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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 COMPANYOR¡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:

Ramp3110 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-Bladeí; 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. I3-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 Companyunder carefully documented conditions and will vary with

individual airplanes and numerous other factors affecting flight performance.

Dec 1/97iii/(iv blank)

lnformation Manual

COPYRIGHT@ 1997

The Cessna Aircraft Company

Wichita, Kansas USA

Nov 1/01

Cessna Aircraft Company

Model 182S

THIS MANUAL INCORPORATES INFORMATION ISSUEDTHRU REVISION 04 TO THE PILOTS OPERATINGHANDBOOK AND FAA APPROVED AIRPLANE FLIGHTMANUAL DATED 3 FEBRUARY 1997.

Q uenaerofGAMA

P/N: 182SlM

v/(viblank)

CESSNA

MODEL 182STABLE 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

1 2 3 4 5 6 7 I I

Feb 3/97vii/(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 . . . 1-8MeteorologicalTerminology 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 Charts1-13

1-2 1-4 1-4 1-4 1-4 1-4 1-5 1-6

1-7iit

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

1-1Nov 15/00

SECTION 1

GENERAL

CESSNA

MODEL 182S

0785T1 001

0785T1 001

Figure 1-1. Three View - Normal Ground Attitude (Sheet 1 ol2)

1-2Feb 3/97

CESSNA

MODEL 182S

NOTE 3:

NOTE 4:

NOTE 5:

NOTE 6:

SECTION 1

GENERAL

NOTE 1: WING SPAN SHOWN WITH STANDARD STROBE

LIGHTS INSTALLED.

NOTE 2:NORMAL GROUND ATTITUDE IS SHOWN WITH

NOSE STRUT SHOWING APPROXIMATELY 2" OF

STRUT, AND WINGS LEVEL.

WHEEL BASE LENGTH lS 661/z'.

PROPELLER GROUND CLEARANCE IS 1O ".

WING AREA IS 174 SQUARE FEET.

MtNtMUM TURNTNG RADTUS (.ptVOT potNT TO

oUTBoARD W|NG TtP) tS 27', - 0".

0785T1001

Figure 1-1. Three View - Normal Ground Attitude (Sheet 2 of 2)

Feb 31971-3

SECTION 1

GENERAL

CESSNA

MODEL 182S

INTRODUCTION

This handbook contains 9 sections, and includes the material required to be furnished to the pilot by FAR Part 23' lt also contains supplemental data supplied by The Cessna Aircraft Company.

Section 1 provides basic data and information of general interest'It also contains definitions or explanations of symbols,

abbreviations, and terminology commonly used.

DESCRIPTIVE DATA

ENGINE

Number of Engines: 1.

Engine Manufacturer: Textron Lycoming.

Engine Model Number: lO-540-AB1 45.

Engine Type: Normally aspirated, direct drive, air-cooled,- horizontally opposed, fuel injected, six cylinder engine with

541 cu. in. displacement.

Horsepower Rating and Engine Speed: 230 rated BHP

at 2400 RPM.

PROPELLER (2-Bladed)

Propeller Manufacturer: Mc0auley Propeller Systems.

Propeller Model N umber: B.2D34C235/90DKB-8'

Number of Blades: 2.

Propeller Diameter: 82 inches.

Propeller Type: Constant speed and hydraulically actuated, wlth .alow'pitch sétting of 17.0' and a high pitch setting of 31.8' (30 inch

station).

PROPELLER (3-Bladed)

Propeller Manufacturer: McOauley Propeller Systems.

Propeller Model Number: 83D36C431/80VSA-1.

Number of Blades: 3.

Propeller Diameter: 79.0 inches.

Propeller Type: Constant speed and hydraulically actuated, wlth.a low pitch sétting of 14.9' and a high pitch setting of 31.7' (30 inch station).

1-4Dec 1197

CESSNA

MODEL 182S

SECTION 1

GENERAL

FUEL

¡[, wnnrrruo

USE OF UNAPPROVED FUELS MAY RESULT IN

DAMAGE TO THE ENGINE AND FUEL SYSTEMCOMPONENTS, RESULTING IN POSSIBLE

ENGINE FAILURE.

Approved FuelGrades (and Colors):

100LL Grade Aviation Fuel (Blue).

100 Grade Aviation Fuel (Green).

NOTE

lsopropyl alcohol or diethylene glycol monomethyl ether(DiEGME) may be added to the fuel supply. Additive

concentrations shall not exceed 17" lor isopropyl alcohol or0.10% to 0.15% for D|EGME. Refer to Section I for

additional information.

FuelCapacity:TotalCapacity: 92.0 U.S. gallons.

Total Usable: 88.0 U.S. gallons.

Total Capacity Each Tank: 46.0 U.S. gallons.

Total Usable Each Tank: 44.0 U.S. gallons.

NOTE To ensure maximum fuel capacity and minimize cross- feeding when refueling, always park the airplane in a wings-

level, normal ground attitude and place the fuel selector inthe Left or Right position. Refer to Figure 1-1 for normal

ground attitude dimensions.

1-5Nov 15/00

SECTION 1

GENERAL

olL

CESSNA

MODEL 182S

Oil Specification:

MiL-L-6082 Aviation Grade Straight Mineral Oil: Used when the airplane was delivered from the factory and should be used toquotesdbs_dbs24.pdfusesText_30

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