Cessna 150 STANDARD User manual

150

SERIES

1969

THRU

1976

SERVICE

MANUAL

0971

C3-13-RAND-1600-7175

LATEST

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JULY

1972

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3 15

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1975

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NOTE:

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portion

the

text

affected

the

changes

indicated

vertical

line

the

outer

margins

the

page.

Changes

illustrations

are

indicated

miniature

pointing

hands.

Dates

issue

for

original

and

changed

pages

are:

Original.

. 1

July

1972

Change

June

1973

Change

July

1974

Change

June

1975

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NUMBER

PAGES IN THIS

PUBLICATION

IS 346, CONSISTING

THE

FOLLOWING-

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Upon

receipt

the

second

and

subsequent

changes

this

book,

personnel

responsible

for

maintaining

this

publication

current

status

should

ascertain

that

all

changes

have

been

received

and

incorporated

•

The

asterisk

indicates

pages

changed.

added

deleted

the

current

change.

Change

TABLE

CONTENTS

SECTION

Page

GENERAL

DESCRIPTION

. . . . . . . . . . .

.........

1-1

2 GROUND HANDLING, SERVICING, LUBRICATION AND INSPECTION 2-1

FUSELAGE

....

3-1

4 WINGS AND

EMPENNAGE

4-1

5 LANDING GEAR AND BRAKES 5-1

AILERON

CONTROL

SYSTEM 6-1

7 WING

FLAP

CONTROL

SYSTEM 7-1

ELEVATOR

CONTROL

SYSTEM 8-1

ELEVATOR

TRIM

TAB

CONTROL

SYSTEM 9-1

RUDDER

CONTROL

SYSTEM . 10-1

ENGINE

11-1

FUEL

SYSTEM 12-1

PROPELLER.

13-1

UTILITY

SYSTEMS 14-1 •

INSTRUMENTS AND INSTRUMENT

SYSTEMS.

15-1

LEC

TRICAL

SYSTEMS . .

.......

16-1

ELECTRONIC

SYSTEMS

(DELETED)

(See

page

iii)

STRUCTURAL

REPAffi

18-1

PAINTING

....

19-1

WffiING DIAGRAMS 20-1

Change

CROSS

REFERENCE

LISTING

POPULAR

NAME VS. MODEL NUMBERS

AND

SERIALS

All

aircraft,

regardless

manufacturer,

are

certificated

under

model

number

designations.

However,

popular

names

are

often

used

for

marketing

purposes.

provide

consistent

method

referring

the

various

aircraft,

model

numbers

will

used

this

publication

unless

names

are

required

differentiate

between

versions

the

same

basic

model.

The

following

table

provides

cross

reference

listing

popular

name

vs.

model

numbers.

MODEL SERIALS

POPULAR

NAME YEAR MODEL BEGINNING ENDING

150 STANDARD 1969

150J

15069309 15071128

150 TRAINER,

1970 150K 15071129 15072003

150 COMMUTER 1971

150L

15072004 15072628

1972

150L

15072629 15073661

1973

150L

15073662 15074850

1974

150L

15074851 15075781

150 STANDARD 1975 150M 15075782 15077005

150

COMMUTER

150 COMMUTER II

150 COMMUTER 1976 150M 15077006

150 COMMUTER II

REIMS 150 1969

F150J

F15000390

F15000529

REIMS/CESSNA

F150

1970

F150K

F15000530 F15000658

1971

F150L

F15000659

F15000738

1972

F150L

F15000739

F15000863

1973

F150L

F15000864

F15001013

1974

F150L

F15001014

F15001143

REIMS/CESSNA

F150

1975

F150M

F15001144 F15001248

REIMS/CESSNA

F150

COM-

1976

F150M

F15001249

MUTER

150 AEROBAT 1970 A150K A1500001 A1500226

1971 A150L A1500227 A1500276

1972 A150L A1500277 A1500339

1973 A150L A1500340 A1500430

1974 A150L A1500431 A1500523

1975 A150M A1500524 A1500609

1976 A150M

A1500610

REIMS/CESSNA

F150

AEROBAT 1970 FA150K FA1500001 FA1500081

1971

FA150L

FA1500082 FA1500120

1972

FA150L

FA1500121

FA1500166

1973

FA150L

FA1500167 FA1500211

1974

FA150L

FA1500212 FA1500261

1975 FA150M FA1500262 FA1500281

1976 FA150M FA1500282

Change

FOREWORD

This

manual

contains

factory-recommended

procedures

and

in-

structions

for

ground

handling,

servicing,

and

maintaining

Cessna

Model

150-Series

aircraft.

