Cessna SKYLANE 182P Pilot Operating Handbook

PilOT'S

PILOT'S

~

Cessna.

~ssna.

OPERATING

SKYLANE

HANDBOOK

./

D1062-13-RAND-2500-9/75

D1

062-13-RAND

THIS

REQUIRED

REQUIRED TO

BY

--2500-9175

1976

Serial

Registration

CAR

No.

HANDBOOK

TO

PART

PART 3

CESSNA

WICHIT A,

MODEL

_________

No.

INCLUDES

INCLUDES THE MATERIAL

BE

FURNISHED

BE

FURNISHED

3

AIRCRAFT

KANSAS,

______

COMPANY

182P

THE

TO

USA

_

MATERIAL THE

PILOT

THE PILOT

LIST

OF

LIST OF

EFFECTIVE

PAGES

CESSNA

MODEL

182P

INSERT

INSERT LATEST CHANGED

LIST

NOTE: This handbook

NOTE: This handbook will

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9 WHICH COVER

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through the Owner

through the Owner Follow-Up System.

you

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mediately after receipt; the handbook should

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text

margin

Dates

TOTAL

thru 1-8 0

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will

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it

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been

it

has

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or

illustration affected

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illustration affected by the

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OF

PAGES

INCLUDES THE SUPPLEMENTS PROVIDED IN SECTION

System. with

to

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the change

changed

O.

. . 29 August 1975

O.

. . 29 August 1975

IN THIS HANDBOOK

SYSTEMS

#Change

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to

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If

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your

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indicated by a vertical line in the outer

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On a changed

are:

IS

IN THE

IN THE AIRPLANE.

6-13 0

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to

Section 9 Table

to

Section 9 Table

for

LATEST

DISPOSE

to

those who subscribe

to

those who subscribe

receiving subscription service,

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be

for

operational purposes

for

operational purposes

page,

by

a vertical line in the outer

258, CONSISTING OF

258, CONSISTING

AIRPLANE.

Pages)

Optional Systems

CHANGED

PAGES.

Cessna

concerning

be

examined

examined im-

the

portion

the portion

of

OF

Aircraft

im- of

of

OF

THE

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the

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page.

CESSNA

MODEL

182P

CONGRATULATIONS

Welcome

Welcome to the ranks

to

give

to

give

flying

it,

flying

This Pilot's Operating Handbook

pleasure and

ment, operating procedures, and performance; and suggestions

urge

you

urge you

Our

Our interest in

wide, the

stands ready

THE

•

• THE CESSNA

at

important

important benefits for you, are contained in

plied

Dealers

Dealers throughout the world upon presentation

establishes

•

FACTORY

•

FACTORY

•

FACTORY

workmanship.

• A STOCK OF

• A STOCK OF GENUINE CESSNA SERVICE PARTS on hand when you

•

THE

•

AIRPLANES,

AIRPLANES, since

Catalogs,

Cessna

We

A

A current

revised frequently, and a current

revised frequently, and a current copy

your

PERFORMANCE -SPECIFICATIONS

SPEED:

Maximum

Cruise,

CRUISE:

75%

56

75%

75

Maximum

56

Maximum

75

RATE

SERVICE CEILING . . . . .

SERVICE

TAKEOFF

LANDING

STALL

MAXIMUM WEIGHT . . . . .

JlM.XIMUM WEIGHT . . . . .

STANDARD

WING LOADING:

OILCAPACITY

OF

Ground

Total

LANDING

Ground

Total

SPEED

Flaps

Skylane

MAXIMUM

Skylane

BAGGAGE ALLOWANCE

BAGGAGE

POWER

FUEL

CAPACITY:

FUEL

CAPACITY:

Standard

Long

ENGINE:

230

PROPELLER:

at

Sea

at

75%

Recommended

engine

reserve

Power

Gallons

Power

Gallons

Range

Gallons

Range

Gallons

CLIMB

CEILING . . . . .

PERFORMANCE:

Roll

Distance

PERFORMANCE:

PERFORJlM.NCE:

Roll

Distance

Up,

Down,

EMPTY

......

11

USEFUL

......

11

ALLOWANCE

LOA

DING:

LOA

DING:

Tanks

Range

Teledyne

BHP

at

BHP

at

Level

Sea

Level

Power

start,

at

(CAS):

Power

•....•

.....•

. . . . . .

. . . .

Tanks

2600

Constant

at

Lean

taxi,

at

45%

at

6500

Usable

6500

Usable

AT

. . . . . .

. . . . . . . . . . .

Power

power.

45%

power.

Ft.

Fuel

Ft.

Ft

Fuel

at

10,000

at

10,000

Fuel

at

10,000

at

10,000

Fuel

SEA

Over

50-Ft

Over

50-Ft

Over

50-Ft

Over

50-Ft

Off . . .

Off

WEIGHT:

LOAD:

..

Pounds/Sq

Pounds/HP

PoundS/HP

Total

.

....

.

Continental

RPM

Speed,

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

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

6500

Ft.

6500

Mixture

takeoff,

.

. .

...

LEVEL

..

.

..

. .

Ft

. . . . . . . . . . .

Ft

. . . . . . . . .

with

fuel

with

fuel

climb

and

climb

and

Ft

Obstacle

Diameter.

allowance

45

minutes

45

minutes

Range

Time

Range

Time

Range

Time

Range

Time

...

MODEL

.

for

CESSNA

182P

148

KNarS

148

KNOTS

144

KNarS

144

KNOTS

475 NM

3.4

HRS

3.4

HRS

670 NM

4.7

HRS

4.7

HRS

565 NM

5.1

HRS

5.1

HRS

810 NM

7.3

HRS

7.3

HRS

FPM

890

FPM

17,700

705

1350

590

1350

56

50

2950 LBS

1707 LBS

1771 LBS

1243 LBS

1179 LBS

1179

200 LBS

16.9

12.8

61

61 80 GAL.

80 GAL. 12

12

0-470-S

82 IN.

FT

KNarS

KNOTS

KNarS

KNOTS

LBS

GAL.

QTS

ii

CESSNA

MODEL

182P

TABLE

OF

CONTENTS

OF

CONTENTS

TABLE

GENERAL

LIMITATIONS

EMERGENCY

NORMAL

PERFORMANCE

WEIGHT

AIRPLANE & SYSTEMS

AIR

AIRPLANE

SUPPLEMENTS

& BALANCE/

EQUIPMENT

PLANE & SYSTEMS

DESCRIPTIONS.

