Mooney M20B Guía de instalación y uso

~SERVICE

nnD

$84~AINTENANCE

~ANUAL

20B

tai~ooNEv’

AIRCRAFT,

INC.

iouls’

SCHREINER

FIELlj

KERRVILLE,

TEXAS

OLDWILLWAYNE

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OLDWILLWAYNE

7A8LE

CONTENTS

~NTRODUCTION

Page

General

Scope

Manual

t‘.

Description

fl.,´•HA~DLING

AND

SERVICING

Page

~4.

General

Access

Provfsions

Ground

Handling

HOISTING

LEVELING

MOORING

TOWING

Servicing

EfUEL

SYSTEM

LUBE

SYSTEM

BRAICE

SYSTEM

Lubrication

III,

POWER

PLANT

Page

General

Troubleshooting

Engine

Removal

Propeller

Removal

Engine

Installation

Propeller

Installation

Adjustments

CARBURETOR

IDLE

~MMTURE--

ENGINE

IDLING

SPEED

rv.

STRUCTURE

Page

´•A.

General

Removal

Wing

Components

REMOVALOFWING

REMOVAL

WING

FLAP

REMOVALOFAaEROr:

Installation

Wing

Conrponents

INSTALLATION

WING

INSTALLATION

FLAP

INSTALLATION

AnLErlN

LANDING

GEAR

AND

BRAKE

S’ISTEM

Page’

General

Removal

Landing

Gears

MAIN

LANDING

GEARS

´•NOSE

GEAR

Removal

ar,t!

Disassembly

Shock

Discs

MAIN

GEAR

NOSE

GEAR

Reassembly

and

Installation

Larding

Gent

MAIN

GEAR

NOSE

GEAR

Brake

a.-,d

Wheel

Maintenance

BRAKE

LINING

INSPECIION

AE~0

REPLACEMEh"P

~HEn

ASSEMBLYINSPECTION

Lctzolrng

Gear

Rigging

Procedure

OLDWILLWAYNE

Ys,

TABLE

CONTENTS,

Continlted

VL.

CONTROL

SURFACES

Page

General

Removal

and

Installation

AnERONS

RUDDER

ELEVATORS

FLAPS

Contro?Swfaces

General

Specifications

WINGS

~MPPYNNACE

REMOVABLE

CONTROL

SURFACE

Rigging

and

Adjustment

ILTLERON

RIGGING

AND

ADJUSTMENT

TRIM

RICGTNG

AND

ADJUSTMENT

FLAP

RIGGING

AND

ADJUSTMENT

RUDDERRIGGINGAND

ADJUSTMENT

ELEVATOR

RIGCINC

END

ADJUSTMENT

VII.

FUEL

SYSTER;Z

Page’44

General

Troubleshooting

Removal

and

nstcrllation

Fuel

Pumps

ELECTRIC

FUEL’PUMP

RIECHANICAL

FUEL

PUZMP

Removal

and

Installation

Fuel

Selector

V~rlve

RE~IOV.4L

INSTALLATION

E..Fietd

Repair

Fuel

Cells

GENERAL

--=-2.´•

APPAOV~DIMATERIALS

HANDLING

AND

MIXNNG

SEALANT

APPLICATIONINSTRUCTIONS

DESCRIPTION

LEAKS

LEAK

DETECTON

LEAK

REPAIR

PROCEDIjRE

vnI.

ELECTRICAL

SYSTEM

Page

General

´•B.

T702tbleshootin4

ELECTRICAL

S~ITCHES

AND

CIRCUIT

BREAKERS

BATTERY

CHARGING

RATE

Electrical

System

Master

Diagram

rr´•

EQUIPMENT

LIST

--;-’z;

DRA\MNG

NOTES

WnuNe

TABLE

IX.

~ZNSTRUMENTS

Page

General

INSPECTION

Page

~74

General

Prefiight’-lnspections

Hour

Inspections

Hour

Inspections

10G

Hour

Inspections

Oz;erLi7nits

Inspections

Post

Inspection

Checks

i’

OLDWILLWAYNE

LIST

ILZIUSTRATIO~S

Table

Leading

Particulars

and

Principal

Dimensions.

Page

Access

Panels

and

Plates.

Page

jacking

Arrangement,

Page

L~Pveling

the

Aircraft.

Page

Plei~fiing

the

Aircraft.

Page

Attachment

Nose

Wheel

Steering

Bat.

Page

Fuel

Strainer

Drain.

Page

B´•ake

Cylinder

Reservoir.

Page

Lubrication

Chart.

Page

Recommended

LubricatingOils.

Page

1’6

Table

Engine~Troubleshooting.

Page

10,

Aircraft

Wing

Skin

Chart.

