Cessna 172S Skyhawk Kurzanleitung zur Einrichtung

CeSSrii

ATextron Company

• 1725 5kyhawk

Information Manual

172SIM

CESSNA

MODEL 172S

NOTICE

INTRODUCTION

THE TIME OF ISSUANCE, THIS INFORMATION

MANUAL WAS

EXACT DUPLICATE OF THE

OFFICIAL PILOT'S OPERATING HANDBOOK AND

FAA APPROVED AIRPLANE FLIGHT MANUAL AND

USED FOR GENERAL PURPOSES

ONLY.

IT WILL NOT

KEPT CURRENT AND,

THEREFORE, CANNOT BE USED AS A

SUBSTITUTE FOR THE OFFICIAL PILOT'S

OPERATING HANDBOOK AND FAA APPROVED

AIRPLANE FLIGHT MANUAL INTENDED FOR

OPERATION

THE AIRPLANE.

THE PILOT'S OPERATING HANDBOOK MUST BE

CARRIED

THE AIRPLANE AND AVAILABLE TO

THE PILOT

ALL TIMES.

I Revision 5

Cessna Aircraft Company

Original Issue - 8 July 1998

Revision 5 - 19 July 2004

U.S.

INTRODUCTION CESSNA

MODEL 172S

PERFORMANCE -SPECIFICATIONS

*SPEED:

Maximum at Sea Level . . . . . . . . . . . . . . . . . . . . . . . . . 126 KNOTS

Cruise, 75% Power at 8500 Feet.

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

124 KNOTS

CRUISE: Recommended lean mixture with fuel allowance for engine

start, taxi, takeoff, climb and 45 minutes reserve.

75% Power at 8500 Feet

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

Range -518 NM

53 Gallons Usable Fuel.

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

Time -4.26 HRS

Range at 10,000 Feet, 45% Power

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

Range -638

53 Gallons Usable Fuel.

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

Time -6.72 HRS

RATE-OF-CLIMB

SEA LEVEL

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

730 FPM

SERVICE CEILING

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

14,000 FEET

TAKEOFF PERFORMANCE:

Ground Roll

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

960 FEET

Total Distance Over 50 Foot Obstacle

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

1630 FEET

LANDING PERFORMANCE:

Ground Roll

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

575 FEET

Total Distance Over 50 Foot Obstacle

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

1335 FEET

STALL SPEED:

Flaps Up, Power Off

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

53 KCAS

Flaps Down, Power Off

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

.48 KCAS

MAXIMUM WEIGHT:

Ramp

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

2558 POUNDS

Takeoff

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

2550 POUNDS

Landing

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

2550 POUNDS

STANDARD EMPTY WEIGHT

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

1663 POUNDS

MAXIMUM USEFUL LOAD

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

895 POUNDS

BAGGAGE ALLOWANCE

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

120 POUNDS

(Continued Next Page)

Iii

U.S. Revision 5

CESSNA

MODEL 172S INTRODUCTION

PERFORMANCE -SPECIFICATIONS (Continued)

WING LOADING: Lbs/Sq.

Ft.

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

14.7

POWER LOADING: Lbs/HP

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

14.2

FUEL CAPACITY

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

56 GALLONS

OIL CAPACITY

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

8 QUARTS

ENGINE: Textron Lycoming

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

IO-360-L2A

180

BHP

at 2700

RPM

PROPELLER: Fixed Pitch, Diameter.

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

76 INCHES

NOTE

*Speed performance

shown for

airplane equipped with

speed

fairings

which

increase

the

speeds

approximately 2 knots. There is a corresponding difference

range,

while

all

other

performance

figures

are

unchanged when speed fairings are installed.

The above performance figures are based

airplane weights at 2550

pounds, standard atmospheric conditions, level, hard-surfaced dry

runways and

wind. They are calculated values derived from flight

tests conducted

Cessna Aircraft Company under carefully

documented conditions and will vary with individual airplanes and

numerous factors affecting flight performance.

I Revision 5 U.S. iii/iv

CESSNA

MODEL 172S INTRODUCTION

Information

Manual

SKYHAVVK

Member

GAMA

Cessna Aircraft Company

Model 172S

THIS MANUAL INCORPORATES INFORMATION ISSUED

THE.

PILOT'S OPERATING HANDBOOK AND FAA APPROVED

AIRPLANE 'FLIGHT MANUAL AT REVISION 5 DATED 19 JULY 2004

(PART NUMBER 172SPHUS05).

CESSNAAIRCRAFT COMPANY

WICHITA, KANSAS USA

I Revision 5 U.S.

172SIM

v/vi

CESSNA

MODEL 172S INTRODUCTION

TABLE OF CONTENTS

SECTION

GENERAL

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

LIMITATIONS

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

EMERGENCY PROCEDURES

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

NORMAL PROCEDURES

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

PERFORMANCE

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

WEIGHT AND BALANCE/EQUIPMENT LIST

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

AIRPLANE AND SYSTEMS DESCRIPTION

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

HANDLING, SERVICE AND MAINTENANCE

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

SUPPLEMENTS

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

I Revision 5 U.S. vii/viii

CESSNA

MODEL 172S

SECTION 1

GENERAL

TABLE OF CONTENTS

Three View -Normal Ground Attitude

SECTION 1

GENERAL

Page

1-2

Introduction

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

1-4

Descriptive Data

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

1-4

Engine

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

1-4

Propeller

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

1-4

Fuel

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

1-4

Oil

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

1-5

Maximum Certificated Weights . . . . . . . . . . . . . . . . . . . . . 1-6

Standard Airplane Weights

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

1-7

Cabin And Entry Dimensions

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

1-7

Baggage Space And Entry Dimensions

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

1-7

Specific Loadings

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

1-7

Symbols, Abbreviations and Terminology

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

1-8

General Airspeed Terminology And Symbols

...........

1-8

Meteorological Terminology

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

1-9

Engine Power Terminology

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

1-9

Airplane Performance And Flight Planning Terminology 1-10

Weight And Balance Terminology

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

1-11

Metric1Imperial 1U.S. Conversion Charts

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

1-13

Weight Conversions

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

1-14

Length Conversions

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

1-16

Distance Conversions

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

1-20

Volume Conversions

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

1-21

Temperature Conversions

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

1-24

Hectopascals

Inches Me.rcury

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

1-251

Volume to Weight Conversions

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

1-26

Quick Conversions

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

1-27/1-28

Revision 4

1-1

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