SERVICE

(Optional

(Optional Systems Description

& Operating Procedures) . . . . . . . • . . 9

&

Operating

OF

..

•.

PROCEDURES

. . . .

• . . .

LIST.

HANDLING,

& MAINTENANCE .

& MAINTENANCE. • . . • . . . . 8

Systems

Procedures) • . • • • • • . • . 9

CONTENTS

.

. . . . . . . . . . . . . 6

. . . . • • . . . • . • . 6

. . .

. . . . • . . • • • 7

Description

.......

SECTION

1

2

3

4

5

7

8

iii/(iv

m/(iv

blank)

CESSNA

MODEL

182P

SECTION 1

SECTION

GENERAL

1

SECTION 1

SECTION

GENERAL

1

TABLE

Three

Introduction

Descriptive

Symbols, A bbreviations

Symbols,

OF

CONTENTS

OF

CONTENTS

View

Engine

Propeller

Fuel

Oil

Maximum

Standard

Cabin

Baggage

Specific

General

Meteorological

Engine

Airplane

Weight

...

. . .

Data

.

..

.

..•.

...

.•...

.

Certificated

Airplane

and

Entry

and

Entry

Space

Loadings.

Abbreviations

Airspeed

Power

Performance

and

Balance

and

Balance

.

Dimensions.

and

Terminology.

Terminology

Weights.

Weights

Weights.

Entry

Terminology

...

. .

.

Dimensions.

. . . . . . . . .

and

Terminology

and

Terminology

and

Terminology

Terminology.

Symbols.

. . . . .

. . . . . .

Flight

.

Planning

..........

• • . . . . • . . .

Terminology

Page

1-2

1-3

1-4

1-5

1-6

1-7

.

1-7

1-'7

1.:.7

1-1

SECTION 1

GENERAL

CESSNA

9'·04"

MODEL

MAX

.

