Mooney M20S 1998 Maintance Manual

SERVICE

OLDWILLWAYNE

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OLDWILLWAYNE

AIRCRAFT

COPORATION

KERRVILLE,

TEXAS

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OLDWILLWAYNE

AIRCRAFT

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M20S

SERVICE

AND

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MANUAL

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OLDWILLWAYNE

AIRCRAFT

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M20S

SERVICE

MAINTENANCE

AND

MANUAL

INTRODUCTION

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INTRODUCTION

INTRODUCTION´•1

SERVICE

OLDWILLWAYNE

AND

MAINTENANCE

MAN

UAL

M20S

MOONEY

AIRCRAFT

CORPORATION

The

following

on

components

listed

due

repair

Any~eublications

available

stations

through

As

publications

ENGINE

The

following

Products,

Overhaul

Illustrated Maintenance Service Fuel

Injector

ACCESSORY

list

the

to

through

Mooney

PUBLICATIONS

P.O.

Manual

Parts

Bulletins

Manual,

PROPELLER

McCauley

dalia,

Propellers

0~.,45377.

of

Manufacturers

of

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configurations

many

for

a

particular

available

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any

Aircraft

various

on

maintenance

Box

90,

Mobile,

for

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Catalog

Operators

Specify

Form

PUBLICATIONS

Obtain

Model

avionics

from

Mooney

Service

Corporation,

components

VENDOR

publications

Alabama,

Continental

for

Teledyne

Manual

model

for

of

X30593A

publications

SUPPLEMENTARY

and/or

publications

M20S.

that

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manufacturer.

Aircraft

Center.

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maintenance

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from

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series

data

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listed

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aircraft

10-550

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and

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in

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publications

applicable

the

to

Continental

Receivable

Models,

engines,

aircraft desired

3535

maintenance

or

publications

be

can

Parts

obtained

Price

are

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below.

Motors,

(Prepaid

Form

X30568A.

Form

engines,

when

Form

ordering.

McCauley

information

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not

only).

X30569A.

from

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Drive,

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Van-

Service

MAGNETO

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cations

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36601,

FUEL

Teledyne

cations

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Master

Aircraft

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SPEED

Precise

Manual

Continental

Dept.,

Service

Alabama,

Manual,

Attn:

PUMP

Continental

Dept

Service

Flight,

No.

TCM

for

Instructions,

Teledyne

Publications

(Engine

SYSTEM

Manual,

Products,

BRAKES

Inc.,

780630

Motors,

USA,

Motors,

63120

(Bendix),

36601,

Continental

Dept

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S6RN´•25

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Products,

Systems

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C200

Publications

Alabama,

Rd.,

Bend,

series

P.O.

Series

Teledyne

Aircraft

P.O.

and

Components,

OR

constant

Box

90,

magnetos.

Continental

Dept.

Products,

Box

90,

USA,

97701,

speed

Mobile,

Form

36601,

Telephone:

propellers.

Alabama,

Motors,

P.O.

Alabama,

X40000,

Attn:

Aircraft

Box

90,

Publications

(503)

USA,

Products,

Mobile,

USA,

36601,

Teledyne

382-8684

36601,

Alabama,

Continental

Dept

Attn:

P.O.

Publi-

Box

USA,

Publi´•

Mo´•

INTRODUCTION-2

INTRODUCTION

MOONEY

OLDWILLWAYNE

AIRCRAfT

CORPORATION

M20S

SERVICE

AND

MAINTENANCE

MANUAL

CHAPTER

4

1

5

6

7

8

9

CHAPTER-

SECTION

00

10

20

00

10

00

10

20 30

TITLE

INDU(GUIDE

TITLE

RESERVED

LIMITS/MAINTENANCE

TIME

GENERAL

TIME

SCHEDULED

DIMENSIONS

GENERAL

LIFTING

JACKING

LEVELING

TOWING

GROUND

TOWING

TAXIING EMERGENCY

LIMITS

AND

MAY

MAINTENANCE

AND

WEIGHING

TAXIING

HANDLING

PROCEDURES

USED

BE

AREAS

LATER

CHECKS

20

21

24

10

11

12

00 10

20

00

10

20/30

00

10

20

00

40

50

60

00

30

40

50

PARKING

AND

GENERAL

PARKING

MOORING

PLACARDS

AND

GENERAL

MARKINGS

PLACARDS

SERVICING

REPLENISHING SCHEDULED

STANDARD

PRACTICES

GENERAL

ENVIRONMENTAL

CABIN

HEATING

VENTILATION

COOLING

TEMPERATURE

ELECTRICAL

GENERAL

DC

GENERATION

EXTERNAL

ELECTRICAL

MOORING

MARKINGS

EXTERIOR/INTERIOR

SERVICING

AIRFRAME

SYSTEMS

SYSTEM

CONTROL

POWER

POWR

LOAD

DISTRIBUTION

INTRODUCTION

INTRODUCTION-3

SERVICE

OLDWILLWAYNE

AND

MAINTENANCE

MANUAL

M20S

MOONEY

AIRCRAFT

CORPORATION

CHAPTER

25

27

28

THISSECTION

INCLUDED

MAYNOTBE

IN

THIS

SECTION

00

M.

10

20

50 60

70

00

10 20 30

40

50 60 90

00

10 20

30

40

90

S

TITLE

EQUIPMENT/FURNISHI

GENERAL FLIGHT

PASSENGER

CARGO EMERGENCY

ACCESSORY

FLIGHT

GENERAL

AILERON

RUDDER

ELEVATOR

STABILIZER

WING

INTERCONNECT

MISCELLANEOUS

FUEL

GENERAL

STORAGE

DISTRIBUTION

DUMP

INDICATING

MISCELLANEOUS

COMPARTMENT

EQUIPMENT

COMPARTMENT

CONTROLS

SYSTEM

TRIM

SYSTEM

FLAP

SYSTEM

NGS

30

32

33

34

00 10

30

40

60

00

10 20

30

40

50

60 80

00

10/20

40

00

10

20

AND

RAIN

ICE

GENERAL

AIRFOIL

PITOT

AND

WINDSHIELDS PROPELLERS

LANDING

GEAR

GENERAL

MAIN

NOSE

LANDING

EXTENSION

WHEELS

AND

STEERING

POSITION

MISCELLANEOUS

LIGHTS

GENERAL

INTERIOR

PRACTICES

EXTERIOR

PRACTICES

NAVIGATION

GENERAL PITOT

STATIC

SYSTEM

DIRECTIONAL

PROTECTION

STATIC

GEAR

AND

BRAKES

WARNING

AND

LIGHTS

AIR

GYRO

AND

RETRACTION

MAINTENANCE

PRESSURE

COMPASS

DOORS

I

NTROD

UCTI

ON

´•4

NTROD

1

UCTI

ON

MOONEY

OLDWILLWAYNE

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AND

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MANUAL

CHAPTER

35

37

39

51

52

SECTION

THIS

INCLUDED

SECTION

TITLE

OXYGEN

GENERAL

CREW/PASSENGERS

MAY

NOT

THIS

S

IN

M.

BE

00

10/20

VACUUM

00

10

20 30

40

00

10

GENERAL

DISTRIBUTION

INDICATING

REPAIR OPERATIONAL

ELECTRICAL

COMPONENTS

GENERAL

INSTRUMENT

PROCEDURES

PANELS

AND

CONTROL

PANELS

ELECTRONICS

20

ELECTRICAL

EQUIPMENT

AND

RACKS

STRUCTURES

00

10

GENERAL

STRUCTURAL

REPAIR

GENERAL

DOORS

00

10

30

GENERAL CABIN

DOOR

PRACTICE

BAGGAGE

MAINTENANCE

COMPARTMENT

PRACTICE

DOOR

53

55

56

57

00

10 20 30

40 50

00

10

20

30

40

00

10/20

50

00

10 20

30

40 50

FUSELAGE

GENERAL

FRAME

MAIN

AUXILIARY

PLATES/SKIN

ATTACH

FITTINGS

FILLETS/FAIRINGS

STABILIZERS

GENERAL

HORIZONTAL ELEVATOR

VERTICAL

RUDDER

WINDOWS

GENERAL

WINDSHIELD

PLEXIGLASS

WINGS

GENERAL

FRAME

MAIN

AUXILIARY

PLATES/SKINS

ATTACH

FLIGHT

FITTINGS

SURFACES

STRUCTURE

STABILIZER

CABIN

DRILLING

STRUCTURE

WINDOWS

INTRODUCTION

INTRODUCTION-5

SERVICE

OLDWILLWAYNE

AND

MAINTENANCE

MANUAL

M20S

MOONEY

AIRCRAFT

CORPORATION

CHAPTER

60

61

71

72

73

SECTION

00

10

20

40

00

10

20

30

60

00

10

20

30

TITLE

STANDARD

PROPELLERS

GENERAL

PROPELLER

CONTROLLING BALANCING

POWERPLANT

GENERAL COWLING MOUNTS

FIRESEALS

NTAKES

AIR

I

ENGINE

GENERAL

ENGINE

FUEL

GENERAL DISTRIBUTION

CONTROLLING

INDICATING

PRACTICES

ASSEMBLY

PROCEDURES

RECIPROCATING

SYSTEM

79

74

76

77

78

40

00

30

40

00

20

00

20

30

00

30

20

50

10

IGNITION

GENERAL POWER

EMERGENCY

ENGINE

GENERAL

POWER

ENGINE

GENERAL

POWER

TEMPERATURE

PRESSURE

EXHAUST

GENERAL

INSTALLATION

EXHAUST REPLACEMENT

OIL

GENERAL

STORAGE DISTRIBUTION INDICATING

TRANSDUCERS

TROUBLE

CONTROL

SHUTDOWN

CONTROLS

INDICATING

SYSTEM

SHOOTING

RIGGING

COMPONENTS

80

INTRODUCTION-6

00

10

STARTING

GENERAL

CRANKING

INTRODUCTION

MOONET

OLDWILLWAYNE

AIRCRAFT

CORPORATION

M20S

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AND

MAINTENANCE

MANUAL

CHAPTER

81

91

95

SECTION

THIS

INCLUDED

SECTION

MAY

NOT

THIS

S

IN

M.

