Cessna 172 Series 1996 Manuale utente

Cessna

Textron

Company

TEMPORARY

REVISION

NUMBER

5-1

DATED

NOVEMBER 2001

MANUAL TITLE

Model

172

Series

1996 And On

Maintenance

Manual

MANUAL

NUMBER

PAPER

COPY

172RMM06

MANUAL

NUMBER

AEROFICHE

172RMM06AF

TEMPORARY

REVISION NUMBER

172RMM06TR5-1

MANUAL

DATE

December

1996

REVISION

NUMBER

DATE 18

August

2001

This

Temporary Revision

consists

the following pages, which

affect

and

replace

existing

pages

the

paper

copy

manual

and

supersede

aerofiche

information.

CHAPTER/

SECTION/

AEROFICHE

SUBJECT

PAGE

FICHE/FRAME

5-11-00

1/B14

5-11-00

1/B15

5-11-00

1/B16

REASON

FOR

TEMPORARY

REVISION

Add

Dry

Vacuum Pump and Vacuum

Pump

Coupling

the Component

Time Limits

Table.

FILING INSTRUCTIONS

FOR

THIS TEMPORARY

REVISION

For

Paper

Publications,

file this

cover

sheet

behind the

publication's

title

page to

identify

inclusion

the

temporary

revision

the

manual.

Insert the

new

pages

the publication

the appropriate

locations

and

remove

and

discard

the

superseded

pages.

For

Aerofiche Publications,

draw

line, with

permanent

red

ink

marker,

through

any

aerofiche

frame

(page)

affected

the

temporary

revision.

This

will

visual identifier that

the

information

the

frame

(page)

longer

valid

and

the

temporary

revision

should

referenced.

For

"added"

pages

temporary

revision,

draw

vertical

line

between

the

applicable

frames.

Line

should

wide enough

show

the edges

the pages.

Temporary

revisions should

collected

and

maintained

ina

notebook

or binder

near

the

aerofiche

library

for quick

reference.

2001

CESSNA AIRCRAFT

COMPANY

WICHITA,

KANSAS,

USA

CESSNA

AIRCRAFT

COMPANY

MODEL

172

MAINTENANCE

MANUAL

COMPONENT

TIME

LIMITS

General

Most

components

listed

throughout

Chapter

should

inspected

detailed elsewhere

this

chapter

and

repaired, overhauled

replaced

required.

Some

components,

however,

have

time

life

limit

associated

with

them,

and must

overhauled or replaced

before

the

specified

time

limit.

NOTE:

The

terms

overhaul

and

replacement

used

within

this

section

are

defined

follows:

Overhaul

Item

may

overhauled

defined

FAR

43.2

can

replaced.

Replacement

Item

must

replaced

with

new item

serviceable

item

that

within

its

service

life

and

time

limits

has

been

rebuilt

defined

FAR

43.2.

This section

(5-11-00)

provides

list

items

which must

overhauled or

replaced

specific time

limits.

Table

lists

those

items

which

Cessna

has

mandated

must

overhauled or replaced

specific

time

limits.

Table 2

lists

component

time

limits which

have

been

established

outside supplier

their

product.

addition

these

time limits,

the

components

listed

herein

are

also

inspected

regular

time

intervals

set

forth

Inspection

Time

Intervals,

and

may

require

overhaul/replacement

before

their

time

limit

reached based

service

usage

and

inspection

results.

Cessna-Mandated

Replacement

Time

Limits

The following

component

time

limits

have

been

established

The

Cessna Aircraft

Company.

Table

Cessna-Mandated

Replacement

Time

Limits

CHAPTER

COMPONENT

PART

NUMBER

REPLACEMENT

OVERHAUL

TIME

Restraint

System,

504516-401-8013

years

Pilot

Left

Hand/Right

Hand

Auto

Adjust.

Restraint

System,

504851-401-8013

years

Pilot

Left

Hand/Right

Hand

Manual

Adjust.

Restraint

System,

504516-403-8013

years

Aft

Bench Left

Hand/Right

Hand

Auto

Adjust.

Restraint

System,

504851-403-8013

years

Aft

Bench Left

Hand/Right

Hand

Manual

Adjust.

