Aircraft > Single-Engine Piston > Aero > N220EX: Aero Comp 6
N220EX: Aero Comp 6
Last Updated
Feb. 13, 2023
Details
Registration #
N220EX
Status
Off Market
Year
2010
Make
Aero
Model
Comp 6
Serial Number
97143
TTAF
141
Engine 1 Time
141
Location
Florida, United States
Price History
Feb. 7, 2023
75,000
Listings
Site
Price
Status
Updated
Description
2010 Aero Comp 6, 141TT, Audio panel PS Engineering Model PMA6000M with Intercom, Nav/Com King Model KX-155 with KI-209 Indicator, Transponder King Model KT-76A with AK 350 altitude sensor, GPS Garmin Model GNS-496, ADS-B In/Out uAvionix Model echoUAT, Heated Pitot, Always hangared, US Registered, All Logs/Manuals, No Damage History.
Avionics
Audio panel PS Engineering Model PMA6000M with Intercom Nav/Com King Model KX-155 with KI-209 Indicator Transponder King Model KT-76A with AK 350 altitude sensor GPS Garmin Model GNS-496 (panel mounted, removable) ADS-B In/Out uAvionix Model echoUAT (operates with Foreflight) ELT Airtex Model ME406 (121.5 & 406 Mhz) REMARKS Engine analyzer Insight Model GEM 602 CHT & EGT monitor Attitude indicator RC Allen Model RCA26AK4 * Directional gyro RC Allen Model RCA15AK2 * Turn coordinator RC Allen Model RCA82A11 * RPM, w/Hobbs UMA Model 9-801-10 Manifold pressure UMA Model 7-260-35 Oil pressure UMA Model 4-210-080 Oil temperature UMA Model 12-200-250F Voltage UMA Model 14-100-15 Amps UMA Model 15-100-60 Clock/Timer Electronics Intl Model SC-5 super clock Fuel gauge (dual) Electronics Intl Model FL-2RA-12 NAV/Strobe lights Whelen Model A600PG/PR wingtip assemblies Landing light Engine has not been modified in any way and is still a certified engine. External oil filter Dual oil coolers (no problems on hot Florida summer days) All oil lines braided stainless steel Aeroquip The main wheels have been upgraded to Grove wheels with dual disc brakes and 8:00 6 tires. The tail wheel has been upgraded to a Model ABI-3224A Alaska Bushwheel with an 8″ tire. Paint on top of cowl needs Repainting. Heated Pitot Always hangared US Registered All Logs, Manuals 23 Square, 120 MPH at 12 GPH These gyro instruments are electrically powered. There is no failure prone vaccum pump. Rather, there is a secondary battery behind the rear seat. A switch on the instrument panel enables this battery to be connected to an “essential buss.” This buss powers the following: Nay/Corn, audio panel, transponder, attitude indicator, turn coordinator, altitude encoder, and trim. In the event of a failure of both the main battery and the alternator, this back up battery should power these essential instruments long enough to get the airplane safely on the ground. There is a voltmeter to indicate the charge of the back up battery. The instruments have light ring bezels, with a dimmer. There is an overhead cabin light and a red/white spotlight. There is a speaker for nay/com audio. There are jacks for passenger headsets. There is also a jack to allow a hand held radio to be connected to the airplanes built in antennas. There is a firewall vent for cabin air and/or heat. There are fresh air vents in the wing roots. A fuel shutoff valve is available in each wing root. All electrical items are protected with fuses, not breakers. Trim is controllable both from switches on the instrument panel and on the yoke grip. There is a push-to-talk switch on the grip. Note that all electrical connections from the engine compartment to the cabin are via military style (MS) connectors. The entire instrument panel my be removed as a complete assembly if necessary. A schematic drawing of all electrical wiring is available. Extensive documentation is available including factory manuals, build notes, photographs, receipts, etc. Specifications Length 24.5′ Wingspan 35′ Height 8′ Cabin width 46″ Cabin height 53″ Wing area 212 sq ft Empty weight 2100 lbs Gross weight 3200 lbs Fuel capacity 88 gal
Airframe
AIRFRAME Total Airframe Time: 141 Hours
Engines / Mods
Engine Time: Lycoming 0-540-E485 260HP (overhauled Aug 1996) Prop: 141 SNEW Hartzell (Model HC-C2YR-1BF 2-blade constant speed Aug 1996)
Interior / Exterior
4 Gray Seats, sprayed with Zolotone, not upholstered Rated “8” White/Gray with Gold Trim (see remarks) Rated “8”
Remarks
REMARKS Engine analyzer Insight Model GEM 602 CHT & EGT monitor Attitude indicator RC Allen Model RCA26AK4 * Directional gyro RC Allen Model RCA15AK2 * Turn coordinator RC Allen Model RCA82A11 * RPM, w/Hobbs UMA Model 9-801-10 Manifold pressure UMA Model 7-260-35 Oil pressure UMA Model 4-210-080 Oil temperature UMA Model 12-200-250F Voltage UMA Model 14-100-15 Amps UMA Model 15-100-60 Clock/Timer Electronics Intl Model SC-5 super clock Fuel gauge (dual) Electronics Intl Model FL-2RA-12 NAV/Strobe lights Whelen Model A600PG/PR wingtip assemblies Landing light Engine has not been modified in any way and is still a certified engine. External oil filter Dual oil coolers (no problems on hot Florida summer days) All oil lines braided stainless steel Aeroquip The main wheels have been upgraded to Grove wheels with dual disc brakes and 8:00 6 tires. The tail wheel has been upgraded to a Model ABI-3224A Alaska Bushwheel with an 8″ tire. Paint on top of cowl needs Repainting. Heated Pitot Always hangared US Registered All Logs, Manuals No Damage History 23 Square, 120 MPH at 12 GPH These gyro instruments are electrically powered. There is no failure prone vaccum pump. Rather, there is a secondary battery behind the rear seat. A switch on the instrument panel enables this battery to be connected to an “essential buss.” This buss powers the following: Nay/Corn, audio panel, transponder, attitude indicator, turn coordinator, altitude encoder, and trim. In the event of a failure of both the main battery and the alternator, this back up battery should power these essential instruments long enough to get the airplane safely on the ground. There is a voltmeter to indicate the charge of the back up battery. The instruments have light ring bezels, with a dimmer. There is an overhead cabin light and a red/white spotlight. There is a speaker for nay/com audio. There are jacks for passenger headsets. There is also a jack to allow a hand held radio to be connected to the airplanes built in antennas. There is a firewall vent for cabin air and/or heat. There are fresh air vents in the wing roots. A fuel shutoff valve is available in each wing root. All electrical items are protected with fuses, not breakers. Trim is controllable both from switches on the instrument panel and on the yoke grip. There is a push-to-talk switch on the grip. Note that all electrical connections from the engine compartment to the cabin are via military style (MS) connectors. The entire instrument panel my be removed as a complete assembly if necessary. A schematic drawing of all electrical wiring is available. Extensive documentation is available including factory manuals, build notes, photographs, receipts, etc. SPECIFICATIONS Length 24.5′ Wingspan 35′ Height 8′ Cabin width 46″ Cabin height 53″ Wing area 212 sq ft Empty weight 2100 lbs Gross weight 3200 lbs Fuel capacity 88 gal All Specifications Subject To Verification Upon Inspection.