BE

00

20

30

TITLE

TURBINES

GENERAL

SCHEMATICS

GENERAL

ELECTRICAL

CHARTS

SCHEMATICS

SPECIAL

SYSTEM

EQUIPMENT

HARDWARE

INTRODUCTION

INTRODUCTION-7

SERVICE

OLDWILLWAYNE

AND

MAINTENANCE

MANUAL

M20S

MOONEY

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BLANK

INTRODUCTION-8

INTRODUCTION

CHAPTER

OLDWILLWAYNE

MAINTENANCE

TIME,

CH

LIMITSI

EC

KS

SERVICE

OLDWILLWAYNE

AND

MAINTENANCE

MANUAL

M20S

MOONEY

AIRCRAFT

CORPORATION

CHAPTER

SECTION SUBJECT

5-Effectivity

5-Contents

5-00´•00 5-10-00 5-20-01 5-20-01 5-20´•01

5-20´•01 5-20-02

5-20-06 5´•20´•06 5-20-06 5-20-06 5-20-06 5-20-07

5´•20´•07

5-20-07

5´•20-07

LIMITS/MAINTENANCE

TIME

LIST

OF

1/2BLANK.

3/4BLANK.

CHAPTER

EFFECTIVE

PAGE

5.

6.

7.

8.

9.

10.

11.

12.

13.

14.

15.

16.

17.

18.

19.

20.

5

CHECKS

PAGES

DATE

11-98

11-98 11-98

11´•98

11-98 11´•98

11-98 11-98 11-98

11´•98

11-98

5-EFFECTIVITY

1/2BLANK

MOONEY

OLDWILLWAYNE

AIRCRAFT

CORPORATION

M20S

SERVICE

MAINTENANCE

AND

MANUAL

CHAPTER SECTION SUBJECT

5´•00-00

5´•00´•01 5-00-02 5-00-03 5-00-04 5-00-05

5-00´•06

5-00-07 5-10-00 5-10-01 5-20-00

5-20-01

5-20-02 5-20-03 5-20-04 5-20-05

5-20-06

5-20-07

LIMITS/MAINTENANCE

TIME

TABLE

General.

Landing

Flight

Wing

Electric

Instruments

Cabin

Fuel

Time

Schedule

CHAPTER

OF

SUBJ

Gear

Control

Flap

Power

Heating

System

Limit

Overhaul

Maintenance

Check

Aircraft

Engine

First

25

50

Hour

100

Access

Lubrication

5

CONTENTS

ECT

System

Systems.

System

Ventilating

Components

and

Replacement

Points,

Functional

File

Hour

Torque

Inspection

Cover

Identification,

and

CHECKS

Checks

Values

Check.

Service

Sy;tems

Schedule

Guide

PAGE

5 5

5 5 5

5

6

7

11

11 11 11

12

17

5-CONTENTS

3/4BLANK

SERVICE

OLDWILLWAYNE

MAINTENANCE

AND

MANUAL

M20S

MOONEY

AIRCRAFT

CORPORATION

5-00-00 AIRCRAFT

aircraft

aspirated,

all´•metal

covered

DESCRIPTION.

four

are

single-engine,

airframe with

semi´•monocoque

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controls

pushpull

control

blocks

dampen

mechanism

assist

co-pllot’s

bra’ke

position.

the

horizontal

5-00-03

Wing

controlled

the

on

wing.

ribs.l)ual

have

cylinders

dlsc

co-pilot

The

nose

is

wing

about

landing

featured

are

lights,

on

Bungee

mechanism

down.

gear

the

in

A

manifold

the

system

to

lowering

malfunction.

the

wheel

performance.

flight

are

tubes

wheels

i

ntai

ma

vibration.

links

control

in

rudder

installation

The

flaps

by

center

GENERAL

place,

has

nonstructural

tailcone,

Control

with

flight

toe

brakes

tricycle

wheel

fully

flaps

trim,

its

LANDING

Single

a

warning

the

electrical

takeoff

on

gear

pressure

landing

has

the

of

wells

FLIGHT

control

pilot

conventional

link

to

and

cent

n

the

pedals

manual

stabilizer

WING

are

electrically

a

spring

console.

M20S

The

high-performance,

low-wing

tubular´•steel

a

surfaces

stressed

control

controls.

brakes

that

supply

each

on

rudder

landing

controlled-bX~udder

ret

cta

ra

are

entire

the

monoplanes.

aluminum

and

a

skins

wheels

The

linkedilot’s

pressure

main

pedals

gear,

ble.

electrically

empennage

series

normally

cabin

skins,

full-cantilever,

structural

have

riveted

accompany

individual

gear

standard

are

having

operated.

of

The

frame

the

to

the

rudder

the

to

wheel.

pedalwide-span

pivots

points.

SYSTEM

system

self-adjusting

main

the

and

horn

rd

that

over-center

an

pressure

system

until

prevents

safe

a

warning

less

is

The

up.

manual

actuator

gear

reduce

extension

in

gear

SYSTEMS

can

co-pilot

in

operation,

control

pedals.

tube

interconnect

and

rudder

nation.

i

removable.

are

for

of

trim

attack.

electric

SYSTEM

actuated

"up-off-down"

has

a

gear.

a

gear

are

preload

actuated

flying

horn

than

electric

that

the

event

doors

sound

be

seat.

surfaces

Formica

alignment

systems

The

the

system

steerable

hydraulic

Gear

position

ndard

sta

thethe

position

safety

electric

speed

sounds

a

pre´•set

gear

system

permits

of

fully

ana

levels

operated

All

flight using

to

guide

and

spring

standard

dual

A

co´•pilot’s

sets

and

switch

an

the

to

are

gear

disc

on

ii

springs

In

air

An

throttle

a

gear

the

CONTROL

or

the

rudder

An

aileron

coord

is

optional

or

FLAP

loaded

GEAR

oorboa

gear

Landing

to

systems

rol

angle

a

5-00-04

Master

The

i.

electrical

28

Volt,

batteries.

protective

lights,

Circuit

lights,

interior

gear

boost

retraction/extension

light.

Standard

landing

lights,

fuel

gear

extension

(optional)

5-00-05 All

flight

Flight

Panel.

co-pilot’s

pressure

instrument

air

pickup

that

open

source

instrument

manual

5-00-06

The

cabin

mixed

is

dimming

heater

heat

temperature.

system

the

system

5-00-07

The

the

through

Fuel tank. forward

The crankcase.

tank

the

side

to

windshield.

is

fuel

system

forward,

aft,

a

sump

The

section

engine-driven

are

engine

the

of

indicating

gauges

A tank

below

5-10-00

It

are

fuel"

"low

activated

is

2

recommended

is

1/2

components

the

specified

component

service

data

ELECTRIC

Switch

alternator

relay

breakers

electrical

system,

and

equipment

power

alternator

The

electrical

2´•100;

lights,instrument

stall

and

pump,

an

override,

and

instruments

to

ports

to

electrical

an

-INSTRUMENTS

operate

static

pressure

tone

the

atmosphere.

provided

panel/glareshield

mechanisms.

CABIN

SYSTEMS

muff

encasing

source.

Air

nozzles

inboard

NACA

drains

electric

Two

cluster

pilot’s

ambient

An

FUEL

has

of

fuel

in

routed

at

top

scoop

are

fuel

the

fuel

series

gauge.

panel,

with

available.

outboard

wired

systems.

for

partial

warning

when

gallons.

TIME

that

should

period

accordance

in

or

airworthiness

or

POWER

and

comprised

two

system

an

overvoltage

circuit

or

wiring

watt

warning

electric

an

flap

are

instruments

pitot

the

airspeed

each

on

HEATING

the

Hot

air

from

windshield

the

optional

SYSTEM

sealed,

section

corner

the

on

the

at

pump

fuselage,

pump

quantity

to

The

activates

The

fueling

annunciator

usable

LIMIT

be

COMPONENTS

overhaul

accomplished

of

SYSTEM

AMP

10

has

and

includes:

relay

breaker

equipment

lights,

power

taxi

panel/glareshield

system,

starter,

system,

electric

system.

in

shock-mounted

the

system

side

of

alternate

An

center

lighting

VENTILATING

exhaust

the

from

the

defrost

controls

main

air,

integral

of

each

of

lower

lowest

the

is

in

aft

mounts

transmitters

fuel

quantity

Master

the

optional

of

wing

fuel

or

operation

with

directives.

control

100

of

a

24

HR,

an

overvoltage

annunciator

switches

2´•100

navigation

electrical

an

electric

an

manual

with

trim

are

system

in

provides

indicator.

has

two

the

tailcone)

console.

systems

heater

tank

bottom

the

gauges

is

defrosts

motor

tanks

Vents

surface.

in

firewall.

engine

in

system

heater

base blower

wing

wing.

wing

point

the

of

on

Switch,

fuel

qua

visual

tanks..

for

light

quantity

replacement

later

not

for

manufactures

5-00-00

the

AMP,

Volt,

from

watt

the

air

The

static

The

have

the

muff,

cabin

duct

in

at

vent

each

left

each

in

left

each

goes

of

than

that

MOONN

OLDWILLWAYNE

AIRCRAFT

CORPORATION

M20S

SERVICE

MAINTENANCE

AND

MANUAL

The

specified

component,

component

maintenance,

5-10-01

ITEM

Actuator

All

other

Engine

Propeller

Magnetos

Induction

All

other

Selector

Fuel

Flexible

All

Hoses

other

overhaul

do

not

will

reach

OVERHAUL

Landing

No-Back

Spring

Avionics

Plessey

Components

Powerplant

-T~M’

Air

Filter..