This

includes

the

Models

150,

Reims

150,

Reims/Cessna

F150, 150

Aerobat,

and

Reims/Cessna

F150

Aerobat.

The

Reims

versions

the

Model 150

identical

the

Model 150

except

that

powered

by a

200-A

Rolls

Royce

en-

gine.

Besides

serving

reference

for

the

experienced

mechanic,

this

book

also

covers

step-

by-

step

procedures

for

the

less

experi-

enced

man.

This

manual

should

kept

a handy

place

for

ready

reference.

properly

used,

will

better

enable

the

mechanic

maintain

Cessna

150-Series

aircraft

and

thereby

establish

repu-

tation

for

reliable

service.

The

information

this

manual

based

data

available

the

time

publication,

and

supplemented

and

kept

current

service

letters

and

service

news

letters

published

Cessna

Aircraft

Com-

pany.

These

are

sent

all

Cessna

Dealers

that

they

have

the

latest

authoritative

recommendations

for

servicing

Cessna

aircraft.

Therefore,

recommended

that

Cessna

owners

utilize

the

know-

ledge

and

experience

the

factory-trained

Dealer

Service

Organi-

zation.

addition

the

information

this

Service

Manual,

group

vendor

publications

available

from

the

Cessna

Service

Parts

Center,

which

describe

complete

disassembly,

overhaUl, and

parts

breakdown

some

the

various

vendor

equipment

items.

list-

ing

the

available

publications

issued

periodically

service

letters.

Information

for

Nav-O-Matic

Autopilots,

Electronic

Communi-

cations,

and

Navigation

Equipment

are

not

included

this

manual.

These

manuals

are

available

from

the

Cessna

Service

Parts

Center.

iii/(iv

blank)

This page intentionally left blank.

SECTION

GENERAL

DESCRIPTION

TABLE

CONTENTS

GENERAL

DESCRIPTION

Model

150

and

Fl50-Series

Description

. . . . .

Model

A150

and

FAl50-Series

1-1.

GENERAL

DESCRIPTION.

1-2.

MODEL 150 AND

FI50-SERIES.

Page

1-1

1-3.

DESCRIPTION.

Cessna

Model

150

and

F150-

Series

aircraft,

described

this

manual,

are

high-

wing

monoplanes

all-metal,

semimonocoque

con-

struction.

These

aircraft

are

equipped

with

fixed

tricycle

landing

gear.

Through

1970

Models,

they

are

equipped

with

flat

spring-steel

main

landing

gear

struts

and

steerable

nose

gear.

Beginning

with

1971

Models,

these

aircraft

are

equipped

with

tubu-

lar

spring-steel

main

gear

struts

and

steerable

nose

gear.

The

steerable

nose

gear

equipped

with

air/hydraulic

fluid

shl

.•

strut.

Two-place

seat-

ing

standard,

and

double-width,

fold-up

auxiliary

rear

seat

may

installed

optional

equipment.

Each

Model

150 and

Fl50-Series

aircraft

equipped

with

four-cylinder,

horizontally

opposed,

air-

cooled

Continental

Rolls

Royce

engine,

driving

all-metal,

fixed-pitch

propeller.

These

aircraft

fea-

ture

"wrap

around"

rear

window

and

swept-back

fin and

rudder.

1-4.

MODEL A150

and

FAI50-SERIES.

1-5.

DESCRIPTION.

Aerobatic

Model

A150

and

Al50-Series

aircraft

are

modification

the

cur-

rently

produced

Model

150.

Structure

has

been

Description

. . . . .

Aircraft

SpeCifications

Stations

...

Torque

Values

. . . .

1-1

"beefed-up"

some

areas

order

meet

require-

ments

the

Acrobatic

Category,

FAR

Part

23. In

addition

the

"beef-up",

quick-release

cabin

doors,

two-strap

shoulder

harnesses,

and

aerobatic

paint

design

are

standard.

Only

momentary

inverted

flight

approved,

therefore

inverted

system

offered,

Removable

seat

and

back

cushions

are

provided

allow

occupants

use

either

seat-pack

back-

pack

type

parachute

during

aerobatic

maneuvers.

1-6.

AIRCRAFT

SPECIFICATIONS.

Leading

partic-

ulars

these

aircraft,

with

dimensions

based

gross

weight,

are

given

figure

1-1.

these

di-

mensions

are

used

for

constructing

hangar

com-

puting

clearances,

remember

that

such

factors

nose

gear

strut

inflation,

tire

pressures,

tire

sizes,

and

load

distribution

may

result

some

dimensions

that

are

considerably

different

from

those

listed.

1-7.

STATIONS.

Station

diagrams

are

shown

fig-

ures

1-2

and

1-3

assist

locating

equipment

when

written

description

inadequate

impractical.

1-8.

TORQUE VALUES. A

chart

recommended

nut

torque

values

shown

figure

1-4.

These

tor-

que

values

are

recommended

for

all

installation

pro-

cedures

contained

this

manual,

except

where

other

values

are

stipulated.

They

are

not

used

for

checking

tightness

installed

parts

during

service.

1-1

GROSS

WEIGHT

. . . .

FUEL

CAPACITY

Standard

Wing

(Total)

Standard

Wing

(Usable)

Long-Range

Wing

(Total)

Long-Range

Wing

(Usable)

OIL

CAPACITY

Without

External

Filter

. .

With

External

Filter

ENGINE

MODEL

(Refer

Section

for

Engine

Data)

PROPELLER

(Fixed

Pitch)

MAIN

WHEEL

TIRES

....

Pressure

.......

NOSE

WHEEL

TIRE

(Standard)

Pressure

......

NOSE

WHEEL

TIRE

(Optional) .

Pressure

. . . . . . . .

NOSE GEAR

STRUT

PRESSURE

(Strut

Extended)

WHEEL

ALIGNMENT

(Flat

Spring

Struts)

Camber

..........

Toe-In

..........

WHEEL

ALIGNMENT

(Tubular

Gear)

Camber

.•.

Toe-In

AILERON

TRAVE L

....

Down

...

WING

FLAP

TRAVEL

RUDDER

TRAVEL

(Measured

parallel

water

line)

Right

. . . . . . . . . . . . . . . .

Left

..................

RUDDER

TRAVEL

(Measured

perpendicular

hinge

line)

Right

. . . . .

Left

.....

ELEVATOR

TRAVEL

(Thru

1974) .

(Beginning

with

1975)

Down

........

ELEVATOR

TRIM

TAB

TRAVEL

.......

Down

..........

PRINCIPAL

DIMENSIONS

Wing

Span

(Conventional

Wing

Tip)

Wing

Span

(Conical-Camber

Wing

Tip)

Length

(With

Large

Spinner)

(Thru

1970)

Length

(With

Small

Spinner)

(Thru

1970)

Length

(With

Large

Spinner)

(Beginning

with

1971)

Length

(With

Small

Spinner)

(Beginning

with

1971)

Fin

Height

(Maximum

with

Nose

Gear

Depressed

and

Flashing

Beacon

Installed

Fin

(Thru

1974) . . .

Fin

Height

(Maximum

with

Nose

Gear

Depressed

and

Flashing

Beacon

Installed

Fin)

(Beginning

with

1975).

Track

Width

(Thru

1970).

. . . .

Track

Width

(Beginning

with

1971)

Tail

Span

......

BATTERY

LOCATION

.....