Page

11.

Aircraft

Fuselage

Skin

Chart,

Page

Aircraft

Tail

Surfaces

Skin

Chart.

Page

13,

GearRig~ingDiagram.

(SeeFigurel3A,13B,P3c)

Page

34,

35,

35B

14.

AiletonControlSystem.

Page

15.

Control

Travel

Jig.

Page

16,

Contrbl

System.

Page

17;

Flap

Control

System,

Page

18.

Ruddez

Control

System.

Page

Table

Fuel

System

Troubleshooting

Page

20,

Fuel

Valve

Assembly..

Page

21.

Typical

Sealant

Application.

Page

22.

FueI

Leak

Classification,

Page

52.

23.

Leaks

Which

Constitute

Flight

Hazard.

.,page

24.

Tank

Leak

Detection.

Page

Table

Hydrometer

Readings

vs.

Battery

Charge

Percent,

Page

Table

Electrical

System

Troubleshooting.

Page

Table

Electrical

Equipment

List,

Pages

26.

.Electrical

System,

Master

Wiring

Diagram.

(Figure26A&26B)

gages

8r´•

27,

Instrument

Panel,

Page

Table

instrument

Troubleshooting.

Page

28.

Three

View

Drawing.

Page

OLDWILLWAYNE

SECTION

INTRODUCTION

OLDWILLWAYNE

GENERAL

This

manual

contains

service

and

maintenance

information

for

the

MOONEY

20B

Aircraft

which

was

designed

and

manufactured

high

performance,

low

main-

tenance,

versatile

aircraft

for

the

personal

and

business

aviation

field.

SCOPE

THIS

MANUAL

Sections

two

and

ten

comprise

the

service

pirt

this

handbo~k,

whereas

the

remaining

sections

comprise

the

maintenance

instructions.

The

service

instructions

in-

clude

ground

handling,

servicing,

and

periodic

inspections.

The

maintenance

instruc-

tions

for

each

system

include

trouble-shooting,

removal

and

installation

components,

corrective

maintenance

and

testing;

each

major

system

the

aircraft

covered

separate

section.

Only

personnel

should

perform

the

operations

described

this

manual.

The

desc’;iption

the

aircraft

includedP

this

section

limited

general

infor-

mation.

Refer

the

"Owners

Operating

Manual"

for

detailed

description

the

aircraft.

Tab;e

lists

the

leading

particula;s

and

principal

dimensions.

OLDWILLWAYNE

Table

I~EADING

PARTICULARS

AND

PRfNCIPAL

´•tio;~

ENGINE

Model

Type

Certificate

286

Rated

Horsepower

180

Rated

Speed,

rpm

2700

rpm

Cruise

speed

(Economy)

2350

rpm

Cruise

speed

(performance)

2450

rpm

Fuelconsumption

(economy

cruise)

gph

OilConsumr,tion

(!!erformance

cruise)

0.80

qt.

Propeller

d~ive

ratio

1.1

Propeller

shaft

rotation

Clockwise

Bore

-5.125

in.

Stroke

4.375

in.

Displacement

361.0

cubic

in.

Compression

Ratio

8.50:1

Pry

weight

(with

starter

generator)

286

Height

24.59

in.

Width

33.57

in.‘

Length

29.81

in.

Oil,

SAE

numbers:

above’40’

F(4.4’

SAE

Between

40’

F14.4’C)

and

10’

(-12.2"

SAE

Below

10"

F(-12.2’

SA~

Oil

Sump

Capacity~

8.qts.

Fuel,

Aviation

grade

(minimum)

91-96

Carburetor,

Marvel-Schebler

4-5

Magneto,

Bendix

Scintilla(2)

S4LN-204

(Right)S4LN-200

(Left)

Magneto

Timing

degrees

RTC

Magneto

Point

Setting

.018 .006

Spark

Plug

Gap

Setting

(Shielded)

,015to.018

Tachometer

drive,

ratio

crankshaft

0;5:1

’i’’

Firing

order

1-3-2-4

Tachometer

drive

rotation

Clockwise

Starter

drive,

ratio

crankshaft

13.55:1

Starter

drive

rotation

Cour;terclockwise

Starter,

Delco-Remy

12V

1109689

Generator

drive,

ratio

crankshaft

Generator

drive

rotation

Clockwise

Generator,

Delco-Remy

12V

Amp

110191.5

Generator

voltage

regulator,

I)elco

Remy

1119224

A-N

Vacuum

Pump

Drive,

ratio

crankshaft

1.30:1

A-N

Vacuum

Pump

Drive

Rotation

Coirntercloc~u´•ise

Propeller

governor

drive

20010

type

FuelPump

drive

E~unger

.i\

,2.

