Aircraft > Single-Engine Piston > Commander > N112CA: Commander 112
N112CA: Commander 112
Last Updated
Nov. 10, 2023
Details
Registration #
N112CA
Status
Off Market
Year
1972
Make
Commander
Model
112
Serial Number
112-23
TTAF
3448
Engine 1 Time
237
Flight Rules
IFR
Location
Bonaire USA
Price History
April 27, 2023
98,500
Listings
Site
Price
Status
Updated
Description
Aircraft Registration: N112CA
Aircraft Make/Model: Rockwell Commander 112
Serial Number: 112-23
Year: 1972
Engine: Lycoming IO-360-C1D6 (200HP, 2,000 TBO)
Propeller Hartzell Top Prop HC-E3YR-1RF/F7392 3-Blade
Airframe Total Time: 3,447.86
Engine Time Since Overhaul 237.37
Propeller Time Since New 237.37
Location: KPXE (Perry, Georgia) Aircraft always hangered and/or covered.
Exterior: 2002 by Commander Aircraft, Painted White, Burgundy, Turquoise, Silver.
2019 new windshield installed
Interior: 2002 by Commander Aircraft, All new interior, grey leather seats, side panels, and carpet. Replaced aft cabin side windows.
History:
2/1976 - Repaired certain structural components in RH wing. Work was not as a result of an accident. Work was done by Commander Aircraft to correct a manufacturing problem. Form 337 filed. Substantial engineering documentation.
5/2015 - Partial nose gear collapse. Engine overhauled by Central Cylinder Service Inc. and prop replaced. No airframe damage.
Complete logs since manufacture.
Inspections:
Annual: Completed 9/2023
Static System: Due 6/2024
Performance:
Cruise Speed: 130 KTS
Fuel Capacity: 60 Gal (Usable)
Fuel Consumption: 9.5 GPH ROP 8.5 GPH LOP 6 hours
Range: 780 nm (no reserve)
Weights:
Gross Weight: 2,650 Lbs.
Empty Weight: 1,916 Lbs.
Useful Load: 734 Lbs.
CG: 104.57
Category:
Utility Category - when within limited aft CG and 2488 GWT
Normal Category - all other operations
Avionics:
Garmin GNS 430W WAAS GPS
Garmin GNS 530W WAAS GPS
Garmin GI-106A ILS Indicator (2X)
Terra 350D Audio Panel
UAvionix AV-30-C Attitude Indicator
UAvionix AV-30-C Heading Indicator
STEC 20/30 Autopilot with Alt Hold
Garmin GTX-330ES (TIS traffic and ADS-B-Out Transponder)
Trans-Cal SSD 120-35C Encoder
Autopilot notes:
The STEC 20/30 System is rate based, not attitude based. It operates from input from the Turn & Bank instrument, not the attitude. It does not need vacuum to operate and will continue to operate even in the case of a failure of the vacuum pump. It has features of Heading, NAV Track, and Altitude hold. It will track a localizer or LPV course but will not follow a glide slope. In this airplane, it is wired to follow either the NAV-1, Garmin GNS-430W or the Nav-2, GNS-530W.
Airframe:
Hartzell 3-blade propeller, eliminates AD
Brackett induction filter
Sky Tec Starter - eliminates sticky Bendix drive
Copper battery cables - eliminates aluminum cables with better electrical connections.
Whelen anti-collision light system
Whelen strobe light
M-20 Turbos air/oil separator
GAMI fuel injectors, allows running lean of peak (allows 8.5 GPH/125 KTS)
Sure Fly Electronic Ignition Model SIM4P (Left Mag)
JPI EDM-830 engine analyzer (EGT (X4), CHT (X4), fuel flow, fuel totalizer, lean finder, OAT, Oil Temp, Oil Pressure, RPM, and MP)
Harrison Aero elevator splice kit on RH side - AMOC for repair under AD 2012-02-11.
Aerodyne modified MLG and NLG actuators
Updated cabin doors installed by Commander Aircraft
Airtex ELT345 (connected to GNS 530 GPS for position information)
Removed vacuum pump and associated systems (UAvionix AV-30-C installation)
Removed both left and right elevators IAW Commander 112/B/TC/TCA Maintenance Manual. Accomplished alteration to the elevators by replacing the right elevator spar and the left and right outboard elevator hinge fittings with Aerodyme PMA (44285-RE2 or 44285-RE2-SP) and associated installation items 44285-RE9 carrier plates, 44285-RE7 shims, and 44285-RE8 radius blocks in accordance with Aerodyme PMA Elevator Hinge Fitting Installation Instructions Doc. No. 44285-RE501-IM dated 15 April 2015.
Avionics
Avionics: Garmin GNS 430W WAAS GPS Garmin GNS 530W WAAS GPS Garmin GI-106A ILS Indicator (2X) Terra 350D Audio Panel UAvionix AV-30-C Attitude Indicator UAvionix AV-30-C Heading Indicator STEC 20/30 Autopilot with Alt Hold Garmin GTX-330ES (TIS traffic and ADS-B-Out Transponder) Trans-Cal SSD 120-35C Encoder
Airframe
Aircraft Registration: N112CA
Aircraft Make/Model: Rockwell Commander 112
Serial Number: 112-23
Year: 1972
Engine: Lycoming IO-360-C1D6 (200HP, 2,000 TBO)
Propeller Hartzell Top Prop HC-E3YR-1RF/F7392 3-Blade
Airframe Total Time: 3,447.86
Engine Time Since Overhaul 237.37
Propeller Time Since New 237.37
Location: KPXE (Perry, Georgia) Aircraft always hangered and/or covered.
Exterior: 2002 by Commander Aircraft, Painted White, Burgundy, Turquoise, Silver.
2019 new windshield installed
Interior: 2002 by Commander Aircraft, All new interior, grey leather seats, side panels, and carpet. Replaced aft cabin side windows.
History:
2/1976 - Repaired certain structural components in RH wing. Work was not as a result of an accident. Work was done by Commander Aircraft to correct a manufacturing problem. Form 337 filed. Substantial engineering documentation.
5/2015 - Partial nose gear collapse. Engine overha
Remarks
Hartzell 3-blade propeller, eliminates AD Brackett induction filter Sky Tec Starter - eliminates sticky Bendix drive Copper battery cables - eliminates aluminum cables with better electrical connections. Whelen anti-collision light system Whelen strobe light M-20 Turbos air/oil separator GAMI fuel injectors, allows running lean of peak (allows 8.5 GPH/125 KTS) Sure Fly Electronic Ignition Model SIM4P (Left Mag) JPI EDM-830 engine analyzer (EGT (X4), CHT (X4), fuel flow, fuel totalizer, lean finder, OAT, Oil Temp, Oil Pressure, RPM, and MP) Harrison Aero elevator splice kit on RH side - AMOC for repair under AD 2012-02-11. Aerodyne modified MLG and NLG actuators Updated cabin doors installed by Commander Aircraft Airtex ELT345 (connected to GNS 530 GPS for position information) Removed vacuum pump and associated systems (UAvionix AV-30-C installation) Removed both left and right elevators IAW Commander 112/B/TC/TCA Maintenance Manual. Accomplished alteration to the elevators by replacing the right elevator spar and the left and right outboard elevator hinge fittings with Aerodyme PMA (44285-RE2 or 44285-RE2-SP) and associated installation items 44285-RE9 carrier plates, 44285-RE7 shims, and 44285-RE8 radius blocks in accordance with Aerodyme PMA Elevator Hinge Fitting Installation Instructions Doc. No. 44285-RE501-IM dated 15 April 2015.