Cessna 182S Skylane Guide de configuration rapide

Textr

182S Skylane

182StM

NOTICE

AT THE TIME OF ISSUANCE, THIS

INFORMATION MANUAL WAS AN EXACT

DUPLICATE OF THE OFFICIAL PILOT'S

OPERATING HANDBOOK AND FAA

APPROVED AIRPLANE FLIGHT MANUAL

AND IS TO BE USED FOR GENERAL

PURPOSES ONLY.

IT WILL NOT BE 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 OPERAT¡ON OF THE

AIRPLANE.

CESSNA AIRCRAFT COMPANY

OR¡GINAL ISSUE .3 FEBRUARY 1997

FebS/97

PERFORMANCE.

SPECIFICATIONS CESSNA

MODEL 182S

PERFORMANCE - SPECIFICATIONS

* SPEED

Maximum at Sea Level 145 KTS

Cruise, 80% Power at 6000 Ft (Best Power Mixture) 140 KTS

CRUISE: Recommended lean mixture with fuel allowance for

engine start, taxi, takeoff, climb and 45 minutes

reserue.

71"/oPower at 6000 Ft Range 820 NM

88 Gallons Usable Fuel Time 6'05 HRS

Max Range at 10,000 Fl,55o/o Power Range 968 NM

88 Gallons Usable Fuel Time 8.05 HRS

RATE OF CLIMB AT SEA LEVEL: 924 FPM

SERVICE CEILING: 18,100 FT

TAKEOFF PERFORMANCE:

Ground Roll 795 FT

Total Distance Over 50 Ft. Obstacle 1514 FT

LANDING PERFORMANCE:

Ground Roll 590 FT

Total Distance Over 50 Ft. Obstacle 1350 FT

STALL SPEED (KCAS):

Flaps Up, Power Otf 54 KCAS

Flaps Down, Power Off . . 4s KCAS

MAXIMUM WEIGHT:

Ramp 3110 LBS

31OO LBS

2950 LBS

1 925 LBS

1 185 LBS

2OO LBS

Takeotf

Landing

STANDARD EMPTY WEIGHT:

MAXIMUM USEFUL LOAD:

BAGGAGE ALLOWANCE:

Nov 15/00

WING LOADING: Lbs/Sq Ft

POWER LOADING Lbs/HP

PER FOR MAN C E.SPECI FICATIONS

(Continued)

17.8

FUEL CAPACITY

OIL CAPACITY

CESSNA

MODEL 182S PERFORMANCE-

SPECIFICATIONS

13.5

92 GAL

9 QTS

ENGINE: Textron Lycoming |O-540-AB1A5

230 BHP at 2400 RPM

PROPELLER: Diameter - 3-Blade

Diameter - 2-Blade í; iill

NOTE

*Speed performance and range are shown for an airplane

equipped with optional speed fairings which increase the

speeds by approximately 3 knots. All other performance

when speed fairings are removed.

based on a 2-bladed propeller. I

3-blade propeller is essentially the I

The above performance figures are based on the indicated

weights, standard atmospheric conditions, level hard'surface

dry runways and no wind. They are calculated values derived

from flight tests conducted by the Gessna Aircraft Company

under carefully documented conditions and will vary with

individual airplanes and numerous other factors affecting flight

performance.

Dec 1/97 iii/(iv blank)

lnformation Manual

The Cessna Aircraft Company

Wichita, Kansas USA

Nov 1/01

Cessna Aircraft Company

Model 182S

THIS MANUAL INCORPORATES INFORMATION ISSUED

THRU REVISION 04 TO THE PILOTS OPERATING

HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT

MANUAL DATED 3 FEBRUARY 1997.

Q uenaerofGAMA

P/N: 182SlM

v/(viblank)

CESSNA

MODEL 182S TABLE OF CONTENTS

SECTION

TABLE OF CONTENTS

GENERAL

LIMITATIONS

EMERGENCY PROCEDURES

NORMAL PROCEDURES

PERFORMANCE

WEIGHT & BALANCE/EQUIPMENT LIST

A¡RPLANE & SYSTEMS DESCRIPTION

HANDLING, SERVICE & MAINTENANCE

SUPPLEMENTS

Feb 3/97 vii/(viiiblank)

CESSNA

MODEL 182S SECTION 1

GENERAL

SECTION 1

GENERAL

TABLE OF CONTENTS

Three View - Normal Ground Attitude

lntroduction

Descriptive Data

Engine

Propeller (2-Bladed)

Page

Propeller (3-Bladed)

Fuel

oit

Maximum Cefi if icated Weights

Standard Airplane Wei ghts

Cabin And Entry Dimensions

Baggage Space and Entry Dimensions

Specific Loadings 1-7

Symbols, Abbreviations and Terminology 1-8

GeneralAirspeed Terminology And Symbols . . . 1-8

MeteorologicalTerminology 1-9

Engine Power Terminology 1-9

Airplane Performance And Flight Planning Terminology 1-10

Weight And Balance Terminology . . . 1-11

Metric / lmperial/ U.S. Conversion Charts 1-13

1-2

1-4

1-5

1-6

1-7

iit

1-7

Weight Conversions

Length Conversions

Distance Conversions

Volume Conversions

Temperature Conversions

Volume to Weight Conversions

Quick Conversions

1-14

1-16

1-20

1-21

1-24

1-25

1-26

1-1

Nov 15/00

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