182P

~~~r·"

L..------

11-<

----36'-0"------1

PIVOT

..£5040'

£-_---J

28"''''''::I.~-------

POINT

*

~

NOTES:

NOTES;

1.

Wing

span shown with strobe

1.

Wing

span shown with

lights installed.

liglus installed.

2.

Maximum height shown

2.

Maximum height shown with

nose gear depressed,

and nose

and flashing beacon installed.

and flashing beacon instaned.

3. Wheel base length

4.

Propeller ground clearance

4. Propeller ground clearance

is

10 7/B".

is 10 7/8".

5.

Wing

area

5.

Wing

area

6.

Minimum

6.

Minimum

(*pivot point

(*pivot

polnt

wing tip)

PIVOT POINT

*

PIVOT

POINT

strut

properly inflated

strut

property inflated

is

174

is

174

square

turning

to

outboard

is

27'.

is

2]'.

strobe

with

all

tires

all

tires

is

66

1/2".

is

66

1/2",

square feet.

feet.

radius

outboard

1-2

Figure

1-1.

Three

View

CESSNA

MODEL

INTRODUCTION

quired

mental

This

to be

to

data

182P

handbook

furnished

be

furnished

data

supplied

contains 9 sections,

to

the

pilot

to

the

by

pilot

Cessna

Cessna A ircraft

by

CAR

by

CAR

Aircraft

and

includes

and

includes

Part

3.

Company.

3.

It

the

also

SECTION 1

material

contains

GENERAL

re-

supple-

Section 1 provides

also

contains

also

contains

terminology

DESCRIPTIVE

ENGINE

Number

Engine

opposed,

displacement.

Horsepower

PROPELLER

PROPElLER

Propeller

Number

Propeller

pitch

FUEL

FUEl

definitions

commonly

of

Engines:

of

Engines:

Manufacturer:

Model

Model Type:

Number:

Type:

Normally-aspirated,

carburetor-equipped,

Rating

Manufacturer:

Model

of

Diameter,

Type:

setting

Number:

Blades:

Number:

Constant

of

basic

or

used.

DATA

1.

Teledyne

0-470-S.

and

Engine

and

Engine

McCauley

2.

Maximum:

Minimum:

speed

12.

50

and a high

12.5°

and

data

and

data

explanations

Speed: 230

2A34C203/90DCA-8.

speed

a high

information

and

information

of

Continental.

direct-drive,

six-cylinder

rated

Accessory

82

inches.

82

inches.

80. 5

inches.

80. 5

inches.

and

hydraulically

and

hydraulically

pitch

setting

pitch

setting

symbols,

rated

of

general

of

general

abbreviations,

air-cooled,

engine

BHP

at

BHP

at 2600

Division.

actuated,

of

25.00 (30

of

25.0°

with

2600

(30

with

interest.

470 cu. in.

RPM.

with

and

horizontally-

a low

inch

station).

inch

station).

It

Fuel

Grade

A

lternate

Alternate

100/130

per

gallon.

per

gallon.

100/130

4. 6

cc

per

cc

4. 6

per

When

(and

Color):

(and

Color):

fuels

Low

Lead

Low

Lead

)

Aviation

gallon.

substituting a higher

80/87

which

are

which

are

AVGAS

AVGAS (blue).

Grade

)

Minimum

also

(blue).

Fuel

approved

(Maximum

(green).

NOTE

octane

Grade

Aviation

are:

(Maximum

fuel,

lead

low

content

lead

Fuel

(red).

content

AVGA

AVGAS

(red).

of 2

S

cc

of

1-3

SECTION 1

GENERAL

100

in

Fuel

Capacity:

Fuel

Capacity:

Standard

Total

Long Range

Total

To

the

tion

OIL

Oil

Grade

Oil

Grade

MIL-L-6082

.MIL-

supply

Continue

consumption

The

sion

drained

should

less

ensure

fuel

to

(Specification):

L-6082 A viation

airplane

be

lead

contamination

lead

contamination

Tanks:

Capacity:

Capacity

Usable:

Tanks:

Capacity:

Capacity

Usable:

maximum

selector

to

prevent

Aviation

during

to

use

to

use

has

airplane

preventive

after

used

Each

56

Each

75

cross-feeding.

first

was

the

whenever

61

gallons.

61

gallons.

Tank:

gallons.

80

gallons.

80

gallons.

Tank:

gallons.

gallons,

NOTE

fuel

capacity

fuel

25

capacity

in

either

in

either

Straight

hours

NOTE

engine

25

hours

25

hours

valve

Grade

until a total

stabilized.

delivered

aircraft

first

possible

of

the

of

the

30. 5

40

and

of 50

from

engine.

gallons.

when

LEFT

Mineral

at

the

at

the

hours

the

oil.

This

of

operation.

of

operation.

since

refueling,

or

RIGHT

or

RIGHT

Oil:

first

has

factory

This

oil

MODEL

it

will

it

result

will

result

place

posi-

Use

to

Use

25-hour

accumulated

with a corro-

with a

should

replenish

to

replenish

oil

corro-

be

CESSNA

182P

change.

or

oil

or

oil

Continental

This

stabilized.

Recommended

Oil

1-4

stabilized.

SAE

50

SAE

SAE 10W30

Capacity:

Sump:

Total:

above

50

above

Multi-viscosity

mended

12

13

Motors

oil

must

oil

must

Viscosity

4°C

or

SAE 30 below

or

SAE 30 below

for

improved

for

improved

Quarts.

Quarts

Specification

be

used

be

(40°F).

oil

(if

after

used

after

For

Temperature

For

Temperature

oil

with a range

starting

oil

filter

oil

filter

MHS-24A,

first

4°C

(40°F).

4°C

(40"F).

NOTE

in

installed).

installed),

Ashless

50

hours

weather.

or

50

Range:

of SAE 10W30

cold

Dispersant

oil

consumption

oil

consumption

is

recom-

is

recom-

Oil:

has

CESSNA

MODEL

182P

SECTION 1

GENERAL

MAXIMUM

Takeoff:

Landing:

Weight

ST

AN D

STANDARD

Standard

Maximum

CABIN

2950

in

Baggage

in

Baggage

""'<>;"'5''5''

120

Baggage

note

note below.

The

areas A and

areas

maximum

AR

Empty

AND

CERTIFICATED WEIGHTS

CERTIFICATED

lbs.

Ibs.

Compartment:

Area

"A"

Area

lbs.

Ibs.

Area

below.

maximum

A and B,

D AIR PLAN E WEIG

AIRPLANE

Weight,

Weight, Skylane: 1707

Useful

ENTRY

(or

!fA!f

{or

See

note

See

note

"B"

and

!fB" and

combined

B,

hatshelf

Load,

DIMENSIONS

WEIGHTS

passenger

below.

Hatshelf-Station

combined

including

load

is

WEIGHTS

Skylane: Skylane II: 1771

Skylane

Skylane:

Skylane: 1243

Sky

lane

Skylane

II:

11:

NOTE

weight

the

is

25

HTS

17071bs.

11:

1771

12431bs. 11791bs.

1179Ibs.

on

child's

on

child's

108 to

108 to 136: 80

capacity

hatshelf,

lbs.

Ibs.

seat)-Station