Components

Fuel

Valve

(All,

Components

time

constitute

that

limits,

time

if

a

guarantee

limit

without

MAINTENANCE

RECOMMENDED

Gear

(GEC)

011

System

(AirightorChristopher

except

(includes

Teffon

Teflon

as

below)

applicable

requiring

Tool)

hoses)

to

that

the

AND

OVERHAUL,

On

Condition

dn

i=ot;dit’ion’

a

"ON

replaced

REPLACEMENT

MAINTENANCE

1000

See

On

2000Hours 2000Hours

or

500Hours

500

OnCondition

7

CONDITION"

or

performance

SCHEDULE

Hours

M20-52A

SI

M20-92A

Condition

6

years

Hours

or

years

Engine

overhauled

reveals

condition.

OR

to

(refer

(referto

data)

NOTE

Items

REPLACE

whichever

O/H,

be

to

are

when

unserviceable

an

inspection

LlME

repaired,

UMITS

repairdata)

repair/inspection

occurs

or

first.

Vacuum Filters-Vacuum

Filters

Other

All

SDeedbrakes

All

Vacuum

Stand-by

E.L.’T.

Oxygen

Regulator

Instruments

Gyro

Components

OtherComponentF;

Pump,

Vacuum

Battery

Cylinders

Wt.

Lt.

Composite

Scott

Air

Conditioning

Other

All

Avionics

Oxygen

Component~

Instruments

Garter

Filter

Pump

Electrical

Controls

Flight

Miscellaneous

Primary

Pump/Cl;tch

Steel

Cylinders

Cylinders.

Regulator

Components

(Excluding

System

Systems

Avionics)

~ee

Section

5

yrs.(O/H)

6

yrs.(O/H)

6

years-overhaul;

21-5800

100

Hours

500

Hours

500

On

Condition

On

Condition

1000Hours

Condition

On

Condition

Hours

200

Years

2

/24

years

/15

years

for

specific

On

RefertoManufacturers

or

3

years-test

Condition

or

10,000

maintenance

(CV1J4

or

Filter-

Annually

(See27-96-00)

Hrs.

500

or

[Inspsct

Hour

1

(See

Drive

Total

recharge recharge

NOTE

On

Coupling)

Use

cycles cycles

and

servicing above)

Publications

Condition)

Engine

O/H

Replace

times.

Components

5-10-00

Hydrostatic

should

be

Test

Required

Inspected

S

serviced

and

Inspection

year

intervals. NOTE

at

chart

regular

of

this

Intervals

manual.

per

the

servicing,

lubrication

end

SERVICE

OLDWILLWAYNE

AND

MAINTENANCE

MANUAL

M20S

MOONEY

AIRCRAFT

CORPORATION

5-20-00

Inspection inspection

recommended

at

following

Aircraft

considered

and

frequent

5-20-01

The

general

are

grouped

function

i.

as

of

Moving

applicable

attachment,

servicing,

condition

cracking, apparent

Metal

2.

for:

security

and/or

cracks,

The

during

corrosion

shall

3.

sealant,

corrosion,

tubular

each

Fuel,

be

inspected

kinks,

improper

Replace

Hose

systems

the

Hose

vacuum

torqued

4.

or

clamp

between

engine

clamp

to

Pipe

procedures.

SCHEDULED

CHECKS

Intervals.

the

of

ai

paragraphs.

operated

high

should

he

intervals.

INSPECTION

points

in

accordance

the

items

Parts

for:

sealing,

safetying,

of

hinges,

corrosion,

damage.

Parts

shall

of

attachment,

distortion,

and

frame

annual

or

damage.

oil

air,

and

deterioration,

bend

radius,

correct

installations

systems

shall

be

installations

Ilnes

15

Threads

Lubricate

drain

jnch’

Perform

rcraft,

intervals

NOTE

in

a

risk

cleaned

to

be

discussed,

shall

proper

adjustment,

binding,

deformation,

be

any

structure

inspection

hydraulic

as

applicable

if

any

torqued

and

pounds.

pipe

MAINTENANCE

a

25,

com

ponents

as

salt

air

for

corrosion

and

Refer

CHECK

covered

with

be

inspected

operation,

cleanliness,

inspected,

condition

fatigue

other

should

obstruction,

insecure

and

of

these

fuel

on

between

or

to

blast

on

vent

Tightening

threads

50,

outlined

environment

damage,

inspected

A%

43-4.

to

POINTS

during

the

and

tension,

excessive

and

as

cracks,

apparent

be

for

any

oil

lines

for:

cracks,

conditions

and

systems

25

inch

tubes,

lines

and

follows:

as

100´•hour

or

and

engi

in

are

af

inspection

nature

checked

security

lubrication,

travel,

wear,

other

any

applicable,

of

finish

welding

damage,

inspected

signs

and

hoses

dents,

chaffing,

installation.

exist,

hydraulic

pounds.

air

ducts,

shall

torque

the

and

be

threads

assemblies

only.

sleeves

with

Use

"Parker

threads,

to

be

installing

is

correctly

full

one

should

with

shall

stretch,

insulation;

and

cleaned

thread

to

care

only.

oil

used.

Tape.

turn

new

broken

that

of

The

the

No

or

oil,

to

be

as

any

Oxygen

compound

valves,

ne

which

th’ead first

three

compound

the

on

should

of

the

grease

Fuel,

Thread

Apply

sparingly

Engine

lubricate

Vacuum

of

Check

components.

p’ocedures

Tapered

(1)

positioned

(2)

more.

(3)

disconnected

components.

of

Bolts

5.

inspected

proper

Electrical

6´•

applicable

terminals;

insecure

Other

apparent

7.

Filters

and

inspected

would

Lines

Teflon

or

connectors,

might

compound

threads

istobe

outside

be

exercised

thread

other

or

Hydraulic,

Lube"

lubricant,

and

carefully.

Fittings

fittings

Lines

manufacturers

on

Threads

Continue

but

If

leaks

If

leaks

and

for:

Refer

torque,

for:

chaffed,

installation;

and

require

come

vacuum

and

replacement.

Use

thread

fittings,

in

must

of

used

of

the

to

compound

lubricant.

Air,

or

equivalent

omitting

Use

threaded

No

to

tighten

do

not

overrun

are

detected,

persist,

nuts

fretting,

(Figure

wiring

loose,

broken,

damage.

screens

for

contamination

only

seal

contact

be

applied

the

on

tube

prevent

or

Oil

the

only

directly

lubrication

instructions

Section

systim.

Use

Teflon

rejected;

in

critical

wear,

and

5´•2)

shall

corroded,

heat

deterioration;

shall

MIL´•T´•5542

tape

parts

with

male

coupling

flares.

the

teflon

Lines

male

on

first

aircraft

37

until

backoff.

or

tighten

the

replace

damage,

safetying.

be

and

be

removed,

on

or

oxygen.

sparingly

fitting

Extreme

contamination

tape

fittings

two

en~gine

to

engine.

is

when

for

maintenance

Threadseal

fitting

parts

areas

inspected

and

worn

or

damage

TORQUE

See

Following

VALUES

Tables.

5´•20´•00

MOONEY

OLDWILLWAYNE

AIRCRAFT

CORPORATION

M20S

SERVICE

MAINTENANCE

AND

MANUAL

FLARE

FITTING

SIZE

.3

´•4

´•5

-6

-8

´•10

-12

-16

-20 ´•24

Failure

and/or

nut

provide

The

torque

1)

2)

3)

4)

5)

NUT

of

an

Material Parent Whether Whether The

depth

TORQUE

CAUTION

threaded

bolts

assembly

value

to

of

the

material

the

screw

the

screw

of

TIGHTENING

VALUES-

MINIMUM

40

60

75

150

200.

300.

500.

fasteners

thread.

capable

be

set

screw.

(steel,

thread.

the

These

torque

due

bolt

A

of

for

a

non-ferrous

untreated

is is

or

dry

TORQUES

Tighten

values

ALUMINUM

METRIC

to

over-tightening

screwassemgld~

or

being

tightened

particular

or

lubricated.

Untreated

minimum

to

TORQUE

MAXI~IUM

65

80

125

250.

350.

500.

700

600.

FLARE

BOLTS,

size

metal

plated.

are

TUBING

FIGURE

to

of

or

plastic).

