith
gear and flaps up.
ISSUED
3 - 90

MOONEY
M20M SECTION
I
GENERAL
ENGINE POWER TERMINOLOGY
BHP
BRAKE HOFSEFOWER - Powerdeveloped bythe engine.
MCP MAXIMUMCONTINUOUSPOWER
- The maximumpower
fortakeoff, normal, abnormalor emergencyoperations.
CHT CYLINDER HEADTEMPERATURE
- Operating temperatureof
engine cylinder(@being monitored by a sensor unit. Expressed in°C
MP MANIFOLDPRESSURE
- Pressuremeasured in the engine's
inductionsystemand
IS expressed in ~nchedof mercury (Hg).
RPM REVOLUTlONS PER MINUTE
- Enginespeed.
TIT TURBINE INLETTEMPERATURE
- The exhaustgas temperature
measuredat theturbocharger turbine inlet. Expressed in
OF.
Turbocharger A device usedto supply increased amounts of air to an engine
inductionsystem. Inoperation,the t~bineisdriven by
engine exhaust gas mixture.The turblne drrectly drivesa
compressorwhich pumpsair intothe engineintake.
AIRPLANE PERFORMANCEAND FLIGHTPLANNINGTERMINOLOGY
Demon- The velocity ofthe crosswind component forwhich adequate
strated control ofthe airplaneduring takeoff and landingtest was
Crosswind actuallydemonstratedduringcertification.The value shown
Velocity is not considered to be limiting.
9 Accelerationdueto gravity.
Service The maximumatiude at which aircraft at gross weight hasthe
Ceiling capability of climbing at the rateof 100ftlmin.
ENGINECONTROLS 8 INSTRUMENTS TERMINOLOGY
Propeller The control usedto select engine speed.
Control
-.
Throttle The control used to select engine power by controllingMP.
Control
Mixture Providesa mechanicallinkageto thefuel injectormixture
Control control Controlto controlthe size ofthe fuel feed aperture, and
thereforethe airlfuelmixture.
It isthe primarymethodto shut the
engine down.
CHIGauge Cylinder headtemperatureindicatorused to determinethat engine
operatingtemperatureiswithin manufacturersspecifications.
Tachometer
An instrumentthat indicatesrotationalspeed ofthe Engine.
The speed
IS shown as revolut~onsper m~nute (RPM).
Propeller The devicethat regulatesRPM ofthe enginelpropellerby
Governor increasina or decreasina the orooelleroitch. throuah a itch
-.
change iechanismintiie propeiler hub.
.
METEOROLOGICALTERMINOLOGY
AGL Above ground level.
Density Altiiudeas determinedby pressure atiudeand existing
Miude ambient temperature. In standard atmosphere (ISA).density and
pressureatiude are ~ual.For agiven pressure
altitude, the h~gher
thetemperature, the hlgher the density altitude.
ISSUED 3 - 90 REV. A 1 - 96 1-7

SECTION I
GENERAL MOONEY
MODEL M20M
Indicated The numberactually read froman altimeter when, and only when
Pressure the barometricsubscalehas been set to 29.92 Inchesof
Altitude mercuryor 1013.2 millibars.
/
ISA INTERNATIONALSTANDARD ATMOSPHERE assumesthat
(1) The air is adry perfect gas; (2) The temperatureat sea level is
15 degrees Celsius (59' F); (3) The pressureat sea level is 29.92
inchesHg (1013.2 mb);
(4) The temperature gradientfrom sea level
tothe altitude at which the temperatureis -56.5' C (-69.7' F) is
-0.00198' C (-0.003564' F) per foot.
OUTSIDEAIR TEMPERATURE
- The free air static temaerature.
OAT
obtainedeither from inflight temperature indicationsoiground
meteorologicalsources. It is expressedindegreesCelsius.
Pressure The indicated pressurealtitudecorrected
for positionand
Altitude instrumenterror. Inthis handbook,altimeter instrument errors
are assumed to be zero.
Station Actual atmosphericpressureat field elevation.
Pressure
WEIGHT AND BALANCE TERMINOLOGY
Arm The horizontaldistancefrom the referencedatumto the center of
gravity (C.G.) of an item.
Basic The actualweight of the airplane and includes all operating
Empty equipment (includingoptional equipment) that has a fixed
Weight locationand is actually installed inthe alc.
It includesthe weight of unusable fuel and full oil.
Center of The point at which an airplanewould balance
if suspended.
Gravity Itsdistancefrom the reference datum isfound by dividingthe
(C.G.) total moment by the total weight of the airplane.
C.G. Arm The arm obtained by adding the airplane's individual moments
and dividingthe sum by the total weight.
C.G. in Center of Gravity expressed in percent of.mean
percent MAC aerodynamic chord.
C.G. The extremecenter of gravity locationswithinwhichthe
Limits airplanemust be operatedat a givenweight.
MAC MeanAerodynamic Chord.
Maximum The maximum authorizedweight of theaircraft and its
Weight contentsas listed in the aircraft specifications.
Moment The product of the weight of an item multiplied by itsarm.
(Momentdivided by a constant is used to simplify balance
calculationsby reducingthe number of digits.)
ISSUED
3 - 90