136:

80

for

baggage

for

baggage

is

200

lbs.

is

82 to

82 to 108:

lbs.

See

lbs.

See

The

108:

Detailed

illustrated

BAGGAGE

Dimensions

trated

SPECIFIC

Wing

Wing Loading:

Power

in

SPACE

in

detail

in

detail

LOADINGS

Loading:

Loading: 12. 8

dimensions

Section

of

in

Section

in

Section

16.9

12. 8

AND

the

6.

lbs.

Ibs./sq.

lbs.

Ibs./hp.

of

the

of

the

ENTRY

baggage

6.

/sq. /hp.

cabin

interior

cabin

interior

DIMENSIONS

area

and

baggage

area

ft.

and

entry

door

opening

openings

are

illus-

are

illus-

are

1-5

SECTION 1

GENERAL

CESSNA

MODEL

182P

SYMBOLS,

GENERAL

KCAS

K1AS

KIAS

KTAS

Vy

M

ETEORO

METEOROLOGICAL

OAT

OA

T

ABBREVIATIONS

AIRSPEED

Knots

for

position

for

position

Knots

mosphere

Knots

indicator

Knots

ative

and

temperature.

and

temperature.

Maneuvering

use

abrupt

use

abrupt

Maximum

sible

Maximum

not

be

not

be

Never

ceeded

Stalling

Stalling Speed

the

airplane

the

airplane

Stalling

Stalling Speed

the

airplane

the

airplane

the

most

the

most

Best

greatest

Best

greatest

LOGICAL

Outside A ir

It

is

It

is

grade)

TERMINOLOGY

Calibrated

calibrated

at

Indicated

and

True

to

undisturbed

to

undisturbed

Flap

with

wing

with

wing

Structural

exceeded

Exceed

at

any

at

any

Speed

forward

Angle-of-Climb

gain

Rate-of-Climb

gain

TERM

expressed

or

degrees

or

degrees

Airspeed

and

instrument

and

instrument

airspeed

sea

level.

sea

level.

Airspeed

expressed

Airspeed

Speed

control

control travel.

Extended

flaps

except

Speed

time.

or

the

or

the

is

controllable.

is

controllable.

or

the

or

the

is

controllable

is

controllable

center

of

altitude

of

altitude

in

altitude

in

altitude

INO

Temperature

in

either

in

either

Fahrenheit.

AND

is

indicated

error

is

equal

is

equal

is

the

is

the

in

knots.

in

knots.

is

the

airspeed

is

the

air

is

travel.

is

Speed

LO

Fahrenheit.

airspeed

which

the

maximum

the

maximum

Speed

in a prescribed

in a

prescribed

Cruising

in

smooth

in

smooth

is

the

speed

the

speed

minimum

Speed

of

gravity.

of

gravity.

Speed

in a given

is

in a given

in

a given

GY

is

degrees

in

is

the

TERMINOLOGY

SYMBOLS

indicated

speed

is

Speed

steady

the

the landing

the

free

airspeed

and

expressed

and

expressed

to

KTAS

to KTAS

shown

shown on the

expressed

KCAS

corrected

speed

the

highest

the

highest

extended

is

air,

then

air,

then

limit

that

limit

that

flight

landing

speed

horizontal

speed

time.

free

air

Celsius

airspeed

corrected

at

the

configuration

which

static

(formerly

corrected

in

standard

in

standard

on

the

in

at

which

which you

speed

position.

speed

that

only

with

only

with

may

not

may

not

speed

results

distance.

results

temperature.

knots.

airspeed

knots

for

altitude

for

altitude

you

permis-

that

should

caution.

be

at

which

at

which

at

which

at

which

in

Centi-

at-

rel-

may

ex-

at

in

the

rel-

the

1-6

CESSNA

MODEL

182P

SECTION 1

GENERAL

Standard

Tempera-

ture

Pressure

Altitude

ENGINE

BHP

RPM

MP

MP Manifold

AIRPLANE

Demon-

strated

Crosswind

Velocity

Usable

Unusable

Fuel

Standard

and

decreases

and

decreases

Pressure A ltitude

when the

of

mercury

of

mercury

POWER

Brake

Revolutions

Manifold

induction

PERFORMANCE

Demonstrated

wind

during

certification

limiting.

Fuel

Usable

Fuel

Usable

Unusable

used

TERMINOLOGY

Horsepower

component

Inflight.-

Temperature

by 26C

by 26 C

barometric

(1013 mb).

Per

Pressure

system

AND

Crosswind

takeoff

Fuel

is

Fuel

and

tests.

is

the

is

for

is

the

is

the

subscale

is

the

is

the

Minute

is a pressure

and

is

and

is

expressed

FLIGHT

for

which

for

which

landing

The

fuel

available

fuel

available

the

quantity

the

quantity

15°C

at

15°C

at

each

1000

each

1000

altitude

has

power

developed

is

engine

is

engine

expressed

PLANNING

Velocity

adequate

was

actually

was

actually

value

shown

value

shown

of

sea

level

sea

level

feet

read

from

read

from

been

set

been

set

developed

speed.

measured

in

inches

in

inches

is

the

is

the

control

demonstrated

is

not

for

flight

for

flight

fuel

that

fuel

that

pressure

of

altitude.

of

altitude.

an

to

29. 92

to 29. 92

by

the

by

the

in the

in

the

of

TERMINOLOGY

velocity

of the

of

the

not

considered

planning.

can

not

can

not

altitude

altimeter

inches

engine.

engine's

mercury

of

the

of

the

airplane

during

be

safely

be

safely

(Rg).

(Hg).

cross-

during

to

be

to be

GPR

GPH

NMPG

g

WEIGHT

Reference

Datum

Station

Gallons

per

Nautical

which

fic

[is

[

is

AND

Reference

all

Station

terms-of

Per

hour.

Miles

can

be

can

engine

BALANCE

horizontal

be

power

acceleration

Datum

is a location

the

Hour

is

the

is

the

Gallon

to

is

an

along

from

amount

per

and/or

gravity.

imaginary

are

Hour

Per

expected

setting

due

TERMINOLOGY

is

distances

distance

is

the

is

the

gallon

flight

measured

the

airplane

the

airplane

the

reference

the

reference

of

fuel

of

fuel

distance

of

fuel

of

fuel

configuration.

vertical

for

(in

gallons)

(in

gallons)

(in

consumed

plane

for

balance

fuselage

datum.

consumed

nautical

at a speci-

from

purposes.

given

miles)

which

in

1-7

SECTION

SECTION 1

GENERAL

1

CESSNA

MODEL

182P

Arm

Moment

Center

Gravity

(C.

G.)

(C. G. )

C.G.

C.

G.

Arm

C.G.

Limits

Standard

Empty

Weight

Basic

Empty

Basic

Empty

Weight

Useful

Load

Gross

(Loaded)

Weight

of

Arm

is

Arm

is

the

center

the

center

Moment

its

arm.

its

arm.

this

handbook

this

handbook

the

number

the

number

Center

ment,

reference

total

Center

airplane's

total

Center

locations

given

Standard

including

oil.

Basic

weight

Useful

basic

Gross

of

would

weight

of

weight.

Empty

of

Load

empty

(Loaded)

the

horizontal

the

horizontal

of

is

the

is

the

(Moment

of

Gravity

datum

of

Gravity

individual

of

Gravity

of

Gravity

within

Empty

unusable

optional

Load

is weight.

gravity

product

to

simplify

to

simplify

digits.

is

balance

is

the

airplane.

Arm

Limits

which

Weight

equipment.

is

the

weight.

Weight

distance

(C. G. ) of

(C.

G.)

of

the

of

the

divided

found

found by

airplane.

Limits

fuel,

equipment.

difference

by

balance

)

the

point

the

point

if

suspended.

if

suspended.

by

is

the

is

the

moments

are

the

airplane

the

airplane

is

the

is

the

full

is

the

is

the

standard

is

the

is

the

by

standard

from

an

item.

of an

item.

weight

the

constant

the

constant

calculations

at

which

at

which

dividing

arm

obtained

arm

obtained

and

dividing

and

dividing

the

extreme

the

extreme

must

weight

operating

between

loaded

the

reference

the

reference

of

an

item

of

an

item

1000

an

airplane,

an

airplane,

Its

distance

Its

distance

the

total

the

total

by

by adding

the

center

be

operated

be

operated

of a standard

fluids

and

fluids

and

empty

takeoff

weight

of

empty

datum

multiplied

is

used

is

used

by

reducing

by redUCing

or

from

the

from

sum

of

airplane,

full

plus

airplane.

the

by

gravity

at

engine

and

moment

adding

sum

weight

the

to

by

in

equip-

by

the

by the

the

a

the

Maximum

Takeoff

Weight

Maximum

Landing

Weight

Tare

1-8

Maximum

for

the

for

Maximum

for

Tare

weighing

Tare

(net)

start

the

start

the

landing

the

landing

is

deducted

airplane

Takeoff

of

Landing

the

weight

the

weight

an

airplane,

an

airplane,

deducted

weight.

Weight

the

takeoff

the

takeoff

Weight

touchdown.

of

chocks,

of

chocks,

and

from

the

from

the

is

the

is

the

run.

is

the

is

the

is

included

is

included

scale

maximum

blocks,

reading

weight

stands,

in

the

in

the

to

weight

etc.

scale

obtain

approved

used

when

used

when

readings.

the

actual

the

actual

CESSNA

MODEL

182P

SECTION 2

LIMITATIONS

SECTION

LIMITATIONS

TABLE OF CONTENTS

TABLE

Introduction

irspeed

A

irspeed

Airspeed

A

irspeed

Power

Weight

Center

Maneuver

Flight

Kinds

Fuel

Placards

OF

. . . . . . . .

• . . . . . . .

Limitations

Indicator

Plant

Limitations

Plant

Limitations

Plant

Instrument

Plant

Instrument

Limits

of

Gravity

of

Gravity

Limits

Limits.

Load

Factor

Load

Factor

of

Operation

of

Operation

Limitations

. . . . . . . .

.......

CONTENTS

. . . .

Markings

. . . . . .

• . . . . .

Limits

.....

. . . .

Limits

. .

Markings

.

2

Page

2-3

2-4

2-5

2-6

2-7

2-8

2-9

2-1/{2-2

2-1/(2-2

blank)

CESSNA

MODEL

INTRODUCTION

basic

gine,

in

When

ment

as

182P

Section 2 includes

placards

standard

this

section

this

section

applicable,

are

Your

Cessna

necessary

systems

have

included

The

airspeeds

The

airspeeds

(figure

shown in

alternate

should

variations

sources

Cessna

Model

2-1)

2-2)

be

been

limitations

in

Section 5 with

static

observed

between

as

is

No.

operating

for

the

for

the

and

standard

and

standard

approved

associated

listed

the

based

source

in

associated

9.

Airspeed

to

the

Section

and

are

shown

certificated

182P.

limitations,

safe

by

by the

NafE

NarE

in

the

Airspeed

in the

Airspeed

on

Airspeed

on

Airspeed

the

normal

the

normal

is

being

is

being

allow

normal

under

instrument

Federal

with

used,

the

and

FAA

instrument

optional

Limitations

Calibration

static

airspeed

alternate

Type

operation

equipment.

the

Indicator

for

5.

of

the

airplane,

of the

airplane,

The

limitations

The

limitations

Aviation

systems

Limitations

Markings

source.

ample

margins

calibration

static

Certificate

SECTION 2

liMITATIONS

II

MIT A TIONS

markings,

data

its

included

If

or

the

No.

or

included

equip-

3A

Administration.

chart

and

en-

13

"

2-3

SECTION

LIMITATIONS

2

CESSNA

MODEL

182P

AIRSPEED

A

irspeed

A

irspeed

figure

2-1.

Never Exceed

V

Never Exceed

NE

Maximum Structural

NO

Cruising

Maneuvering Speed:

A

Maximum Flap Extended

FE

Speed:

Maximum Window Open 172

Maximum Window Open

Speed

LIMITATIONS

limitations

SPEED

Speed

2950 Pounds

2450 Pounds

1950 Pounds

To

100

To

100

-

400 Flaps

100

-

400 Flaps

Speed

Flaps

and

their

operational

their

operational

KCAS

KIAS

KIAS REMARKS

172 176 Do

141

139

109 110 Do

109 110

138

172 176 Do

141

99 100 control movements above

99

100

89

89 89

140

95

176 Do

significance

not

exceed this

not

exceed this

any operation.

Do

not

exceed this

Do

not

exceed this

except in smooth air,

then only

Do

not

make

not

make

control movements above

this

89

95

speed.

this

Do

not

exceed these

not

exceed these

Do

with

the given flap settings.

with

the given flap settings.

not

exceed this

not

exceed this

windows open.

REMARKS

with

are

caution.

full

or

full

or

shown

speed

and

abrupt

speeds

speed

in

with

in

AIRSPEED

Airspeed

shown

2-4

in

figure

Figure

INDICATOR

indicator

2-2.

markings

2-1.

Airspeed

MARKINGS

and

their

Limitations

color

code

significance

are

CESSNA

MODEL

MARKING

White Arc

White

Green Arc

Green

Yellow Arc

Red

182P

Arc

Line

VALUE

KIAS

VALUE

OR RANGE

OR

RANGE

48 - 95

141

-

53