Hardware

torque

derived

INCH

NUT

can

the

screw

from

POUNDS

TORQUE

5-1

SCREWS

occur

with

bolt

is

dependent

(Black

value

a

proof

for

appropriate

oil-free

MINIMUM

30 50 70 90

155.

300

430

550.

900

NUTS

bolt

by

of

nut

load

Finish)

cadmium-plated

shank

the

without

upon:

fracture

appropriate

thread

Friction

site

as

STEEL

MAXIMUM

or

stripping

Coefficient

shown

threads.

70

90 120 150

250

400

575 750

by

class

TUBING

stripping

is

0.14

(Figure

of

intended

occurring.

5-1).

the

to

5-20-01

NOMINAL

DIAMETER

(Coarse

M3 M4

M5

M6

M7 M8 M10

M12

M14 M16

M18

M20

M22 M24 M27 M30 M33

M36 M39

Thread)

5.6

Nm/ft.lb.

0.60/0.44

1.37/1.01

2.70/1.99

4.6/3.3

7.6/5.6 11/8.1

22/16

39/28

62/45

95/70

130/95

184/135

250/184

315/232

470/346

635/468 865/637

1111/819 1440/

1062

8.8

Nm/ft.lb.

1.37/1.01

3.10/2.29

6.15/4.

10.5/7.7

17.5/12.9

26/19 51/37

89/65

141/103

215/158

295/217

420/309 570/420 725/534

1070/789

1450/ 1970/1452

2530/ 3290/2426

54

1069

1865

PROPERTY CLASS

TORQUE

Ma

10.9

Nm/ft.

1.42

1.92/

40/3.

4.

8.

65/6.

15/11 25/18.4 36/26

72/53

125/92

198/146 305/224

420/309

590/435

800/590

1020/752 1510/1113

2050/1511

2770/2042

3560/2625

4620/3407

12.9

Ib.

25 38

Nm/ft.lb.

2.

30/1.70

5.

25/3.

10.4/7.6 18/13

29/21.3

43/33 87/64

150/110

240/177

365/269 500/368

710/523

960/708

1220/899 1810/1334

2450/ 3330/2455 4280/3156

5550/4093

87

1806

SERVICE

OLDWILLWAYNE

AND

MAINTENANCE

MANUAL

M20S

MOONEY

AIRCRAFT

CORPORATION

NOMINAL

DIAMETER

(Fine

Thread)

M8x1

M10

x

M12x1.25

M14x1.5

M16x1.5

M18x1.5

M20x1.5 M22x1.5

M24x2

TIGHTENING

DIAM

ETER

(Coarse

M3 M4 M5 M6

M7

M8

M10

M12

M14

M16 M18

M20 M22

M24

M27 M30 M33

M36 M39

1.25

Thread)

TORQUES

5.6

Nm/ft.

Ib.

56/0.41

0.

1.28/0.94

2.5011.84

4.3/3.1

7.1/5.2

10.5/7.7

21/15 36/26 58/42 88/64

121/89 171/126

230/169

295/217

435/320

590/435

800/590

1030/759 13’40/

988

(METRIC

8.8

Nm/ft.lb.

27/19

52/38 95/70

150/110

225/165

325/239

460/339

610/449

780/575

Electrically

8.8

Nm/ft.

1.28/0.94

2.90/2.

5.75/4.24

9.9/7.3

16.5/12.

24/17.7

48/35 83/61

132/97

200/ 25/202 390/287

530/390

675/497 995/733

1350/995

1830/

2360/1740

3050/2249

TORQUE

Ib.

14

1

147

1349

Zinc

TABLES

PROPERTY

CLASS

TOROUE

Plated

PROPERTY

CLASS

TOROUE

CONTINUED)

10.9

Ma

Hardware

Ma

Nm/ft.lb.

38/28

73/53

135/99

210/154

315/232

460/339

640/472

860/634

1100/811

10.9

Nm/f

1.80/1.33

4.10/3.02

8.10/5.97

14/10.3 23/16.9 34/25

67/49 81/59

117/86.2

185/136

285/210

390/287 550/405

745/549

960/708

1400/1032

1900/

2580/ 3310/2441 4290/3163

Friction

I

t.

b.

1401 1902

12.9

Nm/ft.lb.

45/33

88/64

160/118

250/184

380/280

550/405

770/567

1050/774

1300/958

Coefficient

12.9

Nm/ft.

2.15/1.59

4.95/3.65

9.70/7.

16.5/12.

27/19.9

40/29

140/103 220/1

340/250

470/346 660/486 890/656 1140\840 1680/1239 2280/1681

3090/2278

3980/2935

5150/3798

0.

125

Ib.

15

1

62

NOMINAL DIAMETER

(Fine

Thread)

M8x1

M10x1.25

M12x1.25

M14x1.25

M16x1.5

M18x1.5

1.5

M20

x

M22x1.5

M24x2

METRIC

CONVERSION

8.8

Nm/ft.lb.

25/18

49/36 88/64

140/103

210/154

305/224

425/313 570/420 720/531

FACTOR:

One

Foot

One

Pound

PROPERTY

CLASS

T_OROUE

Ma

Nm(Newton

1.355818

10.9

Nm/ft.

Ib.

35/25 68/50

125/92

195/143

295/217

425/313

600/442 800/590

1000/737

Meter)=.7375

Nm

Foot

12.9

Nm/ft.lb.

42/30

82/60

150/110 235/173 350/258 510/376

720/531

960/708

1200/885

Pound;

5-20-01

MOONEY

OLDWILLWAYNE

AIRCRAFT

CORPORATION

M20S

SERVICE

AND

MAINTENANCE

MANUAL

NUT/BOLT SIZE

8-36

10-32

1/4-28

5/16-24

3/8-24

7/16-20

1/2-20

9/16-18

5/8-18 3/4-16

7/8-14

1´•14 11/8-12

11/4´•12

S

ION

TEN

BOLTS

AN()

AN365/AN310

NUTS

12´•15

20-25

50-70

100-140

160-190

450-500. 480-690.

800´•1000

1100-1300

2300-2500

2500-3000

3700´•5500

5000´•7000

9000´•11000

-type

AN/MS

STANDARD

FINE-THREAD

SHEAR´•type

AN()

AN364/AN320

NUTS

12-15

30-40

60-85

95-110

270´•300.

290-410.

480-600

600-780

1300-1500

1500- 2200-3300 8000-4200

5400-6600

BOLTS.

7-9

1800

BOLT,

NUTS

SERIES

TORQUE

SION

TEN

NASC)

AN365/AN310

11000-13000

BOLTS

NUTS

25-30

80-100

120-145 200-250 520´•630. 770-950.

1100-1300

1250´•1550 2650´•3200

3550´•4350

4500-5500 6000-7300

TABLES

´•type.

SMEAR

NAS()

´•type

BOLTS

AN364/AN320

NUTS

15-20

50-60 70-90

120-150

300´•400 450-550

650-800 750-950

1600-1900

2100´•2600

2700-3300

3600-4400

6600-8000

8-32

10´•24 1/4-20 5/16-18

3/8-16

7/16-14

1/2-13

9/16-12 5/8-11.

3/4´•10 7/8-9

Reference: Recommended

i.

2.

turn

3.

Be Run

Add

are

sure

bolt

"friction

(Units

to

"Final

12´•15

20-25

40´•50

80-90

160´•185

235-255.

400-480.

500-700. 700-900.

1150´•1600

2200-3000

Federal

Aviation

Torque

inch´•pounds)

and/or

nut

down

bolt/nut.

near

drag

Torque

Value".

(FRICTION

Values

bolt

contact

torque"

Agency

for

threads

to

DRAG

(Units

Advisory

Nut´•Bolt

are

with

the

COARSE-THREAD

7-9

12-15 25-30 48-55

95-100

140-155

240-290 300-420

420-540

700-950

1300-1800

TORQUE

are

Inch´•pounds)

Circular

combination

clean

and

washer

recommended

or

TORQUE

VALUES

No.

dry(unless

bearing

torque

REC’MD

SERIES

Figure

43.13´•lA,

Mfg.

surface

value

TORQU.E

and

from

5´•2

p.

states

118

otherwise).

check

Figure

FINAL

"friction

5-2.

This

TORQUE).

drag

value

torque"

is

required

considered

5-20-01

10

DO

NOT

REUSE

LOCKNUTS

CAUTION

IF

THEY

CAN

BE

RUN

UP

FINGER

TIGHT.

SERVICE

OLDWILLWAYNE

MAINTENANCE

AND

MANUAL

M20S

MOONEY

AIRCRAFT

CORPORATION

530-02 Aircraft

addition

the

100-hour

to

status

Regulations.

Airplane

Book,

Airworthiness

Engine

License

and

5-20-03 Prior

and/or

engine,

Then

recommended

record

engine

Flight

Propeller

Service

(if

Mooney

to

a

25

wash

perform

of

runup,

all

compression

and

abnormalities,

after

test

flight

5-20-04

one

The,

time,

inspection

condition,

the

require

including

Airplane

removal

components;

lubrication

all

should

be

maladjustment

first

the

After

operation,

recommended

1.

Visually

Inspect

operating

Inspect

exhaust

or

Inspect

scratches

Inspect

10.

Inspect

remove

of

on

evidence

and

etc.

cowling;

2.

been

operation

3.

oil

4.

installed

5.

external

to

6.

cracks,

7.

freeplay,

8.

obstructions.