Figure

1-1.

Aircraft

SpeCifications

1-2

Change

1600

gal.

22.5

gal.

CONTINENTAL

0-200

Series

69"

McCAULEY

6.00

x 6,

4-Ply

Rating

psi

5.00

x 5,

4-Ply

Rating

psi

15 x

6.00

x 6,

4-Ply

Rating

psi

4°

6°

.06"

3°

5°

TUBULAR

GEAR

00"

+.16"

NON-ADJUSTABLE

20°,

+2°

_0°

14°,

+2° _0°

0°

40°

±2 °

20°

30',

+0° _2°

20°

30',

+0°

_2°

23°,

+0° _2°

23°,

+0° _2°

25°±10

23°,

+1°

_0°

15 ° ±1°

32'

8-1/2"

33'

23'

8-1/2"

23'

6-1/2"

7'7-1/4"

10'

Firewall

. (Add

for

optional

strobe

lights)

0.00

18.50

8.37

36.00

56.69 70.69

95.00

76.44

71.

49.69

Figure

1-2.

Fuselage

Stations

133.31

22.12

31.

44.12

102.00

120.00

Figure

1-3.

Wing

Stations

138.00

173.41 200.37

156.00

174.00

192.00

Change

3 1-3

RECOMMENDED

NUT

TORQUES

THE

TORQUE VALUES

STATED

ARE

POUND-INCHES,

ONLY

STEEL

NUTS ON

OIL-FREE

CADMIUM

PLATED

THREADS.

FINE

THREAD

SERIES

TENSION SHEAR

TAP

SIZE TORQUE TORQUE

STD

ALT

STD

ALT

(NOTE 1)

(NarE

(NOTE

8-36

12-15

7-9

10-32

20-25

20-28

12-15 12-19

1/4-28

50-70 50-75

30-40

30-48

5/16-24

100-140 100-150

60-85

60-106

3/8-24

160-190

160-260

95-110 95-170

7/16-20

450-500 450-560

270-300 270-390

1/2-20

480-690

480-730

290-410 290-500

9/16-18

800-1000

800-1070

480-600'

480-750

5/8-18

1100-1300

1100-1600

660-780

660-1060

3/4-16

2300-2500

2300-3350

1300-1500 1300-2200

7/8-14

2500-3000

2500-4650

1500-1800

1500-2900

1-14

3700-5500

3700-6650

2200-3300

2200-4400

1-1/8-12

5000-7000

5000-10000

3000-4200

3000-6300

1-1/4-12

9000-11000

9000-16700

5400-6600

5400-10000

COARSE

THREAD

SERIES

(NarE

8-32

12-15

7-9

10-24

20-25

12-15

1/4-20

40-50

25-30

5/16-18

80-90

48-55

3/8-16

160-185

95-100

7/16-14

235-255

140-155

1/2-13

400-480

240-290

9/16-12

500-700

300-420

5/8-11

700-900

420-540

3/4-10

1150-1600

700-950

7/8-9

2200-3000

1300-1800

1-8

3700-5000

2200-3000

1-1/8-8

5500-6500

3300-4000

1-1/4-8

6500-8000

4000-5000

NOTES

Covers

AN310, AN315, AN345, AN363, MS20365, MS21042, MS21044, MS21045

and

MS21046.

When

using

AN310

AN320

castellated

nuts

where

alignment

between

the

bolt

and

cotter

slots

not

reached

using

normal

torque

values,

use

alternate

torque

values

replace

the

nut.

Covers

AN316, AN320, MS20364

and

MS21245.

Covers

AN363, MS20365, MS21042, MS21043, MS21044, MS21045

and

MS21046.

Covers

AN340.

I~~~J)~N\

DO NOT REUSE

SELF-LOCKING

NUTS.

The

above

values

are

recommended

for

all

installation

procedures

contained

this

manual,

except

where

other

values

are

stipulated.

They

are

not

used

for

checking

tightness

installed

parts

during

service.

Figure

1-4.

Torque

Values

1-4

Change

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