Restraint

Assy,

2000031-09-201

years

Pilot

Seat

Restraint

Assy,

2000031-10-201

years

Copilot

Seat

Restraint

Assy, 2000031-11-201

years

Right Rear

Seat

Restraint

Assy,

2000031-12-201

years

Left

Rear Seat

172RMM06 Temporary

Revision Number

5-1

Nov

1/2001

5-11-00

Page

Aug 18/2001

CESSNA AIRCRAFT

COMPANY

MODEL

172

MAINTENANCE

MANUAL

Table

Cessna-Mandated

Replacement

Time

Limits (continued)

CHAPTER

COMPONENT

PART

NUMBER

REPLACEMENT

OVERHAUL

TIME

Trim

Tab

Actuator

1260074-1

1,000

hours

YES

years,

whichever

comes

first.

Dry

Vacuum

Pump

Various

Note

37 Vacuum Pump 350

Note

Coupling

Gyro

Filter

C294502-0201

600

Hours

Regulator

Valve

B3-5-1

600 Hours

Filter

Engine Various

years or

engine

Compartment

overhaul,

whichever

Flexible

Fluid

comes

first

(Note

1).

Carrying

Teflon

Hoses

(Cessna

Installed) Except

Drain

Hoses

Engine

Various On

Condition

Compartment

Drain

Hoses

Engine

Flexible

Various

Note

Hoses

(Textron

Lycoming Installed)

Air

Filter

172R

CA3559

100

hours

Air

Filter-172R

and

P198281

500

hours

172S

Mixture

and

Throttle

Refer

Illustrated

engine

TBO

Cables

Parts

Catalog

for

specific

numbers.

Starter, Engine

31B22207

engine

TBO

YES

Supplier

Established

Replacement Time

Limits

The

following

component

time limits

have

been

established

specific

suppliers

and

are

reproduced

as follows:

Table

Supplier

Established

Replacement

Time

Limits

CHAPTER COMPONENT

PART

NUMBER

REPLACEMENT

OVERHAUL

TIME

Pointer

ELT

Battery

2020

NOTE

37 Vacuum

Manifold 1H5-25

NOTE

Slick

Magnetos

4371

NOTE

YES

172RMM06

Temporary

Revision

Number

5-1

Nov

1/2001

5-11-00

Page

Aug

18/2001

CESSNA AIRCRAFT

COMPANY

MODEL

172

MAINTENANCE

MANUAL

Table

Supplier

Established

Replacement

Time

Limits

(continued)

CHAPTER COMPONENT

PART

NUMBER

REPLACEMENT

OVERHAUL

TIME

Engine

IO-360-L2A

NOTE

YES

Engine

Oil

Filter CH48110

NOTE

NOTES:

Note

(This

life

limit

not

intended

allow

flexible fluid carrying

teflon

hoses

deteriorated

or damaged

condition

to remain

service.) Replace engine

compartment

flexible

fluid

carry

teflon

hoses (Cessna

installed only)

every

ten

years or

engine

overhaul,

whichever occurs first.

This

does

not

include

drain

hoses.

Hoses which

are beyond

these

limits

and are

in a

serviceable

condition,

must

placed

order immediately

and

then

replaced within

days after

receiving

the

new

hose

from

Cessna.

Note

Refer

latest

Textron

Lycoming Engine

Service

Bulletins.

Note

Refer

FAR

91.207

for

battery

replacement

time

limits.

Note

Refer to

Airborne Air

Fuel

Product

Reference

Memo

No.

39 or

latest revision

for

replacement

time

limits.

Note

Refer to

Slick Service

Bulletin SB2-80C

or latest

revision

for time limits.

Note

Refer

Textron/Lycoming

Service

Instruction

S.I.

1009AJ or

latest revision

for

time

limits.

Note

Referto

Textron/Lycoming

Service

Instructions

S.I.

1492

S.I.

1267C, and

Service

Bulletin

480C.

Note

Replace

the

engine driven

dry

vacuum

pump

coupling

years

per

the

pump

manufacturer's

recommended

inspection

and

replacement

interval,

whichever

occurs

first.

Note

Replace the engine driven dry vacuum

pump

not

equipped

with

wear

indicator

every

500

hours

operating,

replace

according

to the

vacuum

pump

manufacturer's

recommened

inspection

and

replacement

interval,

whichever

occurs

first.

For

vacuum

pump

equipped

with

wear indicator,

replace

according

the

vacuum

pump

manufacturer's

recommended

inspection

and

replacement

interval.

172RMM06

Temporary

Revision

Number

5-1

Nov

1/2001

5-11-00

Page

Aug

18/2001

Cessna

Textron

Company

TEMPORARY

REVISION

NUMBER

61-1

DATED

NOVEMBER

2001

MANUAL TITLE

Model

172

Series

1996 And

Maintenance

Manual

MANUAL

NUMBER

PAPER

COPY

172RMM06

MANUAL

NUMBER

AEROFICHE

172RMM06AF

TEMPORARY

REVISION NUMBER 172RMM06TR61-1

MANUAL

DATE

December

1996 REVISION NUMBER

DATE

August

2001

This

Temporary Revision

consists

the following

pages,

which

affect

and

replace

existing pages

the

paper

copy

manual

and

supersede aerofiche

information.

CHAPTER/

SECTION/

AEROFICHE

SUBJECT

PAGE

FICHE/FRAME

61-10-00

201

4/C12

61-10-00

202

4/C13

REASON

FOR

TEMPORARY

REVISION

Propeller

bolt

torque

value.

FILING

INSTRUCTIONS

FOR

THIS

TEMPORARY

REVISION

For

Paper

Publications,

file

this

cover

sheet

behind

the

publication's title

page to

identify inclusion

of the

temporary

revision

the

manual.

Insert the

new

pages

the

publication

the

appropriate

locations

and remove and

discard

the

superseded

pages.

For

Aerofiche

Publications,

draw

line,

with

permanent

red

ink

marker,

through

any

aerofiche

frame

(page) affected

the

temporary

revision.

This

will

visual identifier that

the

information

the

frame

(page)

longer

valid

and the

temporary

revision

should

referenced.

For "added"

pages

temporary

revision,

draw

vertical

line

between the

applicable

frames.

Line

should

wide

enough

show

the edges

the

pages. Temporary

revisions should

collected

and

maintained

notebook

or binder

near the

aerofiche library

for

quick

reference.

2001

CESSNA AIRCRAFT

COMPANY

WICHITA,

KANSAS,

USA

CESSNA AIRCRAFT

COMPANY

MODEL

172

MAINTENANCE

MANUAL

PROPELLER

MAINTENANCE

PRACTICES

Description

and

Operation

The

airplane

equipped

with

two bladed,

fixed

pitch metal

propeller.

Maintenance

practices

consist

propeller/spinner

removal and

installation.

For

information

beyond

the

scope

this

section,

refer

the

applicable

McCauley

Service

Manual.

Propeller

and

Spinner

Removal/nstallation

Remove

Propeller

and

Spinner

(Refer

Figure

201).

WARNING:

EXERCISE CARE

WHEN

WORKING

WITH

THE

PROPELLER.

ENSURE

MAGNETO SWITCH

THE

OFF

POSITION

BEFORE

TURNING

PROPELLER.

(1)

Remove

screws

securing

spinner

bulkheads.

Remove

spinner

and

cut

safety

wire

from

propeller

mounting

bolts.

(2)

Remove mounting

bolts

and

remove

forward

bulkhead,

propeller,

aft

bulkhead

and

spacer

from

crankshaft.

(3)

starter

ring

gear

removed,

loosen

alternator

adjusting

arm and

slip

alternator

belt

off

starter

ring

gear

before removing

gear.

NOTE:

Remove

cowling

and

nosecap

for

access.

Refer

Chapter

71,

Cowling

Maintenance

Practices.

Install

Propeller

and

Spinner

(Refer

Figure

201).

(1) If

starter

ring

gear

was

removed,

clean the

mating

surfaces

the

ring

gear

and

crankshaft before

reassembly.

NOTE:

Ensure

that

"O"

identification

mark

starter

ring

gear

and

"0"

identification

mark

crankshaft flange

overlap.

Starter

ring

gear

must

located correctly

crankshaft

assure proper

alignment

the

timing marks

the

ring

gear.

(2)

Clean mating

surfaces

and

assemble the

spacer,

propeller

and

bulkheads

crankshaft.

Assemble

ensuring that

the serial number stamped

the

side

the

spacer

lines

with

either

the

propeller

blades.

NOTE:

not

necessary

align

the

spacer

serial

number

with

specific

blade. However,

the

spacer

and

propeller

have been

balanced

pair

and

must

reinstalled

together.

(3)

Secure

propellerassembly

using

propeller

bolts and

washers.

Tighten

bolts

crossing pattern

660-780 inch-pounds

(55-65

foot-pounds), safety

wire

and

install

spinner.

(4)

After securing

spinner

the

bulkheads,

check spinner

to aft

bulkhead

clearance.

(a) If

not

removed, remove

upper

cowling

and

upper nosecap.

Refer

Chapter

71,

Cowling

Maintenance

Practices.

(b)

Using a

0.03

inch

feeler

gauge

insert

gauge between

spinner

and aft

bulkhead

ensure

the

gap

0.03

inches

less.

NOTE:

gauge

not

available,

fabricate

gauge

from

phenolic,

aluminum or

steel

that

0.5

inches

wide

0.03

inches

thick

and 2.0

inches

long.

(c)

Replacement

the

Aft

Bulkhead

will

required

gap

than 0.03 inches.

(d)

Adjust alternator

belt tension.

Refer

to Chapter

24,

Alternator

Maintenance

Practices.

(e)

Reinstall

nosecap

and

cowling.

Refer

Chapter

71,

Cowling

Maintenance Practices.

172RMM06

Temporary

Revision Number

61-1

Nov

15/2001

61-10-00

Page

201

Aug

18/2001

CESSNA AIRCRAFT

COMPANY

MODEL

172

MAINTENANCE

MANUAL

B1786

~~~~~~~~~~A ~~~SPACER

DOWEL

byN \ \\ />

( |AFT

BULKHEAD

ASSEMBLY

PROPELLER

FORWARD

BULKHEAD

ASSEMBLY

DETAIL

0510T1007

Propeller

and

Spinner

Installation

Figure

201

(Sheet

172RMM06 Temporary

Revision

Number

61-1

Nov

15/2001

61-10-00

Page

202

Aug

18/2001

Cessna

Textron

Company

Maintenance

Manual

1996

MODEL

172

SERIES

REVISION

THE

BASIC MANUAL PROVIDES

ADDITIONAL

INFORMATION

NECESSARY TO

MAINTAIN

THE

AIRPLANE

AND

INCORPORATES

TEMPORARY

REVISIONS 172RMM06

TR5-1

AND

TR61-1.

)

Member

GAMA

FAA

APPROVAL HAS BEEN

OBTAINED

TECHNICAL

DATA

THIS

PUBLICATION

THAT

AFFECTS

AIRPLANE TYPE

DESIGN.

CESSNA AIRCRAFT

WICHITA,

KANSAS,

172RMM07

REVISION

FEBRUARY

2002

CESSNA

AIRCRAFT

COMPANY

MODEL

172

MAINTENANCE

MANUAL

LIST

EFFECTIVE

PAGES

CHAPTER-SECTION-SUBJECT

PAGE DATE

Introduction

List of

Effective

Pages

Feb

15/2002

Record of

Revisions

Service

Bulletin

List

Feb

15/2002

Feb

15/2002

Feb

15/2002

Feb

15/2002

Introduction

Feb

15/2002

Feb

15/2002

Feb

15/2002

Feb

15/2002

Feb

15/2002

Feb

15/2002

List

Revisions

Added

Feb

15/2002

List

Chapters

Feb

15/2002

INTRODUCTION

LIST

OF EFFECTIVE

PAGES

Page

Feb

15/2002

CESSNA

AIRCRAFT

COMPANY

MODEL

172

MAINTENANCE

MANUAL

RECORD OF

REVISIONS

REVISION DATE

DATE

PAGE

REVISION

DATE

PAGE

NUMBER

INSERTED

REMOVED NUMBER NUMBER

INSERTED

REMOVED NUMBER

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