PERFORMANCE-
SPECIFICATIONS
CESSNA
MODELTR182
PERFORMANCE - SPECIFICATIONS
SPEED:
Maximum at 20,000 Ft
Cruise, 75% Power at 20,000 Ft
Cruise, 75% Power at 10,000 Ft
CRUISE: Recommended lean mixture with fuel allowance for
engine start, taxi, takeoff, climb and 45 minutes
reserve at 45% power,
75% Power at 20,000 1ft
88 Gallons Usable Fuel
75% Power at 10,000 Ft
88 Gallons Usable Fuel
Maximum Range at 20,000 Ft
88 Gallons Usable Fuel
Maximum Range at 10,000 Ft
88 Gallons Usable Fuel
RATE OF CLIMB AT SEA LEVEL
CERTIFICATED MAXIMUM OPERATING ALTITUDE
TAKEOFF PERFORMANCE:
Ground Roll . . . . . . . . . . .
Total Distance Over 50-Ft Obstacle
LANDING PERFORMANCE:
Ground Roll . . . . . . . . . .
Total Distance Over 50-Ft Obstacle
STALL SPEED (CAS):
Flaps Up, Power Off
Flaps Down, Power Off
MAXIMUM WEIGHT:
Ramp .
Takeoff or Landing . .
STANDARD EMPTY WEIGHT:
Turbo Skylane fiG
Turbo Sky lane RG II ..
MAXIMUM USEFUL LOAD:
Turbo Skylane RG
Turbo Skylane.RG
II . .
BAGGAGE ALLOWANCE'
WING LOADING: Pounds/Sq Ft
POWER LOADING: Pounds/HP
FUEL CAPACITY: Total
OIL CAPACITY . .•.. ' '.' .
ENGINE: Turbocharged Avco Lycoming
.235 BHP at 2400 RPM
PROPELLER: Constant Speed, Diameter
Range
Time
Range
Time
Range
Time
Range
Time
ii
.187 KNOTS
.173 KNOTS
.158 KNOTS
875 NM
5.3 HRS
845NM
5.4HRS
1010 NM
8.1 HRS
1030 NM
8.5 HRS
.1040 FPM
.20,000 FT
.820 FT
.1570 FT
.600 FT
.1320 FT
.54 KNOTS
.50 KNOTS
.3112 LBS
.3100 LBS
.1764 LBS
.1815 LBS
.1348 LBS
.1297 LBS
.200 LBS
.17.8
.13.2
.92 GAL
.9
QTS
. 0-540-L3C5D
.82
IN
1 October 1978
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