Cessna 182S Skylane Quick setup guide

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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 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
COPYRIGHT@ 1997
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
1
2
3
4
5
6
7
I
I
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
1-4
1-4
1-4
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