9.

screws,

AIRCRAFT

examining

of

compliance

This

Manual,

Log

Certificate,

Information,

applicable),

service

ENGINE

scheduled

after

hours

down

an

engine

the

in

malfunctions

complete

check.

perform

completing

FIRST 25-hour

the

of

propeller,

Flight

of

however,

service

extensive

which

25

hours

refer

engine

inspect

cowling.

clean

and

alternate

engine

leaks.

security

engine.

fuselage,

dents.

and

windshields

scratches.

control

damage.

pitot

aircraft

service

and

annual

aircrafi

the

with

review

Aircraff

Book,

Weight

FAA

documents.

FUNCTIONAL

100-hour

installation

the

engine

runup

Airplane

and

To

a

verify

a

the

25-HOURS

inspection

a

prefiight

Manual.

all

access

it

should

requirements.

enough

might

of

to

a

paragraph

inspection.

propeller,

induction

under

air

door.

compartment

and

wing

of

damage.

systems

static

and

exterior

batteries.

INSPECTION

FILE

inspections

current

includes

Log

Registration

Aircraft

Airworthiness

or

of

and in

accord

Flight

abnormalities.

differential

correction

second

inspection.

engine,

inspection

The

panels

include

detect

to

jeopardize

or

new

spinner,

air

dusty

for

condition

and

Pay

and

windows

for

systems

for

proper,

a

Federal

inspection

Book,

Engine

Balance

Radio

CHECK

annual

or

new

engine

components.

with

Manual.

(hot

malfunctions

of

engine

INSPECTION

consists

and

runup

aircraft

as

inspection

or

disassembly

completion

The

anydmage

night

ovemauled

5-20-05

and

if

filter

conditions.

evidence

of

empennage

particular

for

binding,

for

security

cover,

review

Aviation

of

Certificate,

Record,

Station

Directives,

inspection,

ovemauled

procedure

Make

After

engine)

and

visual

of

a

general

outlined

does

inspection

safety.

engine

for

engine

aircraft

Check

of

fuel,

equipment

attention

crazing,

excessive

possible

of

bolts,

the

Log

the

not

the

has

for

in

of

a

in

of of

or

5-20-05

60-hour

The 25-hour

inspection

hours

newly

of

overhauled

inspection

filter.

and

1.

Engine.

for

A.

B.

C.

oil

Drain

Remove

and Remove

data

strainer

cartridge.

Remove

D. E.

Service

,,d

amount

F.

G.

Inspect Inspect

evidence

security.

H.

Inspect

I.

Inspect

around

J.

Inspect

cylinders,

movement,

K.

Drain

L.

connections

Visually

M.

Visually

operation

71-62-00).

N.

2´•

Propeller.

A.

Inspect

mounts

Inspect

isolator

condition,

B.

Inspect

discrepancy

Cabin.

3.

A.

Inspect

systems

B.

Inspect

operation

C.

Inspect

proper

operation,

D.

Lights

glareshield,

lights.

E.

F.

4.

Landing

A.

B.

Inspect

pump

Inspect

static

boost

attachments

inflation.

aircraft

-50-HOUR

inspection

inspection,

doors,

operating

including

(Refer

change

engine

and

plug.

and

engine

of

lubricating engine

of

leakage,

spark

cylinders

baffles

engine

and

security.

and

clean

inspect

evidence

and

alternate-air

of

engine

for

propeller

looseness,

blades

prior

for

proper

trim

travel.

and

cabin

Inspect

position,

fuel

for

proper

Inspect

installed).

(if

Gear.

tires

shock

weight.

includes

plus

panels,

time,

engine

replacement

to

frequency)

oil

sump

clean

Safety

and

replace

clean

oil

intake

looseness

plug

for

freedom

and

controls

fuel

inspect

mount

security

and/or

for

to

operation

system

and

sealing.

cabin

anti-collision

selector

operation.

oxygen

for

discs

INSPECTION

the

or

fairings.

a

new,

should

engine

suction

strainer

wire

fuel

injector

with

sump

oil.

and

elbows

for

evidence

secure

from

for

strainer.

and

of

leakage

induction

door

bolts

and

hub

oil

nicks

flight.

and

parking

and

baggage

interior,

valve,

system,

blisters,

cuts,

for

-(Repetitive)

all

requirements

necessary

After

re-manufactured,

be

given

the

of

manufacturer’s

oil

lubricating

strainer;

plug.

full-flow

the

fuel

proper

exhaust

or

damage.

and

shielding

of

overheating.

anchorage,

cracks.

full

travel,

lines

air

(refer

or

damage.

system;

firewall

far

to

oil

condition.

spinner

leakage.

cracks.

and

brake

fluid

level.

indicator

doors

instrument

and

landing

gascolator,

plumbing

wear

proper

removal

the

50-hour

a

reinstall

oil

strainer.

type,

systems

nuts

close

freedom

security

paragraph

for

general

Repair

for

damage,

and

extension

of

first

service

filter

grade,

check

Lord

any

control

free

panel,

and

proper

the

of

25

or

oil

for

fit

of

taxi

at

5-20-02

MOONEY

OLDWILLWAYNE

AIRCRAFT

CORPORATION

M20S

SERVICE

AND

MAINTENANCE

MANUAL

C.

Inspect

disc

wear,

installation.

5.

Wings.

A.

Inspect

B.

C.

D.

6.

Fuselage

A.

B.

C.

7.

See

Inspect

operation.

of

Lubricate

Inspect

proper

Lubricate

Check

bellcranks

proper

evidence

necessary.

damage,

necessary,

inspections

5-20-06

(RefertoPig.

The

100-hour

searching

for

the

exterior,

all

fuselage,

plates,

bearing

fuselage

inspection

AIC of

cover

and

to

replacements testing

when

of

components

applicable.

Directives,

applicable

Bulletins

conformance

aircraft. Recommended

requirements

EN61NE

1.

remove

engine

an

recommended

engine

and

engine

Operators

and

abnormalities,

test

after

set-up.

A.

Complete

compression rev.):

necessary.

leakage.

for

clean full-flow and

obstruction.

clean

B.

Inspect

condition

C.

Drain

oil

safety.

Inspect

suction

oil

hydraulic

warpage,

surfaces

ailerons,

for

damage

flaps

binding.

and

stabilizer,

operation

Trim

Section

and

component

-100-HOUR

ANNUAL

5-3)

(or

inspection

engine

wing,

and

locations

mating

(See

Airworthiness

Mooney

and

FAA

to

100-hour/annual

outlined

are

INSPECTION.

cowling

engine

runup

in

Manual.

the

100-hour/annual

check

and

engine

oil

and

security.

engine

screens;

filter

cartridge;

Check

Safety

brake

hydraulic

and

tips

aileron

and

proper

and

attachments

flaps,

observe

per

Cycle

controls

Empennage.

elevators,

and

controls

System

5-20-07

proper

per

for

proper

for

any

service

INSPECTION

INSPECTIONS)

annual)

of

includes

and

fairings

inspection

entire

the

engine

empennage

at

all

(including

points).

Section

is

Comply

or

Instructions.

to

be

Directives

Vendor

5-10-01)

included

with

Specification

in

the

Prior

and

propeller

compartmentdown.

in

accord

TCM

To

perform

(Ref.

gap

cooler.

verify

a

for

oil

with

Engine

correction

a

differential

TCM

or

replace

evidence

Inspect

sump;

reinstall

second

replace

crank

wire

case

oil

filter

installation.

system

fluid

for

level

damage.

attachments,

operation,

for

travel

Section

and

fin,

attachment.

Section

operation,

repetitive

guides.

is

aircraft.

thorough

compartment,

inspection

systems

wing

attach,

and

Operating

at

applicable

Notes

mandatory

Check

2A3

for

and

special

following

to

the

paragraphs:

spinner.

100

Then

hour

Maintenance

of

runup

inspection

(hot

SE

M84-15

spark

of

oil

and

remove,

and

safety.

with

new

breather

disc

or

and

proper

damage

and

5-20-07,

rudder

5-20´•07,

50

for

a

thorough,

Preparation

cleaning

removal

doors,

hinge,

empennage

and

special

this

interval,

(AD’s),

Service

aircraft

for

M20S

Model

inspection

inspection,

Wash

perform

procedure

malfunctions

and

engine

engine)

current

or

plugs,

fuel

and

fuel

hoses

inspect

Remove

cartridge

lines

pad

and

any

for

hour

limit

FAA

and

flight

oil

and

for

grade,

security

Strainer.

check and

heating

exhaust/manifold

if

manifolds

500

security

connections

if

synchronization

points

Inspect

cam

excessive

inspect

manual.

holes,

Inspect

broken

of

vacuum

and

damage

isolation

operation, housing

attachment.

Service 71-00-50.

ignition

terminals,

system

for solution

and

damaged

if

damage

cracks, belts,connections

21-58-00.

proper

slip-joints

D.

and

E.

F.

Remove

fuel

BOOST

G.

H.

Remove

Hrs).

I.

follower

J.

Inspect

deformation,

K.

damage.

L.

M.

Cablecraft

life

of

N.

O.

P.

Inspect

obstruction.

Q.

Inspect

for

R.

S.

Inspect

T.

Inspect

torque.

U.

