Saturday, February 27, 2021

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Cessna 182

Summary

The Cessna 182 is a powerful touring aircraft with excellent short field capabilities. You'll soon realize why the Skylane is the four-passenger aircraft chosen by more pilots as their personal favourite aircraft than any other.
  
Instrument Panel
  
  
  
  
  

 

Specifications:

Electronics:

Avionics/Radios:  
  Bendix/King KX-155A Digital Nav/Com with Glide Slope
  Bendix/King
KX-155A Digital Nav/Com with VOR/LOC

  Bendix/King KCS-55A Slaved HSI System 
 
Bendix/King KSN-765 GPS, Multi-Function Display, Short Guide

  Bendix/King KSN-765 GPS, Multi-Function Display, Full Manual

  Bendix/King KSN-765 GPS, Multi-Function Display, Simulator

  Bendix/King KGP-560 Enhanced Ground Proximity Warning System

  Bendix/King KT-74  ADS-B Transponder

  Bendix/King KAP-140 Autopilot with Pre-Select and Alert

  Bendix/King KR-87 Digital ADF Receiver

  Bendix/King KMA-26 Audio Panel with 3LMB/Intercom
  BFG
WX-500 Stormscope

  JPI EDM 830 Engine Management System


Exterior:            Allover White with Red and Blue Trim Stripes


Interior:             Deluxe Grey Leather

Specifications:

Performance:  

SPEED

            Maximum at Sea Level...............................................................

            Cruise, 80% Power at 6000 Ft...................................................

CRUISE

Using recommended lean mixture with fuel allowance for engine start, taxi,

takeoff, climb and 45 minutes reserve.

 

            75% Power at 6000 Ft.................................................. Range  

            88 Gallons (333 L) Usable Fuel .....................................Time

RATE OF CLIMB AT SEA LEVEL............................................................

SERVICE CEILING.................................................................................

TAKEOFF PERFORMANCE:

            Ground Roll...............................................................................

            Total Distance Over 50 Ft. Obstacle...........................................

LANDING PERFORMANCE:

            Ground Roll...............................................................................                Total Distance Over 50 Ft. Obstacle............................................

STALL SPEED:

            Flaps Up, Power Off..................................................................

            Flaps Down, Power Off..............................................................

MAXIMUM WEIGHT:

            Ramp........................................................................................

            Takeoff.....................................................................................

            Landing.....................................................................................

STANDARD EMPTY WEIGHT................................................................

MAXIMUM USEFUL LOAD....................................................................

BAGGAGE ALLOWANCE......................................................................

WING LOADING: Lbs/Sq Ft...................................................................

POWER LOADING: Lbs/HP...................................................................

Engine:  

FUEL CAPACITY...................................................................................

OIL CAPACITY....................................................................................... ENGINE: Textron Lycoming...................................................................

            230 BHP at 2400 RPM

PROPELLER: Diameter  3-blade..........................................................

 

 

 

145 KTS

140 KTS

 

 

 

 

820 NM

6.05 HRS

924 FPM

18,100 FT

 

243 m

462 m

 

180 m

412 m

 

43 KIAS

36 KIAS

 

1410 kg

1406 kg

1338 kg

873 kg

537 kg

90 kg

17.8

13.5

 

348 L

9 Qts

IO-540-AB1A5

 

79 In

 

Planning:

Command Flight Planner Data VH-PAF

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.