53 -141

- 176

141

- 176 Operations must

176

Full Flap Operating

limit

landing configuration. Upper

is

flaps extended.

Normal Operating

limit

flaps retracted.

mum structural cruising

Operations must caution

caution

Maximum

SIGNIFICANCE

maximum weight VSo in

is

maximum weight VSo in

permissible

maximum

speed

maximum weight

is

maximum weight

Upper

be

only in smooth air.

and

only in smooth air.

for

speed

for

permissible with

Range.

SECTION 2

LIMITATIONS

LIMIT A TIONS

Lower

Range.

conducted

conducted with

Lower

Range.

limit

with

Lower

with

Vs

with

maxi-

is

limit

is

maxi-

speed.

with

all operations.

POWER

Engine

Oil

Propeller

Manufacturer:

Model

Operating

Maximum

Pressure,

Figure

PLANT

Number:

Limits

Power:

Engine

Cylinder

Oil

Minimum: Maximum:

Manufacturer:

Model

Diameter,

Blade

Speed:

Temperature:

Minimum: Maximum:

Number:

Maximum: Minimum:

Angle

Airspeed

2-2.

2-2. A irspeed

LIMITATIONS

Teledyne

0-470-S.

for

230

230 BHP.

Speed:

Head

McCauley

Maximum: Minimum:

at

30

Continental.

116°C

psi.

82

80.5

80. 5 Station,

and

116°C

Accessory

inches.

Station,

Takeoff

BHP.

2600 RPM.

Temperature:

psi.

10

psi.

100

McCauley

2A34C203/90DCA-8.

Inch

30

Inch

Indicator

Continuous

238°C (460°F).

(240°F).

inches.

Low:

High:

Markings

Mar

kings

Operations:

Division.

12.5°.

25.0°.

2-5

SECTION 2

llMITA

LIMITA TIONS

TIONS

CESSNA

MODEL

182P

POWER

Power

are

shown

are

shown

INSTRUMENT

Tachometer

Manifold

Oil Temperature - - -

Oil Temperature - --

Cylinder

Temperature

Pressure

Oil

Pressure

Carburetor

Temperature

PLANT

plant

in

figure

in

figure

Pressure

Head

Air

Figure

instrument

2-3.

INSTRUMENT

markings

RED LINE GREEN ARC

RED

LINE

MINIMUM

LIMIT

- - -

- - - 2200 -

- - -

-- 15-23

- - -

--

10

psi

10

psi

- - - - - -

- -

Power

and

their

and

their

GREEN ARC

NORMAL

NORMAL CAUTION

OPERATING RANGE

OPERATING

2200 -

2450

RPM

2450

RPM

15-23 in.

Hg

in.

Hg

100° -240°F

240°F

100°

200° -460°F

460°F

200°

30-60

psi

30-60

psi

- - -

Plant

Instrument

Plant

Instrument

MARKINGS

color

code

color

code

YELLOW ARC

CAUTION

RANGE

- - -

-

- - -

- -

-- -

- - -

_15°

to

-15°

5°C

to

5°C

Markings

significance

RED LINE

MAXIMUM

LIMIT

2600

RPM

2600

RPM

- - -

--

240°F

460°F

100

psi

100

psi

- - -

-

WEIGHT

Maximum

Baggage

Station

Baggage

Station

The

areas A and

maximum

2-6

LIMITS

Takeoff

Landing

Weight

Area

82

Area

108

maximum

Weight:

in

Baggage

in

Baggage

"A"

''A''

82

to

"B"

fiB"

108

to

hatshelf

(or

108:

and

136:

combined

B,

including

B,

including

2950

lbs.

2950 Ibs.

2950

lbs.

2950

lbs.

Compartment:

passenger

120

lbs.

120

lbs.

Hatshelf

80

load

lbs.

NOTE

weight

the

is

25

-

on

child's

on

child's

See

note

See

note

- See

note

See

note

capacity

hatshelf,

lbs.

Ibs.

seat)

below.

for

is

200

is

200

-

baggage

lbs.

The

CESSNA

MODEL

182P

SECTION 2

LIMIT A TIONS

LIMITATIONS

CENTER OF

Center

Reference

MANEUVER

category

These

whip

of

of bank

FLIGHT

Flight

of

Forward:

line

Aft:

Aft: 48. 5

This

airplane

is

include

stalls),

bank

is

Aerobatic

Load

*

Flaps

*Flaps

*The

the

structure

the

structure

Gravity

33. 0

variation

48. 5

inches

Datum:

airplane

applicable

any

lazy

not

more

not

more

maneuvers,

LOAD

Factors

Up: +3.

Up:

Down:

design

GRAVITY

Range:

33.0

inches

to 39. 5

to

aft

Front

LIMITS

is

certificated

is

certificated

to

maneuvers

eights,

than

maneuvers,

FACTOR

8g,

+3.8g,

+2.0g

load

factors

load

factors

meets

aft

of

aft

of

inches

39. 5

inches

of

datum

of

datum

face

of

face

of

aircraft

incidental

chandelles,

0

60

•

60°.

including

-1.

52g

-1.

52g

are

or

exceeds

or

exceeds

LIMITS

datum

fire

firewall.

in

at

aft

of

aft

of

at

all

weights.

at

all

weights.

wall.

in

the

normal

the

normal

intended

150% of the

150% of

to

and

spins,

LIMITS

the

design

2250 Ibs.

2250

lbs.

datum

category.

for

non-aerobatic

for

non-aerobatic

normal

steep

turns

steep

turns

are

not

are

not

above,

loads.

or

less,

or

less,

at

2950 Ibs.

at

2950

flying,

in

in which

approved.

and

with

lbs.

The

operations.

stalls

which

in

all

in

all

straight

normal

(except

the

angle

the

angle

cases,

KINDS

The

VFR

and/or

VFR

and/or

quired

ence

flects

ance.

instrumentation

to

equipment

eqUipment

Flight

OF

airplane

IFR

types

into

into known

OPERATION

is

equipped

is

equipped

operations.

and

flight

operations

installed

icing

and

at

of

flight

known

for

day

for

day

FAR

equipment

eqUipment

on the

at

on the

the

time

the

time

conditions

LIMITS

VFR

and

VFR

Part

and

91

for

these

for

these

operating

of

Airworthiness

of

Airworthiness

is

prohibited.

is

prohibited.

may

be

may

establishes

be

operations.

limitations

equipped

the

minimum

the

minimum

The

placard

Certificate

for

refer-

night

re-

issu-

re-

2-7

SECTION 2

LIMITA TIONS

CESSNA

MODEL

182P

FUEL

2

Standard

2

Standard

Total

Usable

Unusable

2 Long

Total

Usable

Unusable

Fuel

Grade

Fuel

Grade

Alternate

100/130

per

100/130

4. 6 cc

LIMITATIONS

Tanks:

Fuel:

Fuel

Range

Fuel:

Fuel

To

the

tion

Takeoff

the

(and

gallon.

per

ensure

61

(all

Fuel:

Tanks:

80

(all

Fuel:

fuel

selector

fuel

selector

to

prevent

to

prevent

and

BOTH

Color):

Calor):

fuels

Low

Lead

Low

Lead

)

Aviation

gallon.

30.5

U.

S.

U.

S.

flight

5.0

40

U.

S.

U.

S.

flight

5.0

maximum

land

position.

which

Grade

)

U.

S.

gallons

U.

S.

gallons

gallons.

conditions):

U.

S.

gallons.

U.

S.

gallons.

U.

S.

gallons

U.

S.

gallons

gallons.

conditions):

U.

S.

gallons.

U.

S.

gallons.

NOTE

fuel

capacity

fuel

in

the

Minimum

also

Fuel

capacity

either

NOTE

fuel

approved

(green).

valve

cross-feeding.

with

80/87

are

AVGAS (blue).

each.

56

U.

56

U.

each.

75

U.

75

U.

when

LEFT

selector

Grade

(Maximum

S.

gallons.

S.

gallons.

S.

gallons.

S.

gallons.

or

valve

Aviation

are:

refueling,

RIGHT

handle

lead

content

lead

content

lead

place

posi-

Fuel

content

in

(red).

of 2

cc

of

2-8

substituting a higher

When

substituting a higher

When

100

in

should

less

be

lead

contamination

lead

contamination

used

NOTE

whenever

of

of the

octane

possible

the

fuel,

since

engine.

low

lead

it

will

it

will

AVGAS

result

CESSNA

MODEL

PLACARDS

individual

shown on the

182P

The

following

The

following

placards.

(1)

In

(1)

In

This

airplane

This

airplane

in

compliance

in

compliance

form

of

form

of

--------

full

example

placards,

information

view

of

view

of

below,

must

with

the

pilot:

the

pilot:

below,

markings,

will

be

operated

be

operated

the

operating

the

operating

markings,

is

displayed

is

displayed

(The

''DAY-NIGHT-VFR-IFR''

(The

"DA

vary

as

vary

as

as a normal

limitations

and

manuals.

and

manuals.

MAXIMUMS

in

the

form

of

in

the

form

Y-NIGHT-VFR-IFR"

the

airplane

the

airplane

category

as

-------

of

is

stated

composite

equipped.

equipped.)

airplane

air

in

SECTION 2

LIMIT A TIONS

LIMITATIONS

or

entry,

)

plane

the

MANEUVERING

GROSS WEIGHT . .

FLIGHT LOAD

FLIGHT

No Altitude known icing certified of

(2)

On

(2)

On

(3) On the

(3)

On the

LOAD

No

acrobatic

Altitude known certified of

original

control

Control

Off

Left

Both

Both - 56

Right

loss

icing

conditions

for

airworthiness

lock:

lock -remove

fuel

selector

fuel

selector

- 29

- 56 takeoff

takeoff

- 29

SPEED

..

FACTOR

maneuvers,

in a

stall

in a stall

the

following

the

following

DA

Y - NIGHT -

DA

Y - NIGHT -

valve

gal.

Level

gal.

Level

gal.

All

gal.

All

and

gal.

Level

gal.

Level

(IAS) . . . .

(IAS)

• . . .

.

....

.

....

. .

Flaps

..

including

recovery

prohibited.

flight

certificate:

before

plate

flight

flight only,

flight

landing.

flight

Up .

Flaps

Up .

Flaps

Down.

Flaps

Down.

- 160 ft.

operations

VFR -IFR

starting

(standard

only.

attitudes.

only.

spins,

This

. 110

.

. 2950 Ibs.

+3.8,

+2.0

approved.

Flight

airplane

as

engine.

tanks):

Both

on

Both

on

110

of

for

knots

-1.

-1. 52

into

is

date

52

2-9

SECTION

SECTION 2

LIMITA TION S

LIMITATIONS

2

On

the

On the

fuel

selector

fuel

selector

Off

Left

- 37

Left

- 37

Both

- 75

Both

- 75

takeoff

Right

Right -37

takeoff

- 37

gal.

valve

Level

All

and

Level

plate

flight

attitudes.

flight

attitudes.

landing.

flight

(long

only.

range

Both

Both on

tanks):

on

for

CESSNA

MODEL

182P

(4) On

(5) On

0°

10°

the

baggage

the

baggage

FORWARD

BAGGAGE

BAGGAGE INCLUDING 25 LBS MAXIMUM IN

BAGGAGE INCLUDING

FOR

FOR ADDITIONAL

flap

control

flap

control

to

20° -T.O.

to

20° -

to

20° -FULL

to

20° -

door:

OF

BAGGAGE DOOR LATCH

OF

120 POUNDS MAXIMUM

AND/OR

AFT

OF

AFT

OF

BAGGAGE

BAGGAGE WALL HATSHELF

MAXIMUM 200 POUNDS COMBINED

ADDITIONAL LOADING INSTRUCTIONS

WEIGHT AND BALANCE DATA

indicator:

T.O.

FULL

BAGGAGE DOOR LATCH

AUXILIARY PASSENGER

BAGGAGE DOOR

BAGGAGE DOOR LATCH

80 POUNDS MAXIMUM

25

WALL

WADING

(Takeoff

and

140

and

140

detent

(Indices

color

code

color

code

mechanical

LATCH

LBS MAXIMUM IN

HATSHELF

INSTRUCTIONS SEE

range

kt

callout;

kt

calloutj

at

10°.

at

10°.)

at

these

at

these

and

detent

with

)

positions

pOSitions

95

blue

also,

kt

at

blue

SEE

col

color

mechanical

with

callout;

calloutj

10°

and

10°

and

or

with

also,

20°

code

white

. )

• )

2-10

(6)

Forward

Service

gasoline.

gaSOline.

of

fuel

of

fuel

this

Capacity

tank

airplane

filler

with

30.5

30. 5

cap

80/87

gal.

(standard

minimum

tanks):

aviation

grade

CESSNA

MODEL

182P

Forward

of

fuel

tank

filler

cap

(long

range

tanks):

SECTION

SECTION 2

LJMITATIONS

LIMITA TIONS

2

Service

gasoline.

(7) On

(7)

On

Adjacent

(8)

Adjacent

aft

this

panel

to

Capacity

airplane

of

over-voltage

with

40.0

baggage

OXYGEN

HIGH VOLTAGE

minimum

80/87

gal.

compartment

light:

minimum

REFILL

(all

aviation

models

grade

with

oxygen):

oxygen);

2-11/(2-12

blank}

blank)

CESSNA

MODEL

MODEL 182P

182P

SECTION 3

EMERGENCY PROCEDURES

SECTION 3

SECTION

EMERGENCY

TABLE OF

Introduction

Airspeeds

Engine

Forced

Fires

Icing

Landing With a

Electrical

Engine

Forced

Failures

Engine

Landings

Landings . . . . . . . . . . . . . .

Emergency

Precautionary

Ditching

.........

..........

During

Engine

Electrical

Cabin

Wing

Fire

..........

. . . . . . . . . . .

Inadvertent

Static

Suspected).

Over-

Ammeter

Failure

Landings

CONTENTS

. . . . . . . . . . .

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

For

Emergency

For

Emergency

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

Failure

......

Start

start

Fire

Source

Power

Voltage

During

Immediately

During

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

Landings

Landings Without Engine

Landing

Landing With Engine

......

On

On Ground .

In

Flight

In

Flight

Fire

In

.....

......

Icing

Blockage

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

Flat

Main

Supply

Light

Shows

Operation

OPERATIONAL CHECKLISTS

Takeoff

Flight

Without Engine

With

.

Ground

In