MOONEY
MODEL M20M SECTION
I
GENERAL
Reference
Datum An imaginaryvertical planefromwhichall horizontal distances
are measuredfor balance purposes.
Station
A locationalongthe airplanefuselage usually given in
terms of distancefrom the referencedatum.
The weight of chocks, blocks, stands, etc. used when
weighingan airplane, and is includedinthe scale readings.
Tare isdeductedfromthe scale readingto obtain the actual
(net) airplaneweight.
Tare
Unusable
Fuel Fuel remainingafter a runout test has been completed in
accordancewith governmentalregulations.
Usable
Fuel Fuelavailablefor aircraft engine combustion.
Useful
Load The basic empty weight subtractedfrom the maximum weight of theaircraft.
This loadconsists of the pilot, crew
if applicable,fuel,
passengers,and baggage.
..............................................- ....................................................
!MEASUREMENTCONVERSION TABLES,!
....................................................................................................
U. S. CustomaryUnit
. . Metric Equivalents
1 inch
. .
1foot . .
1yard
1 mile statute, iand)'
1mile [nautical .
internatidnat)
. 2.54centimeters
... 0.3048 meter
. .0.9144meter
. 1, 609 meters
. 1, 852 meters
U.
S. CustomaryUnit
. . Metric Equivalents
1 square inch .
1 square foot .
1 square yard .
. 6.4516 sq. centimeters
. 929.030 sq. centimeters
. . 0.836 sq. meter
U. S. CustomaryUnit
. Metric Equivalents
1cubic inch
1 cubicfoot
1 cubic yard
,16387cubic centimeters
. . 0.028 cubic meter
. . 0.765 cubic meter
U.S. Customary
LiquidMeasure
. MetricEquivalents
. 29.573 milliliters
........ 0.473 liter
.. 0.946 liter
........
3.785liters
I fluid ounce
1pint
. .
1quart . .
1gallon . .
ISSUED 3 - 90 1-9

SECTION I
GENERAL MOONEY
MODEL M20M
U.S. Customary . MetricEquivalents
Dry Measure
1 pint
...... 0.551 liter
..........
1 quart 1.101liters
...
BritishImperial . . U. S. Metric
Liquid and Dry ~easurd
. .
~~uivalenis . . ~~uivalents
...
1fluid ounce .0.961 U.S. . . 28.412 milliliters
. .fluid ounce,
. 1.734 cubic
inches
.....
1 pint . 1.032 U.S.
. dry pints,
. 1.201 U.S.
... liquidpts.,
. 34.678 cubic
inches
1quart
. 1.032 U.S.
.. dry quarts
.. 1.201 U.S.
. liquid qts.,
. 69.354 cubic
.. inches
1gallon
. 1.201 U.S.
. .277.420
, . . cubic inches
. . 568.26 milliliters
1.136liters
, . . 4.546 liters
.....
U. S. Customary Unit Metric Equivalents
(Avoirdupois)
........
1grain ,6479891 milligrams
..........
1dram 1.772 grams
..........
1ounce 28.350 grams
.........
1pound 453.59237 grams
.....
U.S. Customary Unit Metric Equivalents
..........
1PSlG 6.895 KPA
..........
1Inch Hg 3.388 KPA
..........
1 Inch Hg
25.40 mm Hg
ISSUED
3 - 90