Cessna 152 Guía de configuración rápida

Cessna,.

152

CESSNA MODEL 152

INFORMATION

MANUAL

.....___~

NOTICE

THE

TIME

ISSUANCE,

THIS

INFOR-

MATION

MANUAL

WAS

EXACT

DUPLI-

CATE OF THE

OFFICIAL

PILOT'S

OPERAT-

ING

HANDBOOK

AND

FAA

APPAOVED

AIRPLANE

FLIGHT

MANUAL

AND

USED

FOR

GENERAL

PURPOSES

ONLY.

WILL

NOT

BE KEPT

CURRENT

AND,

THEREFORE,

CANNOT

USED

SUBSTITUTE

FOR THE

OFFICIAL

PILOT'S

OPERATING

HANDBOOK

AND

FAA

APPROVED

AIRPLANE

FLIGHT

MANUAL

INTENDED

FOR

OPERATION

THE

AIR-

PLANE.

CESSNA

AIRCRAFT

COMPANY

JULY

1978

PERFORMANCE-

SPECIFICATIONS

CESSNA

MODEL 152

PERFORMANCE SPECIFICATIONS

*SPEED:

Maximum

Sea

Level

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

Cruise,

75%

Power

8000

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

CRUISE:

Recommended

lean

mixture

with

fuel

allowance

for

engine

start,

taxi,

takeoff,

climb

and

minutes

reserve

45%

power.

75%

Power

8000

. . .

24.5

Gallons

Usable

Fuel

75%

Power

8000

...

37.5

Gallons

Usable

Fuel

Maximum

Range

10,000

24.5

Gallons

Usable

Fuel

Maximum

Range

10,000

37.5

Gallons

Usable

Fuel

RATE

CLIMB

SEA

LEVEL

SERVICE

CEILING

. . . . . .

TAKEOFF

PERFORMANCE:

Ground

Roll

. . . . . . . .

Total

Distance

Over

50-Ft

Obstacle

LANDING

PERFORMANCE:

Ground

Roll

. . . . . . . . . . .

Total

Distance

Over

50-Ft

Obstacle

STALL

SPEED

(CAS):

Flaps

Up,

Power

Off

Flaps

Down,

Power

Off

MAXIMUM

WEIGHT:

Ramp

.......

Takeoff

Landing

. .

STANDARD

EMPTY

WEIGHT:

152

.........

152

. . . . . . . . .

MAXIMUM

USEFUL

LOAD:

152

........

· ·

152

. . . . . . . . .

BAGGAGE

ALLOWANCE

WING

LOADING:

Pounds/Sq

POWER

LOADING:

Pounds/HP

FUEL

CAP

ACITY:

Total

Standard

Tanks

Long

Range

Tanks

OIL

CAPACITY

ENGINE:

Avco

Lycoming

110

BHP

2550

RPM

PROPELLER:

Fixed

Pitch,

Diameter

Range

Time

Range

Time

Range

Time

Range

Time

110KNOTS

107

KNOTS

350NM

3.4

HRS

580NM

5.5

HRS

415NM

5.2

HRS

690NM

8.7HRS

715

FPM

14,700

725

1340

475

1200

KNOTS

43KNOTS

1675

LBS

1670

LBS

1101

LBS

1133

LBS

574

LBS

542

LBS

120

LBS

10.5

15.2

GAL.

6QTS

O-235-L2C

IN.

*Speed

performance

shown

for

airplane

equipped

with

optional

speed

fairings,

which

increase

the

speeds

approximately

knots.

There

corresponding

difference

range,

while

all

other

performance

figures

are

unchanged

when

speed

fairings

are

installed.

July

1978

INFORMATION

MANUAL

CESSNA

AIRCRAFT

COMPANY I

1979 MODEL 152

C 1993

CESSNA

AIRCRAFT

COMPANY

WICHITA,

KANSAS,

USA

Dll36-13-RGI-2500-4/97

REPRINTING OF THIS

MANUAL

INCORPO-

RATES

INFORMATION

ISSUED

REVISION 1

DATED

MARCH

1983 FROM

Tl!E

PILOT'S

OPERATING

HANDBOOK

AND

FAA APPROVED

AIRPLANE FLIGHT

MANUAL.

iii

TABLE

CONTENTS

CESSNA

MODEL

152

TABLE

CONTENTS

SECTION

GENERAL

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

LIMITATIONS

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

EMERGENCY

PROCEDURES

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

NORMAL PROCEDURES

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

PERFORMANCE

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

WEIGHT

& BALANCE/

EQUIPMENT

LIST

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

AIRPLANE

SYSTEMS

DESCRIPTIONS

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

AIRPLANE

HANDLING,

SERVICE

& MAINTENANCE

........

SUPPLEMENTS

(Optional

Systems Description

Operating

Procedures)

..........