Encounter

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

Main

Discharge

.

• .

Flight

.

(Erroneous

Tire.

System

Illuminates.

AMPLIFIED

3

PROCEDURES

. . . • . . .

Run.

After

. . . . . .

. . . . • .

Engine

. . . . . .

Malfunctions

......

. . .

Takeoff

Power

Instrument

. . . .

PROCEDURES

.

Reading

Page

3-3

3-4

3-5

3-6

3-7

3-8

3-1

SECTION 3

EMERGENCY PROCEDURES

CESSNA

MODEL

182P

TABLE

Landing

Landing Without

Fires

Emergency

Flight

Spins

Rough

Rough Engine

Electrical

OF

CONTENTS

OF

CONTENTS

Without

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

Executing

Emergency

Recovery

In

Icing

In

Icing

Static

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

Engine

Carburetor

Spark

Magneto

Magneto Malfunction . . . . . . . .

Low

Oil

Low

Oil

Excessive

Insufficient

Elevator

Operation

A 1800 Turn

Descent

From a Spiral

Conditions . . . . . . .

Source

Plug

Power

Blocked.

Operation

Icing

Fouling

Malfunction

Pressure

Supply

Rate

Control

In

Clouds

In Clouds (Vacuum

In

Clouds.

In Clouds

Through

Dive

. . . . . .

Or

Loss

Or

Loss

. .

..

. . . . . . . . .

. . . . . . . .

. . . . . . . . .

System

Of

Charge.

Of

Charge

Of

Charge

Of

Charge

.

(Continued)

. . . . . . . . . . .

(Vacuum

Clouds

Of

Malfunctions

. . . . . .

.

..

.

Power

System

Failure)

Failure).

Page

3-10

.

3-10

3-11

3-12

3-13

3-14

3-15

3-2

CESSNA

MODEL

INTRODUCTION

emergencies

malfunctions

tenance

or

ed

basic

as

with

182P

Section 3 provides

section 3 provides

eliminated

weather

guidelines

necessary

the

are

ELT

is

practiced.

that

may

are

extremely

are

extremely

by

careful

by

careful

encountered.

described

to

correct

to

correct

and

other

may

other

checklist

occur.

Enroute

flight

flight planning

the

optional

and

Emergencies

rare

if

weather

planning

However,

in

this

in

this

problem.

systems

amplified

if

proper

section

EMERGENCY

EMERGENCY PROCEDURES

procedures

caused

preflight

emergencies

and

good

and

good

should

Emergency

can

be found

can

be found

by

judgement

an

emergency

an

emergency

be

considered

procedures

by

inspections

considered

PROCEDURES

for

air

plane

airplane

can

be

can

be

when

in

Section

in

Section 9.

SECTION

SECTION 3

coping

coping with

or

engine

or

engine

and

main-

minimized

unexpect-

arise

the

arise

the

and

applied

and

applied

associated

9.

3

with

main-

AIRSPEEDS FOR EMERGENCY

AIRSPEEDS FOR EMERGENCY OPERATION

Engine

Maneuvering

Maximum

Precautionary

Landing

Landing Without Engine

ENGINE

Failure

Wing

2950

2450

1950

2950

Without

Wing

(1)

Throttle --IDLE.

(1)

Throttle --IDLE.

(2)

Brakes --APPLY.

(3)

Wing

(3)

Wing

(4)

Mixture --IDLE

(5)

Ignition Switch --OFF.

After

Flaps

Speed:

Lbs

Glide:

Lbs

Flaps

FAILURES

FAILURE

Brakes --APPLY.

Flaps --RETRACT.

Mixture --IDLE Ignition

Takeoff:

Up.

Down.

.

Landing

Landing With Engine

Engine

Up.

Down.

OPERATIONAL

DURING

Flaps --RETRACT.

Switch --OFF.

Takeoff:

.

With

Power:

.

. . . .

CUT-OFF.

Engine

TAKEOFF

Power

TAKEOFF

OPERATION

CHECKLISTS

CHECKLI

RUN

STS

70 KIAS

70

KIAS

65 KlAS

65 KIAS

1l0KIAS

100 KlAS

100 KIAS

89 KIAS

89

KIAS

70 KIAS

70

KIAS

65

KlAS

65 KIAS

70 KIAS

65 KlAS

65 KIAS

3-3

SECTION

SECTION 3

EMERGENCY

EMERGENCY PROCEDURES

3

PROCEDURES

CESSNA

MODEL

182P

ENGINE

FORCED

EMERGENCY

FAILURE

(1)

Airspeed --70 KIAS

(1)

Airspeed --70

(2)

Mixture --IDLE

(2)

Mixture --IDLE

(3)

Fuel

(3)

Fuel

(4)

Ignition

(4)

Ignition

(5)

Wing

(5)

Wing

(6)

Master

(6)

Master

FAILURE

(1)

Airspeed --70 KIAS.

(1)

Airspeed --70 KIAS.

(2)

Carburetor

(2)

Carburetor

(3)

Fuel

(3)

Fuel

(4)

Mixture --RICH.

(4)

Mixture --RICH.

(5)

Ignition

(5)

Ignition

(6)

Primer --IN and LOCKED.

(6)

Primer --IN and LOCKED.

(1)

Airspeed --70 KIAS

(1)

Airspeed --70 KIAS

(2)

Mixture --IDLE

(2)

Mixture --IDLE

(3)

Fuel

(3)

Fuel

(4)

Ignition

(4)

Ignition Switch --OFF.

(5)

Wing

(5)

Wing

(6)

Master

(6)

Master

(7)

Doors --UNLA

(7)

Doors --UNLA

(8)

Touchdown --SLIGHTLY

(8)

Touchdown --SLIGHTLY

(9)

Brakes --APPLY

(9)

Brakes --APPLY

IMMEDIATElY

KIAS

65

KIA S (flaps

65

KIAS (flaps DOWN).

CUT-OFF.

Selector

Switch --OFF.

Flaps --AS REQUIRED (40°

Flaps --AS REQUIRED (400 recommended).

Switch --OFF.

Selector

Switch --BOTH

LANDINGS

LANDING

Selector

Switch --OFF.

Flaps --AS REQUIRED (40°

Flaps --AS REQUIRED (400 recommended).

Switch --OFF.

CUT-OFF.

Valve --OFF.

DURING

Heat --ON.

Valve --BOTH.

WITHOUT

65 KIAS

65

KIAS

CUT-OFF.

Valve --OFF.

TCH

TCH PRIOR TO TOUCHDOWN.

HEAVILY.

HEA

AFTER

(flaps

UP).

(flaps UP).

DOWN).

FLIGHT

fliGHT

(or

START

(or

START

ENGINE

(flaps

UP).

(flaps

UP).

(flaps

DOWN).

(flaps DOWN).

PRIOR

TO

TOUCHDOWN.

TAIL

LON.

TAIL

LON.

VILY.

TAKEOFF

recommended).

if

propeller

if

propeller

POWER

recommended).

is

stopped).

is

stopped).

PRECAUTIONARY

(1)

Wing

Flaps --20°.

Airspeed --65 KIAS.

Selected

retract

Radio

and

Radio and

Wing

Flaps --40°

Wing

Flaps --400 (on

Airspeed --65

Airspeed --65 KIAS.

Master

Switch --OFF.

3-4

(1) Wing

(2)

(3)

tJMln

tllen

(,.

~

(5)

(5}

(6)

(7)

('7)

LANDING

Field --FLY

flaps

upon

flaps

Electrical

reaching a safe

upon

reaching a safe

(on

KIAS.

WITH

ENGINE

WITH

ENGINE

OVER, noting

Switches --OFF.

final

approach).

final

approach).

altitude

POWER

terrain

and

airspeed.

obstructions,

Cessna SKYLANE 182P Pilot Operating Handbook

Specifications and Main Features

Frequently Asked Questions

User Manual

CONGRATULATIONS

PERFORMANCE -SPECIFICATIONS

GENERAL

LIMITATIONS

EMERGENCY PROCEDURES