OVERALL

’C~ing

Span

ft.

in.

Length

2.3

ft.

in.

Height

ft.

in.

´•Clearance,

Propeller

tips

10~

in:Approx.

-2-

OLDWILLWAYNE

Table

L~EADIPfG

PARTICULARS

PRINCIPAL

DIMENSIONS

CONTROL

SURFACES

Aileron

Travel

12540

170

Down

Neutral

Static

00to20Down

´•Full

Down

213/4

Flb,

Travel

Intermediate

Down

110

Neutral

Elevator

Travel

240

Down

10’~40

Trim

Full

Nose

-180

to-200

RudderRight

180

Left

1801~

LL4NDING

Type

Manually

Retracted

Thread

feet

inches

Main

FVh,el

T;ypi~

Cleveland

Air

Products

Main

Tire

6iPly,

6:00

Main

Tire

Pressure

Pounds

Brake

Type

Cleveland

Hydraulic

Fluid

Required

Hydraulic,

3580

Nose

~cel

Type

Goodyear

Products

Nose

Tire

ply,

500x5

Ndse

Tire-Pressure

Pounds

PROPELLER

Manufacturer

McCauley

tr.s

Type

Constant

Speed

´•c,

Hub

2D36C14

Blade

78KM-4

’Diameter

Inches

Control

Governor

Woodward

Blade

´•Ang~e,

Low

12.7"t

B1´•de

Ane~e,

High

n.5’

.5’

TANK

CAPACITIES

Main

Fuel

Cells(2)

Gallons

Engine

Oil

Sump

Quarts

mT~INGS

Span

Feet

Inches

Len~th

Flap,

Trailing

Edge

Fee-i

Inches

Length.of

Airleron,

Trailing

Edge

Feet

3’k

Inches

Dihedral,

Leading

Edge

5’

Minutes

Incidence

2’

~Iinutes

OLDWILLWAYNE

:;:~r´•´•

AND

PRINCIPAL

DIMENSIONS

EMPEi\TNAGE

Vertical

Fin

Art~a

7.9

Square

Feet

Rudder

Area

5.01

Square

Feet

Horizontal

Stabilizer

Area

21.5

Square

Feet

Elevator

Area

12.0

Square

Feet

WING

AREAS

Wings

(total

area

less

naps

and

ailerons)

16?,Square

Feet

Total

Aileron

Area

11.2

Square

Feet

Total

Flap

Area

17.2

Square

Feet

DESCRIPTION

The

NEY

0 8

four

place,

low

wing_monoplane

metal

construc-

tion.

powered

180

horsepower

Lycoming

0-360-AID

engine

and

equipped

with

all

metal

McCauley

constant

speed

propeller.

Conventional

i;Sipe

controls

are

provided

with

rudder

pedals

and

control.

wheels.

Entrance

the

cabinis

made

through

the

cabin

door

:ocated

the

right

side

the

airplane.

The

front

seat

backs

fold

forward

allow

passenger

entry~to

the

rear

seats.

The

baggage

compartmen~

the

rear

seat

and

outside

baggage

door

located

aft

the

cabin

door.

The

baggage

compartmenf

is’

accessible

from

the

rear

seat

during

flight.

I.’ENGINE

The

Lycohing

0-360-AID

engine

rated

180

27d0

RPM

and

mounted

on~dynafocal

engine

mounts

dynamically

~balance

the

engine

during

flight

and

the

transmission

vibration

the

cabin

WING

The

MoontyM2OB

uses

laminar;flow

wing.

This

wing

reduces

drag

improves

aerodynamic

efficiency

over

standard

airfoils,

and

yet

retains

verv

docile

slow-

flight

and

stall

characteristics.

FUSELAGE

The

fuselage

tailcone

section

monocaque

construction.

Aluminum

ski?,

dip-

ped

zinc-chromate

primer

for

corrosion

protection,

riveted

heat-treated

aluminum

b~kheads

form

the

tail

cone

section.

Extruded

aluminum

stringers

add

longitudinal

strength

the

tail

cone.

The

tail

empenr~age

constructed

optically’aligned

jigs

that’~sure

uni-

formity

and

tolerance

fit~

for

all

parts.

IGNITION

This

engine

utilizes

the

latest

ignition

system

which

gives

quicker,

easier

starts

and

longer

ignition

life.

PROPEI~LER

inch

M~Cauley

all

metal

constant

speed

propeller

provides

low

pitch

set-

ting

for

maximum

take-on

power

and

automatic

pitch

changing

controlled

bj´•

engine

mounted

governor

for

maximum

efficienc3´•

cruising

speeds.

--e

OLDWILLWAYNE

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