1978 Rockwell Commander 112TCA (Alpine Commander)

Recently upgraded | Low hour engine

SOLD
Posted:
A year ago
Views:
2075
Make
Rockwell
Model
Commander 112TCA (Alpine Commander)
Year
1978
Seller
WilcoAviation
Location
Lydd, United Kingdom
Condition
Pre-owned
Seller type
Broker
Total Time
2183 h
Engine Time
244 h
Undercarriage
Retractable Tricycle
Seats
4
Flight Rules
IFR
Serial Number
13274
Registration
N4698W

Highlights

  • Returning to us we are proud to exclusively offer this recently upgraded Rockwell Commander 112 TC-A powered by a very low hour Lycoming TO-360-C1A6D 210 HP turbocharged engine overhauled by Nicolson McLaren in 2010.
  • Eight Whiskey is located in the South East of England at Lydd Airport

Exterior

  • 8/10
  • White & Grey with Black Trim

Interior

  • 8/10
  • Cream Leather

Maintenance

  • Prop: new 2020
  • Engine overhauled by Nicolson McLaren in 2010
Airworthiness Until
02/29/2024

Specifications

Seat Configuration
1+3
Gross Weight
1338 Kg
Empty Weight
923 Kg
Useful Load
415 Kg
Cruise Speed
154 Kt
Range
835 Nm
Fuel Burn
38 l/h
Fuel Capacity
257 l

Engine

Manufacturer, Model
Lycoming, TO-360-C1A6D
  • Prop: HARTZELL 3 BLADE
Power
210
Fuel Type
Avgas 100LL
TTSN
244
OHD
03/23/2010

Avionics

Audio Panel
Garmin, GMA 340
EMS
J.P. Instruments, EDM 700
Basic instruments
  • Direction Indicator (DI)
  • Vertical Speed Indicator (VSI)
  • Air Speed Indicator (ASI)
  • Altitude Indicator (AI)
  • Course Deviation Indicator (CDI)
  • Distance Measuring Equipment (DME)
  • Automatic Direction Finding (ADF)

Electrical equipment

Landing / Taxi lightning
  • NAV Lights
  • LED Landing light
  • Strobe Lights

Additional Remarks

  • 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. The 1976 Commander line introduced two new models one of which was the Commander 112TC with a turbocharged engine of 210 hp and MTOW of 2,850 lb, The 112TC had a significantly improved cruise speed of 160 knots (300 km/h; 180 mph) when flying at higher altitudes, as high as 20,000 feet (6,100 m), which was aided by a 32 inches (810 mm) increase in wingspan.
  • In the late 70’s the 112TC was further upgraded with a 50 pounds (23 kg) maximum weight increase and minor detail changes. The major change was a complete makeover of the avionics suite with a three-axis autopilot, producing the 112TCA “Alpine” such as N4698W we have listed.
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