Rockwell Commander 112 / 114

ICAO aircraft code AC11
Manufacturer Rockwell International
Country United States
New price USD 0.6 million (2005)

The Rockwell Commander 112 is an American four-seat single-engined general aviation aircraft designed and built by North American Rockwell.

Specifications

Full description

Similar aircraft

Rockwell Commander 112 / 114 specifications

General

ICAO aircraft code
AC11
Manufacturer
Rockwell International
Manufactured
1972 - 2005
Country
United States
New purchase price
USD 0.6 million (2005)

Aircraft performance

Avionics:
Garmin GNC-300XL
Engine:
1x 1 × Lycoming IO-540-T4B5D
Piston
Power:
260 HP
Max Cruise Speed:
166 Kts
307 Km/h
Approach Speed (Vref):
56 Kts
Travel range:
732 Nm
1,356 Kilometers
Fuel Economy:
10.39 Nm / gallon
5.083 Km / liter
Service Ceiling:
17,400 feet
Rate of Climb:
1070 feet / minute
5.44meter / second
Take Off Distance:
655 meter - 2,148.92 feet
Landing Distance:
366 meter - 1,200.77 feet

Weight & dimensions

Max Take Off Weight:
1,479 Kg
3,261 lbs
Max Landing Weight:
1,424 Kg
3,139 lbs
Max Payload:
446 Kg
983 lbs
Fuel Tank Capacity:
70 gallon
265 liter

Disclaimer: The information on this page may not be accurate or current. Never use it for flight planning or any other aircraft operation purposes. No warranty of fitness for any purpose is made or implied. Flight planning or any other aircraft operations should only be done using official technical information provided by the manufacture or official aviation authorities.

About the Rockwell Commander 112 / 114

The Rockwell Commander 112 is an American four-seat single-engined general aviation aircraft designed and built by North American Rockwell (later Rockwell International) starting in 1972.

In 1976, they introduced the turbocharged version 112TC and mounting a larger engine with other minor improvements they introduced the Rockwell Commander 114. A total of approximately 1,300 examples of all models were produced before the production line shut down in 1980.

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