Inspect

Refill

quantity

inspect

and

condition

Inspect

system

PUMP

Inspect

air

(SEE

Inspect

and

in

Check

for

condition,

distributor

oil

magneto

Repair

cylinders

fins.

Inspect

pumps

Inspect

and

mounts

Insped

full

travel,

swage

the

control

Inspect

information

Inspect

harness

and

for

condition

neutralize

to

evidence

area.

is

found.

Inspect

distortion

for

cracks,

fuel

and

fuel

with

air

connections

Para.

and

alternate

induction

of

inspect

"ON".

clean

oil

sump

lubricating

injector,

fuel

and

lines

mixture

ducting

for

5-20-06,1,Q,

Inspect

engine

all

systems

operation.

the

magnetos

(timing

to

clearance,

block

for

felt

for

proper

breaker

from

TCM/magneto

per

or

replace

baffles

for

accessory

hoses,

tubular

corrosion;

for

engine

at

control

lubricate

or

engine

battery

for

condition,

bumed

batteries,

Flush

exhaust

for

and

burned

baffle

firewall

security

and

proper

the

HEAD

NOTE

cables

cable.

for

IO´•550-G

cables,

chaffed

or

battery

and

battery

corrosive

system

of

leakage.

components,

sealant.

engine

inspect

corrosion.

Replaceorrepair

exhaust

and

looseness.

airconditioning

(if

installed).

exhaust

nuts,

couplings,

studs,

deformation,

with

oil.

fuel

line

noules

gascolator

and

connedions:

control

and

connections

leaks.

and

induction

air

door

all

air

system

for

engine);

lubrication,

close

and

anchorage,

fit

erosion

compartment.

secure

paint

case,

and

starter,

and

mount

all

condition.

propeller

connedion

tube

lubricated

are

DO

NOT

control

proper

cable.

set-up.

engine

electrical

secure

insulation.

mount

action,

for

Replace

muffler

stacks

bolts,

for

compressor

Reference

etc.

seals,

leaks

the

proper

connections

TCM

(Ref

strainer,

at

IDLE

Leak

engine

R8S

air

and

air

filter

for

below).

ducting

leaks.

grounding inspect

internal

cracks.

and

At

maintenance

if

required.

around

and

cracked

fittings

for

bolts

and

controls

(security)

and

REMOVE

and

wiring,

anchorage,

areas,

Inspect

areas

if

necessary.

cracks,

if

any

burned

For

damage

clamps

and

type,

SE).

reinstall

pressure

CUTOFF

in

cabin

check

exhaust

(replace

magnet

and

magneto

timing.

Inspect

remove

500

hours

cracks,

cylinders.

and

altemator,

for

security

cracks,

rubber

for

free

cable

of

security

the

for

seals

TCM

(See

Section

and

loose

and

vent

tube

blast

soda

with

looseness

or

repair

internal

areas,

installation,

SECTION

and

security.

for

all

at

for

of

5-20-06

12

SERVICE

OLDWILLWAYNE

AND

MAINTENANCE

MANUAL

M20S

MOONEY

AIRCRAFT

CORPORATION

V.

for

indication.

security

Inspect

operation,

2.

PROPELLER

A.

Remove

B.

Inspect

C.

Inspect

and

5,6.

D.

Inspect

blades

and

flight,

E.

Inspect

F.

G.

LANDING

3.

A.

Inspect

hub

Inspect

condition.

propeller

necessary

INSPECTION.

slippage

approved,

Always

Retraction

removed

B.

Inspect

misalignment,

condition

at

250

warpage

leakage,

C.

D.

E.

F.

of

hour

Inspect

(Ref.

Inspect

inspect

dents,

Inspect

engagement

Check

G.

landing landing

Jack

for

Inspect

or

H.

aircraft,

the

I.

Inspect

broken

Maximum

gear

Inspect

damage

following

nose

roll

assembly

heat

on

J.

Inspect

adjustment,

K.

Inspect

L.

Inspect

bellcranks,

distortion,

lubrication.

M.

Inspect

mounting,

and

damage.

re-install

and

condition,

INSPECTION.

spinner

securityofpropeller

hub

studs/nuts/bolts

damage.

hub

for

components

cracks

Anti-ice

spinner

fit..

GEAR

tires

excessive

if

necessary.

least

at

wheels

corrosion

seals

and

for

checks

cylinder

for

snug

and

tire(s),

run

felt

inteluals.

Cycle

andlor

brakes

Section

hydraulic

cracks

parking

and

release.

shock

assemblies.

leg

Landing

SECTION

(Ref.

recommended

as

inspections:

nose

gear

retraction

gear

pins.

allowable

is

1/32

inch

treated

nose

landing

wheel

alignment,

main

gear

landing

pivots

and

misalignment,

landing

cleanliness,

Check

motor

cowling.

proper

not

(if

Reference

nicks.

and

for

boots

and

bulkhead

3

rear

and

RETRACTION

proper

wear.

CAUTION

5

complete

after

replaced,

aircraft.

for

and

bearings;

for

disc

32-40-04).

reservoir

brake

chafing,

brake

disc

gap

(Ref.

Gear

components

cleanliness

for

tube

NOTE

towing

dent.

steering

corrosion,

cleanliness

for

gear

bearings

corrosion,

gear

and

indication

operation

opening

already

installation.

SECTION

for

Repair

security.

bulkhead.

inflation,

Replace

any

before

cracks,

bolt

and

for

lines

kinks

system

on

32-81-00)

32-82-00)

in

paragraph

bungees

damage

No

repair

gear

and

retraction

for

actuator

Check

cowl

and

removed).

for

proper

damage

and

prior

for

cracks

for

snug

fl

Use

cuts,

with

Landing

tire

has

flying

failure.

re-pack

pad

wear,

and

main

fluid

and

security.

for

and

for

on

is

hoses

and

allowed

proper

components.

mechanism

lubrication.

and

damage.

wear,

cleanliness,

for

security

of

overheating

and

brush

flap’s

position

torque,

61-00-20,

leaks,

to

ne~ct

and

between

shims

SYSTEIVI

blisters,

new,

Gear

been

the

distortion,

Inspect

bearings

and

disc

level.

proper

nose

hard

any

7-10-00,

damage.

sheared

leg

linkage,

damage,

and

wear.

for

as

of

Perform

N.

Section32-30-01.

4.

A.

seepage

B.

seepage

C.

and

water

D.

E.

selection,

OFF

F.

sediment,

G.

mounting,

condition

and

Check

(1)

"T

ing"

High reading

H.

security

electrical

i.

security,

fuel

needed

5.

EXTERIOR

A.

damage,

FUEL

Inspect

and

Drain

is

Inspect

position.

Inspect

water

Inspect

into

boost

(mixture

Inspect

of connections.

Inspect

and

filler

(Reference

Inspect

SYSTEM

evident.

contamination.

smooth

adequate

electric

line

operation

mounting

cap

loose

oilcans(stretched

deteriorated

B.

crazing,

installation.

C.

damage,

cracks,

freedom

weight

D.

Check

wear.

E.

loose

cracks,

attachment

operation,

F.

corrosion,

G.

lubrication 52-11-00

H.

paint.

Inspect

scratches,

Inspect

loose

condition

of

operation,

attachment.

Inspect

for

Inspect

or

popped

condition

of

manually

Inspect

nicks,

Inspect

and

for

rigging

Inspect

compartment

condition

i.

Inspect

J.

Inspect

K.

Inspect

condition

and

ventilating

and

for

adjustment

security,

condition and

condition

33-43-00

location.

landing

INSPECTION.

fuel

tank

stain.

tank

and

fuel

tank

fuel-tank

fuel

selector

operation

gascolator

and

other

electric

of

fuel

condition

boost

fuel

and

wiring

boost

withacalibrated

full

RICH,

quantity

and

tank

O’rings

Section

INSPECTION.

fuselage

and

skins),

windshields

condition

wings,

or

flaps,

popped

of

free-play,

Speed

proper

cabin

Brake

operation.

empennage

rivets,

and

balance

and

door

dents,

hinge

cabin

proper

procedures.

baggage

for

damage,

to

door

operation

of

cargo

restraintsniedowns.

system

landing

proper

Decals/Placards

operational

gear

exterior

inspect

drains

vents

pump

should

for

valve

and

for

leakage;

contamination.

pump

pressure,

electrical

for

result

throttle-IDLE).

gauges

condition

filler

port

of

servicing

for

condition

28-00-01).

exterior

surfaces

popped

scratches,

and

of

sealant,

and

ailerons

rivets,

attaching

cartridges

for

free-play,

lubrication

weights

electrically.

door

and

security

door

lock

engagement.

door

corrosion,

frame

of

door

drain

and

taxi

adjustme

procedures.

evidence

for

tank

leakage,

obstruction.

for

leakage

any

inspect

for

leaks,

switch

connections.

proper

fuel

pressure

in

transmitters

and

of

for

cleanliness,

placards.

and

rivets,

windows

and

dents,

points,

travel,

for

(Ref.

27-96-01)

corrosion,

dents,

of

and

frames

and

mechanism

and

warpage,

and

locking

for

line

lights

nt.

condition

for

check

interior

sediment,

proper

security

operation,

operation

15

a

wiring

replace

for

corrosion,

cracks

for

security

for

corrosion,

scratches,

lubrication,

and

damage

scratches,

hinge

freedom

for

lubrication.

See

door

mechanism

obstruction.

for

See

per

fuel

of

when

tank

when

for

sump

gauge.