July

1978

CESSNA

MODEL

152

SECTION 1

GENERAL

TABLE OF

CONTENTS

SECTION

GENERAL

Page

Three

View

1-2

Introduction

1-3

Descriptive

Data

1-3

Engine

1-3

Propeller

1-3

Fuel

. . . 1-3

Oil

Maximum

Certificated

Weights

1-5

Standard

Airplane

Weights

. 1-5

Cabin

And

Entry

Dimensions

. 1-5

Baggage

Space

Dimensions

. . 1-5

Specific

Loadings

. . . . . . 1-5

Symbols,

Abbreviations

And

Terminology

1-5

General

Airspeed

Terminology

And

Symbols

1-5

Meteorological

Terminology

. . . . . . . 1-6

Engine

Power

Terminology

. . . . . . . . 1-7

Airplane

Performance

And

Flight

Planning

Terminology

1-7

Weight

And

Balance

Terminology

. . . . . . . . . . . 1-7

July

1978 1-1

SECTION

GENERAL

•------10'-0"----

NOTES:

CESSNA

MODEL 152

Wing

span shown with conical camber wing

tips and strobe

lights

installed. If standard

wing tips without strobe lights are installed,

wing

span

32' • 8 1

/2".

Maximum height shown with nose gear

depressed, all tires and nose

strut

prop•

erly inflated and flashing beacon installed.

Wheel

base

length

58".

Propeller ground clearance

12".

Wing

area

159 1/2 square feet.

------33'-4"------+-1•1

Figure

1-1.

Three

View

1-2 1

July

1978

CESSNA

MODEL

152

THIS DATA APPLICABLE ONLY TO AIRPLANES WITH LYCOMING

O-235-L2C ENGINE.

FOR

AIRPLANES WITH ENGINE MODIFIED TO

O-235-N2C,

REFER

TO DATA IN.SECTION 9 SUPPLEMENT.

INTRODUCTION

SECTION 1 I

GENERAL

This

handbook

contains

sections,

and

includes

the

material

required

furnished

the

pilot

CAR

Part

also

contains

supplemental

data

supplied

Cessna

Aircraft

Company.

Section

provides

basic

data

and

information

general

interest.

also

contains

definitions

explanations

symbols,

abbreviations,

and

terminology

commonly

used.

DESCRIPTIVE

DATA

ENGINE

Number

Engines:

Engine

Manufacturer:

Avco

Lycoming.

Engine

Model

Number:

O-235-L2C.

Engine

Type:

Normally-aspirated,

direct-drive,

air-cooled,

horizontally-

opposed,

carburetor

equipped,

four-cylinder

engine

with

233.3

cu.

in.

displacement.

Horsepower

Rating

and

Engine

Speed:

110

rated

BHP

2550

RPM.

PROPELLER

Propeller

Manufacturer:

McCauley

Accessory

Division.

Propeller

Model

Number:

1A103/TCM6958.

Number

Blades:

Propeller

Diameter,

Maximum:

inches.

Minimum:

67.5

inches.

Propeller

Type:

Fixed

pitch.

FUEL

Approved

Fuel

Grades

(and

Colors):

100LL

Grade

Aviation

Fuel

(Blue).

100

(Formerly

100/130)

Grade

Aviation

Fuel

(Green).

Fuel

Capacity:

Standard

Tanks:

Total

Capacity:

gallons.

Total

Capacity

Each

Tank:

gallons.

Total

Usable:

24.5

gallons.

July

1978

Revision

1 -

March

1983

1-3

SECTION

GENERAL

THIS DATA'APPUCABLE ONLY TO AIRPLANES WITH LYCOMING

0-235-UC

ENGINE.

FOR

AIRPLANES WITH ENGINE MODIFIED TO

O-Z35-N2C,

REFER

TO DATA IN SECTION 9 SUPPLEMENT.

CESSNA

MODEL

152

OIL

Long

Range

Tanks:

Total

Capacity:

gallons.

Total

Capacity

Each

Tank:

19.5

gallons.

Total

Usable:

37.5

gallons.

NOTE

Due

cross-feeding

between

fuel

tanks,

the

tanks

should

re-topped

after

each

refueling

assure

maximum

capacity.

Oil

Grade

(Specification):

MIL-L-6082

Aviation

Grade

Straight

Mineral

Oil:

Use

replenish

supply

during

first

hours

and

the

first

25-hour

oil

change.

Continue

use

until

total

hours

has

accumulated

oil

consumption

has

stabilized.

NOTE

The

airplane

was

delivered

from

the

factory

with

corro-

sion

preventive

aircraft

engine

oil.

This

oil

should

drained

after

the

first

hours

operation.

MIL-L-22851

Ashless

Dispersant

Oil:

This

oil

must

beused

after

first

hours

oil

consumption

has

stabilized.

Recommended

Viscosity

for

Temperature

Range:

MIL-L-6082

Aviation

Grade

Straight

Mineral

Oil:

SAE

above

16°C (60°F).

SAE

between

-1°C (30°F)

and

32°C (90°F).

SAE

between

-18°C (0°F)

and

21°c

(70°F).

SAE

below

-12°C (10°F).

MIL-L-22851

Ashless

Dispersant

Oil:

SAE

above

16°C (60°F).

SAE

between

-1°C (30°F)

and

32°C (90°F).

$AE

SAE

between

-18°C "(0°F)

and

21°c

(70°F).

SAE

below·

-12°c

(10°F).

Oil

Capacity:

Sump:

Quarts.

Total:

Quarts

(if

oil

filter

installed).

1-4 1

July

1978

Revision

1 -

March

1983

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