1966 Piper Cherokee Six 260
| Overview | |||||||||||||||||||||||||||||
| 1966 Piper Cherokee Six 260 - Excellent Cosmetics, Paint is super nice, 8372 Hours TTSN, Only 710 SMOH, Only 431 Hours Since a 3-Blade Hartzell Simitar Propeller Upgrade, Brittain B5B Autopilot Featuring Altitude Hold, Deluxe PS Engineering PMA-450B Blue Tooth Audio Panel, Garmin 430W WAAS Approved GPS Navigator, King KX-155 Nav / Com, Dual Glideslope Presentation, Sky Beacon ADS-B Out Solution, Cargo Door, Davtron Digital OAT, Value Priced for Quick Sale! | |||||||||||||||||||||||||||||
| Price: |
$149,500 USD
Reduced by $10,000
(6.3%)
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| Offered By: | Bartelt Aviation | ||||||||||||||||||||||||||||
| Registration: | N3534W | ||||||||||||||||||||||||||||
| S/N: | 32-421 | ||||||||||||||||||||||||||||
| Location: |
Michigan United States 
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| Days Active: | 24 days ago | ||||||||||||||||||||||||||||
| Airframe | |||||||||||||||||||||||||||||
| USEFUL LOAD: 1455.8 Pounds / (GW 3400 Pounds) | |||||||||||||||||||||||||||||
| Total Time: | 8,372 Hours | ||||||||||||||||||||||||||||
| Avionics | |||||||||||||||||||||||||||||
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Brittain B5B Autopilot Featuring Altitude Hold – (No Guarantees) PS Engineering PMA-450B Blue Tooth Audio Panel / (5) Place Intercom Garmin 430W GPS / Com / NAV – (WAAS Approved) Garmin GI-106A VOR Indicator with Glideslope Garmin 396 – Panel Mounted Dock Station – (INOP) King KX-155 Nav / Com King KI-209 VOR / Glideslope Indicator King KT-76A Transponder Electric Trim – (INOP) Avionics Master Switch Pilot Push To Talk Switch Sky Beacon ADS-B Out Solution – (Wing Tip Mounted) |
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| Additional Equipment | |||||||||||||||||||||||||||||
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SUPER FEATURES / OPTIONS / MODIFICATIONS Cargo Door Skycraft Outboard Leading Edge Wing Landing Lights – (LH & RH) Wheel Pant Fairings Speed Enhancement Hartzell Simitar 3-Blade Constant Speed Propeller Featuring a Polished Spinner Upgraded Front and Rear Door Seals – (Aircraft Door Seals, LLC) Davtron M303 Digital OAT and Voltmeter Chrome Polished Fuel Caps Stand-By Vacuum System – (Manifold Type) Vertical FinTail Beacon Glove Box – (Panel Mounted) 84 Gallons Total Fuel Capacity Sky-Tec Light Weight Starter Cabin Cover for Transient Trips ADDITIONAL OUTSTANDING FEATURES Pilot Toe Brakes, and Parking Brake Pilot / Co-Pilot Sun Visors Overhead Cockpit Map Lights - (2) Windshield Defrosters & Control Tie Down Rings 12” Registration Numbers CHT / EGT Gauge Pitot Heat ELT Pilot Vent Window |
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| Engines & Props | |||||||||||||||||||||||||||||
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Engine Engine 1 Make/Model - LYCOMING Engine Horsepower - 260 HP Engine TBO - 2,000 Engine Notes The engine overhaul was performed by Pacific Continental - (See Log Entry 12/8/1989) 433 Hours Since IRAN – (Due to Prop Strike – See Log Entry 10/01/2011) |
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| Engine Hours: | 710 SMOH | ||||||||||||||||||||||||||||
| Interior & Exterior | |||||||||||||||||||||||||||||
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Number of Seats - 6 Burgundy Tweed Executive Seating Featuring Harmonizing Side Panels. Burgundy Carpeting. (6) Place Interior – (Forward Seating Configuration) The Pilot and Co-Pilot Adjustable Seats Individual Headrest for each seat Overhead Fresh Air Vents – (6) The Interior Shows Well. |
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White Base Featuring Blue and Burgundy Accents. The aircraft is kept in a hangar when not flown. The Exterior Shows Well. |
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| Other Info | |||||||||||||||||||||||||||||
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Inspection Status: ANNUAL DUE: February 1, 2025 BI-ANNUAL IFR (91.411 AND 91.413) CHECKS DUE: November 22, 2025 ELT BATTERY DUE: January of 2026 NOTATIONS October 9, 1990 (No Log Entry) – The left wing skins were repaired with seven 2 ¾ x 3/14 patch plate aluminum repairs. (Most likely due due common wing skin cracks). See FAA 337 Dated October 9, 1990 for details. November 9, 2011 (Tach 1527.0) – The aircraft was involved in a prop strike incident. Repairs were made to the aircraft. The firewall also required repair. An IRAN was performed on the engine by Custom Airmotive. March 5, 2016 (Tach 1816.2) – Piper SB 1006 was performed on the right wing. The wing was also removed and reinstalled after spar replacement and repairs were performed by Airframe Components by Williams (WO 17752 and yellow tag dated February 17, 2016). October 4, 2021 (Tach 1899.6) – AD 20-24-05 IAW SB 1404A was completed. The mechanic also replaced rivets on top skin of forward upper wing spar at WS 08-WS 27. October 4, 2021 (Tach 1899.6) – AD 2026-16 IAW SB 1345 was CW. Nondestructive testing completed by Tailwind Inspection Inc (FAA CRS: T0WR995N). |
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| Aircraft Documents | |||||||||||||||||||||||||||||
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