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Cessna 182E

AircraftCessna182 / R182 / TR182 › 182E

The Cessna 182E Skylane is a four-seat, high-wing, fixed-tricycle-gear piston single associated with the 1962 model year. It uses the Continental O-470-R rated at 230 hp and has a maximum takeoff weight of 2,800 lb.

The 182E was part of the early development of the Cessna 182 line, combining the O-470-R engine with a higher certificated weight than the earlier 182B represented in this reference.

Cessna 182E Weight and Balance Calculator →

Cessna 182E specifications

ManufacturerCessna
Model182E
Production years1962
Aircraft typeFour-seat piston single
Seats4
EngineContinental O-470-R
Power230 hp at 2600 rpm
PropellerConstant-speed, 2-blade
Landing gearFixed tricycle
CertificationFAA 3A13

Cessna 182E weights and capacities

Maximum takeoff weight2,800 lb
Standard fuel capacity65 gal total / 60 gal usable
Maximum baggage120 lb combined

Cessna 182E history and development

The Cessna 182E is associated with the 1962 model year and is certificated under FAA Type Certificate Data Sheet 3A13.

The model uses the Continental O-470-R engine rated at 230 hp at 2,600 rpm and has a maximum takeoff weight of 2,800 lb. The following 182F, 182G, 182H and 182J variants retained the same basic engine model and 2,800 lb maximum takeoff weight in the reference data used here.

Cessna 182E certification and applicability

FAA type certificate3A13
Model year1962

Cessna 182E fuel capacity

Standard fuel capacity is 65 U.S. gallons total with 60 gallons usable.

Fuel installation and approved optional equipment should be confirmed from the documentation applicable to the individual aircraft before using fuel quantities for weight and balance.

Cessna 182E model applicability and configuration

The 182E model designation identifies the certified variant, but installed equipment and approved modifications can differ between individual airplanes.

Operational limits and weight and balance calculations must use the approved documentation and current aircraft records applicable to the specific airplane.

Cessna 182E vs 182B

Specification182E182B
EngineContinental O-470-RContinental O-470-L
Power230 hp230 hp
Maximum takeoff weight2,800 lb2,650 lb
Standard usable fuel60 US gal55 US gal

The 182E and 182B are both 230 hp members of the Cessna 182 family, but the reference configurations use different Continental O-470 engine variants. The 182E also has a higher maximum takeoff weight and greater standard usable fuel.

Cessna 182E weight and balance

Cessna 182E weight and balance calculations must use the loading limits and current basic empty weight and moment or arm for the individual airplane.

The model-level 2,800 lb maximum takeoff weight and standard fuel capacity do not replace the approved weight and balance records for a specific aircraft.

Use the applicable owner's manual, approved supplements, equipment records and current weight and balance data for the individual airplane.

Open Cessna 182E Weight and Balance Calculator →

Always verify aircraft applicability. Check the current POH or AFM, equipment list and weight and balance records for the individual aircraft.

Cessna 182E frequently asked questions

What year is the Cessna 182E?

The Cessna 182E is associated with the 1962 model year.

What engine does the Cessna 182E use?

The Cessna 182E uses the Continental O-470-R rated at 230 hp at 2,600 rpm.

What is the maximum takeoff weight of a Cessna 182E?

The Cessna 182E has a maximum takeoff weight of 2,800 lb in the reference data used here.

How much usable fuel does a Cessna 182E hold?

The standard fuel system provides 60 U.S. gallons usable from 65 gallons total.

Reference sources

FAA: Type Certificate Data Sheet 3A13

Cessna: 1962 Model 182E Owner's Manual

Related 182 / R182 / TR182 models

← All Cessna 182 / R182 / TR182 models
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