P.S.I.

for

and

cap

Inspect

dents,

and

cracks,

balance

damage,

points,

damage,

for

Section

baggage

hinge

seals,

security,

Section

and

5-20-06

in

of

by

if

of

or

of

13

MOONEY

OLDWILLWAYNE

AIRCRAFT

CORPORATION

M20S

SERVICE

AND

MAINTENANCE

MANUAL

L.

Inspect

extremities

and

trailing

high

voltage/am

6.

INTERIOR

A.

cleanliness

condition structure mechanism

brackets

Inspect

B.

security

C.

restrict

35

location.

panels

and

D.

Inspect

this

of

E.

7.

INTERNAL

A.

B.

safetying,

control

Open

and

Inspect

(interior

adequately

C.

Inspect

D.

damage

\(Reference

specific

E.

F.

G.

and

Inspect

and

Inspect

evidence

cracks,

lines

chaffing

Seal

H.

corrosion,

I.

Inspect

hardware

8.

FLIGHT

A.

travel,

Inspect

proper

mounting,

surface

movement.

All

inspected

B.

Inspect

lubrication,

all

bearings,

downspn’ng

mounting

C.

Inspect

lubrication,

static

wicks,

(vertical

edges

and

operation

for

lubrication.

Inspect

for

cleanliness,

of

attachment,

Inspect

movements.

O~gen

S

8

M

Inspect

inspection

fairings

wing

and

ABS

side

accomplish

forward

Inspect

(interior

Mooney

procedures

wing

of

damage

corrosion.

electrical

air

ducts

and

de-bonding.

all

receptacles

environment

Inspect

and

evidence

empennage

for

corrosion. CONTROL

control

rigging,

proper

movement

control

flight

to

are

elevator

rigging,

pivots,

eyes,

and

proper

aileron

rigging,

exterior

wing

8

hon’zontal),

for

signs

damage.

INSPECTION.

seats,

seat

mounting

cracks,

safety

for

belts,

loose

system

manual.

Decals/Placards

INSPECTION.

as

required.

attaching

evidence

panels/carpet

this

side

tubular

side

panels

Service

required

ribs

and

wing

spars

for

security,

NOTE

with

wing

interior

of

INSPECTION.

column

free-play,

lubrication

with

CAUTION

components

that

verify

free

of

system

travel,

bellcranks,&

cable

pulley

relation

system

travel,

for

signs

antennas,

tips,

of

burned/charred

tracks,

security.

of

position

deformation,

hamess

condition,

equipment,

(if

installed)

doors

bolts

of

damage

and

will

inspection).

of

firewall

structure

will

Bulletin

annually).

and

stringers

corrosion.

for

wiring,

fuel,

damage,

and

plugs

Dow

Coming

for

fuel

leakage.

attachment

and

proper

relation

all

moisture

obstructions.

for

stop

adjustment,

and

to

control

for

adjustment,

stop

of

lightning

and

Inspect

locks.

latch

etc.

for

remove

for

require

for

require

damage,

oil

outside

foreign

control

binding,

direction

to

should

damage,

hinges

fittings,

movement.

damage,

empennage

propeller

or

upholstery

seats

Inspect

corrosion

and

attaching

operation

that

CHAPTER

per

condition

proper

and

corrosion

removal

damage.

corrosion

removal).

M20-208A

for

cracks

distortion,

and

hydraulic

interference,

cabin

#4.

material,

brackets

wheels

security

of

control

be

drain

holes

corrosion,

condition

wear

security

corrosion,

condition

strikes.

tips

other

for for

seat

and

might

and

access

torque

and

for

and

for

full

control

wheel

of

on

of

to

of

security

D.

E.

guide

F.

All

with

bellcranks,

Inspect

and

relation

wheel

Inspect

proper

trim

threads

Check

for

position

control

the

rigging,

of

travel.

adjustment,

joints

blocks

27-42-00

n’gging,

push-pull

and

aircraft

hinges,

bolt

lubrication,

pivots

proper

movement

"OSe

a"d

rigging,

universal

actuator and

SECTION maintenance.

tubes

flap

actuator,

bellcranks lubn’cation.

7)

Some

wrapped

ShowS

Trim

Y9265

signs

poiyurethane

tubes,

abrading

MAX.

TUBE

diameter

9.

condition

filter

Check

lights

reduction.

INSTRUMENT/AVIONICS

A.

Inspect

and

B.

Clean

on

vacuum

C.

Inspect

operation

or

vacuum

D.

Inspect

indication,range

indicator

marks,

E.

markings,

and

security

Inspect

compensation,

discoloration.

and

after

any

Degaussing

F.

Inspect

G.

Inspect

structure

H.

Inspect

will

Instruction

proper

and

markers.

of

shock

compass

Se"ice

markings,

freedom reference

condition

with

8

security.

and

proper

rudder

rod-end

to

toe-brake

stabilizer

control

for

flap

condition

bearings,

control

free-play

for

lubrication,

for

looseness

for

system

wheel

travel,

indicator

for

tubes,

hinges

pivots

rigging

inspections

jacked

and

landing

elevator

wrapped.

VVEAR-.0O7

proper

and

security

Swing

tubular

not

synchronization

and

Avionics

trim

at

bulkhead

of

wear,

without

bulkhead

all

instrument

connections.

inspect

regulator.

vacuum

of

gage.

all

instruments

and

cracked

of

installation.

compass

new

equipment

structure

compensate

M20-95.

altimeter

pointer

flight

panel

mounts,

condition

tape,

See

regulator

high-and

of

Equipment

and

relation

movement.

pedals

trim

control

shaft

and

Electric

for

rigging

and

stop

proper

flap

for

corrosion,

NOTE

and

gear

NOTE

tubes

penetrations.

re-wrap

tape

which

grommet

SE

in.

wall

wiring

vacuum

limit

markings,

or

mounting,

within

for

scale

readings,

of

for

freedom

of

ground

rod

end

control

to

for

damage,

of

hinges,

bolt

link

and

proper

system

stop

for

smooth

good

linkage

excessive

or

Trim

System

actuator,

adjustment.

operation.

rods,

should

leveled

retracted.

have

poly

tube

with

(1/2

tape

show

should

M20-185.

thickness

INSPECTION.

and

filter.

at

vacuum

low-vacuum

for

proper

loose

glass,

for

proper

liquid

annual

at

has

been

be

may

100.

error,

barometric

security

from

straps.

for

proper

bearings,

movement.

corrosion,

bellcranks,

security

Check

nuts

rudder

for

security

proper

operation,

working

for

corrosion,

weal:

bearing

push/pull

Check

Inspect

interconnects,

security,

be

made

Section

(Per

tape

If

tape

2"

wide

overlap).

signs

be

.014

or

plumbing

Replace

garter

manifold.

warning

pointel:

condition

slippage

lighting,

leakage

inspection

installed.

necessary

See

Mooney

discolored

setting

scale

of

mounting,

interference

operation

link

and

free

and

order,

See

and

of

in.

for

of

and

if

knob

with

5-20-06

14

SERVICE

OLDWILLWAYNE

i.

Inspect

obvious

lines

security

leaks.

J.

for

K.

damage

Inspect

of

Inspect

aerodynamic

for

lines

attachment.

attemate

freedom

for

10.

ELECTRICAL

Check

A.

B.

Check

C.

lighter.

D.

Check

E.

Checkoperation

Check

lights.

dropouts.

F.

G.

H.

Check

only)

Check

duration

MAINTENANCE

AND

Avionics

defects,

or

head

pitot

cracks,

bends,

static

dents,

attachment.

static

smoothness

cracks,

Drain

system

pressure

of

valve

movement.

FUNCTIONAL

operation operationoflanding

operation

rheostat

operation

observing

by

operation

Antennas,

for

kinks,

Drain

ports

at

port

dents,

and

source

of

navigation

of

anticollision

of

travel

for

of

pitot

ammeter

of

cluster

of

fuel

MANUAL

wiring,

obstruction;

port

proper

system

for

installations.

kinks,

inspect

located

TEST.

dome

instrument

dimming

head

gauge,

gauges.

bend

and

obstruction

and

for

on

lights.

taxi

lights.

lights

lights,

needle

shielding

radius

inspect

security

leaks.

flight

and

without

heater

flucuation,

for

inspect

and

for

and

Inspect

Check

panel

cigar

placard

any

(short

M20S

of

MOONEY

Check

i.

switch.

J.

solenoid.

K.

(See (See

L.

Section

Check

During

operation

24-36-00

32-00-00).

post

setting/operation

Check

M.

Push

switch

illumination fluctuation

N.

Inspect

proper

covered

attachment

Flight

malfunctions aircraft

V~ng

between

installation

11.

MISCELLANEOUS/OPTIONAL

A.

12~

POST

test

log

access

Component

"ON",

during

Inspect

and

INSPECTION

the

book.

model

locations

operation

(BLUE

batteries,

any

obvious

and

covers

year

of

inspection

of

stall

warning

of

observe

light).

action

cycle

connection

corrosion

other

paragraphs

damage

aircraft

abnormalities.

may

aircraft.

remain

AIRCRAFT

annunciator

ignition

landing

32-60-00)

"Prop

prop

Observe

of

and

installed

FLIGHT

to

verify

Make

vary

basically

CORPORATION

light

switch,

gear

and

flight,

horn.

De-ice"

de-ice

timer.

3

battery

cleanliness.

EQUIPMENT

for

proper

malfunctions.

or

TEST.

correction

proper

to

unchanged.

press-to-test

and

position

warning

check

installed).

(if

annunciator

ammeter

areas

equipment

operation,

entries

some

degree

starter

lights

horn

proper

of

for for

for

not

all

in

5-20-07

ITEM

NUMBER

1

2

Access

See

No

periodic

use

Change

Inspect

Service

REFERENCE

covers

ITEM

Flight

Vacuum

Control Control

Engine

Vacuum

last

page

Aeroshell

garter

instrument

Stand-by

Letter

ACCESS

DESCRIPTION

Instruments

Vacuum

Turn

Rod

Universal

Bellcranks

of

lubricant

22,

filter

No.

FIGURE

riveted

in

COVER

place

Regulator

Coordinator

Filters--Replaceat

System

Column

End

Adjustments:

Bearing

Bearings

Joints

Cowling

Pumps

section

on

Mobil

on

filters

Vacuum

for

Avionics

28

vacuum

at

Pump

lubrication

or

500

34)

FOR

LOCATION

production

5-3

during

IDENTIFICATION,

Ball

symbol

Products

MIL-G-81322

regulator

hours,

drive

#102000-2.

ONLY.

every

clean

coupling

NOTE

legend.

100

every

OF

THE

need

LUBRICATION

If

necessary

hours.

100

hours.

200

hours.

FOLLOWING

removed

be

not

AND

LUBRrCATION

SYMBOL"

\y

W

C

0

Q

to

(Refer

COMPONENTS

for

SERVICE

relubricate,

to

Airborne

routine

GUIDE

inspections.

INTERVAL

(HRS)

500

100

100 100

100

500

5-20-07

15

MOONEY

OLDWILLWAYNE

AIRCRAFT

CORPORATION

M20S

SERVICE

AND

MAINTENANCE

MANUAL

ACCESS

23

7

COVER

1

FIGURE

IDENTIFICATION,

5-3

LUBRICATION

SERVICE

GUIDE

I

1

2

L

3

L

4

29

13

30

10

11

32

12

14

I’

14

’I

6

7

L

5

18

28

13

10

12

I

I I I

L

9

L

8

31

12

11

32

r

o

0

27

19

o

000

oooo

27

000

C)

Q

o

ooo,.

00

000

o

0

27

17

c

o

15616

19

27 27

27

20

21

22

5-20´•07

16

CI

7

25

33

24

---~J

1

26

SMR5-3

SERVICE

OLDWILLWAYNE

AND

MAINTENANCE

MANUAL

M20S

MOONEY

AIRCRAFT

CORPORATION

ITEM

No.

3

4

5

6

7

DESCRIPTION

ITEM

Gear

Nose

Retraction

Bellcranks

Bungees

Gear

Door

Gear

Main

Retraction

Bellcranks

Bungees

Gear

Door

Electric

Elevator

Gear Gear

Control Bellcranks

Batteri

es

Stabilizer

Universal

Guide

Hydraulic Oxygen,

Elevator

Stabilizer

Variable

Tail

High

Control

Bellcranhs

Downspring

Strobe

Empennage

Stabilizer

Grease

Tube

Rod

Grease

Tube

Rod

Actuator Actuator

Rudder

Tube

Trim

Joints

Blocks

Reservoir

Pressure

Rudder

Tube

Trim

Jack

Light

Attach

Trim

Fittings

Rod

End

Bearings

End

Bearings

Fittings

End

Rod

End

Bearings

Gear

Ball

Box"

Screw.

Contr~[s:

Rod

End

Bearings

Control

Shaft:

Fittings

Controls:

End

Rod

Bearings

Screw/Actuator

System

Power

Points

Attach

Supply

Point

Brgs’

LUBRICATION.

SYMBOL"

Q

\y

\y.

yl

Q

\y

C. C.

\V

ZZ

yl.

C~.

P

A

\y.

.O

\y.

0.

Li.

INTERVAL

(HRS)

100

100 100 100

50

100

50

AR

1000

100 100

50 50

100 100

100 100 100

100

8

9

10

12 13 14

15

11

Elevator

Control

Elevator

Control

Aileron

Aiieron

Control

Controls: Control Bellcranks

Aileron

Main

Control

Gear

WingPoints

Control Stabilizer

Indicator

Stabilizer

Tube

Rudder

Rod

Tube

Rudder

Tube

Rod

Tube

Rod

Tube

Retraction

Guide

Screw

Trim

Adjustment

Chain

Trim

controls:

End

Controls:

End

Guide

End

Guide

Blocks

Point

Bearings

Blocks

Bearings

Blocks

Stops

Gear

y,

W.

y,

Q.

100

100 100

100

C.

0

100

100 100

100

5´•20´•07

17

MOONEY

OLDWILLWAYNE

AIRCRAFT

CORPORATION

M20S

SERVICE

AND

MAINTENANCE

MANUAL

ITEM

No.

16

17

18

19.

20.

21

22

23 24

DESCRIPTION

ITEM

Elevator

Control Bellcranks

Guide

Flap

Electric

Gascolator

Control

NLGr Rudder

Rudder-Aileron

Hyd.

Aileron

Outboard

Baggage

Cabin

Engine

Radios

Engine

Oil

Wheels

Wheel

Tube

Blocks

Indicator

Flap

Boost

Systems:

Tube Yoke

Steering

Pedal

Brake

Control

Hinges

Latches. Lock

Seals

Hold

Open

Door:

Hinges

Latches. Lock

Seals

Hold-Open

Instruments

Controls

Stick,

Dip

8(

Bea

Brake

Shock

Pressure

Guide

Discs

Rudde;

Rod

Cable

Actuator

Controls:

End

Pump

Rod

End

(Lower

Link

Rod

Cross

Shaft

Bungee

Cylinder

Tube

Flap

Stops

Compartment

arm:

Arm.

Oil

Filler

Brakes:

rings

Plates

Pins

Bearings

Gear

Ball

Bearings

Section)

End

Pedal

Rod

End

Door:

Tube

Anchor

Box

Screw

Brgs.

Linkage

Brgs

Bolts

LUBRICATION.

SYMBOL"

C.

C

R

8.

C

\y.

C

5.

C

C.

Q.

C.

a. b.

C.

a.

W.

V

yl

Q

INTERVAL

(HRS)

100 100 100

100

500

100

50

100

100 100

100

100 100

100 100 100

100

100 100 100

100

AR

250

50

25

26

27 28

5´•20-07

18

Elevator Nose

Wheel

Shock

Control

Exhaust

Wheel:

Bea

Surface

Assy

Rudder

Discs

ri

ngs

Hinges

Control

Stops

Q.

Q

C.

a.

100

250

50 100 100

SERVICE

OLDWILLWAYNE

MAINTENANCE

AND

MANUAL

M20S

MOONEY

AIRCRAFT

CORPORATION

29.

30

31

32

33

34.

SYMBOL

C

n.

p

5

\V

c

0

b

Q

ii

V

Air

Induction

Cabin Remote

Heat

Strobelight

ELT

(Batteries)

ELT

ANTENNA

MIL.

SPEC.

MIL´•L-7870

MIL-G´•81322 MIL-L-3545 MIL´•H-5606

MIL´•G-23827

Filter

Shroud

Compass

Power

NO.

(MIL;27j30)

Ducts

Flux

Supply(Wing)

(UNDER

LUBRICATION

Valve

DORSAL

FIN)

SYMBOL

a. a

Q

Q Q.

LEGEND

Low

Temperature

Grease

(High

Hydraulic

Graphite

Powdered

Teflon

Stick

Q

Spray

Lubricant

Equivalent)

Aeroshell

(On

Grease

jackscrew

Actuator

Lubriplate

Molybdenum

Permissible)

Seal

Dressing

Inspect

Tape,

Tetrafluoroethylene

Permacel

New

Brunswick,

TCM

Spec.

DESCRIPTION

Oil

Purpose)

Temperature)

Fluid

/Red)

MIL-G´•3278

Graphite

(Tri-Flow)

(Door

NO.

and

Bearing

630AA

Tape

(10~

Corp.,

NJ

MHS´•24(

(GeneraJ

Grease

or

Ease

7

inside

Housing)

by

Disulfide

100

AR

or

Equivalent

or

Volume

Mixture

Above

Below

30

Deg

30

Deg

Mooney

be

changed,

For

Aircraft

M20S

F

Ambient,

F

Ambient,

aircraft

after

are

S.L. S.L.

delivered

hours

25

S/N

or

30-0001

Viscosity

with

after

aircraft,

Requirements

the

oil

Specification

ON

both

NOTE

proper

consumption

It

is

mineral

SAE

break-in

has

MHS-24~

recommended

additive

40

30

MIL-C-6529,

oil;

stabilized,

SAE

or

to

oil.

15W-50

SAE

20W-30

to

use

multiviscosity

Type

oil

conforming

II.

This

oil

in

to

should

TCM

these

5-20´•07

19

MOONEY

OLDWILLWAYNE

AIRCRAFT

CORPORATION

M20R

SERVICE

MAINTENANCE

AND

MANUAL

BLANK

5-20-07

20

Mooney M20S 1998 Maintance Manual

Specifications and Main Features

Frequently Asked Questions

User Manual

warning

GENERAL

instruments