Cessna 182S Skylane Performance and Specifications PDF

Cessna 182S Skylane Performance and Specifications the Cessna Aircraft Company under carefully documented conditions and will vary with individual ...

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Cessna 182S Skylane Performance and Specifications

Cessna 182S Skylane Performance and Specifications the Cessna Aircraft Company under carefully documented conditions and will vary with individual ...

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Cessna 182S Skylane Performance and Specifications

Performance - Standard Specifications

SPEED -Maximum at Sea Level .......................................................145 KTS -Cruise, 80% Power at 6000 Ft.............................................140 KTS CRUISE Using recommended lean mixture with fuel allowance for engine start, taxi,

takeoff, climb and 45 minutes reserve. -75% Power at 6000 Ft ............................................... Range 820NM

-88 Gallons Usable Fuel ..............................................Time 6.05 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:

-Flaps Up, Power Off ........................................................... 43 KIAS -Flaps Down, Power Off ....................................................... 36 KIAS

MAXIMUM WEIGHT:

-Ramp ............................................................................ 3110 LBS -Takeoff .......................................................................... 3100 LBS -Landing .............................................................. ........... 2950 LBS STANDARD EMPTY WEIGHT ..................................................... 1925 LBS MAXIMUM USEFUL LOAD......................................................... 1185 LBS BAGGAGE ALLOWANCE.............................................................200 LBS WING LOADING: Lbs/Sq Ft ............................................................ 17.8 POWER LOADING: Lbs/HP .............................................................. 13.5 FUEL CAPACITY ........................................................................ 92 GAL OIL CAPACITY ............................................................................ 9 QTS ENGINE: Textron Lycoming .............................................. IO-540-AB1A5,

230 BHP at 2400 RPM

PROPELLER: Diameter - 3-blade ....................................................79 IN

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 Cessna Aircraft Company under carefully documented conditions and will vary with individual airplanes

and numerous other factors affecting flight performance.

AIRSPEEDS - NORMAL OPERATIONS

Takeoff:

-Normal Climb Out.......................................................70 - 80 KIAS -Short Field Takeoff, Flaps 10º, Speed at 50 ft........................ 57 KIAS

Enroute Climb, Flaps Up:

-Normal, sea level ....................................................... 85 - 95 KIAS -Best Rate-of-Climb, Sea level.............................................. 80 KIAS -Best Rate-of-Climb, 10,000 ft ............................................. 72 KIAS -Best Angle-of-Climb, Sea level ............................................ 63 KIAS -Best Angle-of-Climb, 10,000 ft ............................................ 66 KIAS

Landing Approach (2950 Lbs):

-Normal Approach Flaps Up........................................... 70 - 80 KIAS -Normal Approach, Flaps FULL....................................... 60 - 70 KIAS -Short Field Approach, Flaps FULL......................................... 60 KIAS

Balked Landing (2950 Lbs):

-Maximum Power, Flaps 20º ................................................ 55 KIAS

V-Speeds:

-Vne (never exceed) ......................................................... 175 KIAS -Vno (Maximum structural cruising speed) ........................... 140 KIAS -Vfe (Flaps 10°) ............................................................... 110 KIAS -Vfe (Flaps 20°) ............................................................... 101 KIAS -Vfe (Flaps 30°) ................................................................. 88 KIAS Maximum Recommended Turbulent Air Penetration Speed: -3100 Lbs........................................................................ 110 KIAS -2600 Lbs........................................................................ 101 KIAS -2000 lbs .......................................................................... 88 KIAS

Maximum Demonstrated Crosswind Velocity:

-Takeoff or landing .......................................................... 15 KNOTS

Stall Speed: