1956 180

Avionics/Radios

• Garmin 296 GPS
• Collins AMR-350 Audio Panel with 3 Light Marker Beacons
• King KX-155 Nav / Com – (#1)
• King KI-209 VOR / Glideslope Indicator – (#1)
• King KX-155 Nav / Com – (#2)
• King KI-209 VOR / Glideslope Indicator – (#2)
• King KR-86 ADF
• King KN-64 DME Featuring Nav 1 and Nav 2 Switching
• King KT-76A
• Sigtronics SPA-400 Four Place Intercom System
• Dual Push To Talk Switches
• Electronics International Digital EGT
• Electronics International C-6 Digital CHT – (6-Position)
• Custom Metal Avionics Panel


Additional Equipment

• Flint Aero 12 Gallon Aux Fuel Tanks – (An additional 24 gallons of fuel)
• Fuel Capacity – (80 Gallons)
• BAS, Inc. Tail Pull Handle Upgrade – (STC SA3812NM)
• Madras Air “Super Tips” Wing Tip Upgrade – (STC SA1943WE)
• Aero-Trim – (Aileron Trim System / STC SA1296SO)
• Tanis Engine Pre-Heater – (Oil Pan Mounted)
• Flap Gap Seals Speed Enhancement – (Aircraft Development STC SA1493CE)
• Aileron Gap Seals Speed Enhancement – (Aircraft Development STC SA1493CE)
• Concord Battery
• Whelen HR-14 Strobe – (Mounted on Vertical Fin)
• Vertical Card Compass
• Brackett Air Filter – (STC SA71GL)
• 60 AMP Alternator Upgrade
• Center Line Camera Kit Provisions – (Currently there is an inspection plate installed)
• Nav / Position Lights – (Tail & Wing Tips)
• Landing Light
• Outside Air Temperature Gauge
• Heated Pitot Tube Upgrade – (12/5/1990)


Exterior Notes

• Beige Base featuring Brown and Blue Accents
• The aircraft is kept in a hangar when not flown.
• The exterior shows well.


Interior Notes

• Brown Tweed Fabric Seating featuring Harmonizing Side Panels.
• The interior appearance shows well.
• Map Light – (Overhead and Pilot Side Pillar Post Mounted)
• Sun Visors – (Pilot & Co-Pilot)
• Instrument Panel Post Lights


Inspection Status

ANNUAL DUE: October 1, 2026

BI-ANNUAL IFR CHECKS DUE: May 27, 2027

ELT BATTERY DUE: August 2025

ADDITIONAL INFORMATION

• The aircraft does not currently have an ADS-B solution installed.

• There is an airframe log entry dated August 16, 1956 the describes some repairs most likely caused by an incident. Please review the log book for details.

• The rudder was replaced with a serviceable unit due to skin cracks. See airframe log book entry dated January 24, 1988.

• Engine Model 0-470K, s/n 47347-6-k was removed. An overhauled Continental 0-470-RCS engine s/n 133534-6-R was installed by Robert Mukenschnabl via field approval. See FAA 337 dated October 10, 1989 and log entries for complete details. The engine was overhauled and converted to an S Model by Technical Airmotive per TCM SB M75-13R1. See engine log book entry by Technical Airmotive dated July 5, 1989 for details.

• RH Engine Mount was repaired with a sleeve reinforcement. See FAA 337 dated October 10, 1989 for complete details.

• The firewall had two cracks repaired with doubler patches. See FAA 337 dated July 10, 2007. for complete details.

• The forward dorsal fin was repaired. See FAA 337 dated March 18, 2010 for complete details.

• The LH aileron was repaired. See FAA 337 dated August 12, 2011 for complete details.

Specifications are Subject to Verification upon the Buyer’s Inspection of the Aircraft. Optional aircraft transition flight training solutions are available. We accept trades and offer a variety of low fixed rate interest rate financing solutions up to 20 years.

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