N3534W - 1966 PIPER CHEROKEE 6/260
Aircraft Summary
General
Year
1966
Manufacturer
PIPER
Model
CHEROKEE 6/260
Serial Number
32-421
Registration #
N3534W
Condition
Used
Based at
Michigan
Description
1966 Piper Cherokee Six 260 - Excellent Cosmetics, Paint is super nice, 8372 Hours TTSN, Only 711 SMOH, Only 433 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, Only $119,500.
Airframe
Total Time
8372
Airframe Notes
INTERESTED IN FINANCING SOLUTIONS? Reach out to us for one-on-one personalized service. Attractive fixed rates with amortizations up to 20 years available. Low down payment options and customizable amortization schedules are also available.
Visit our website - www.BarteltAviation.com or www.PA32.com
Engine
Engine Manufacturer
LYCOMING
Engine Model
O-540-E4B5
Engine Serial Number
L-755-40
Engine Horsepower
260 HP
Engine Time
711
Engine Time Since
SMOH
Engine TBO
2000
Engine Notes
See Engine Overhaul Log Entry Dated September 29, 2006 for complete details.
433 Hours Since IRAN – (Due to Prop Strike ) - See Engine Log Entry dated October 1, 2011 for complete details.
Props
Prop Manufacturer
HARTZELL
Prop Model
HC-I3YR-1RF
Prop Time
433
Prop Time Since
SNEW
Number of Blades
3
Avionics
Avionics/Radios
• 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)
Additional Equipment
Additional Equipment
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
Exterior
Exterior Notes
• White Base Featuring Blue and Burgundy Accents.
• The aircraft is kept in a hangar when not flown.
• The Exterior Shows Well.
Interior
Number of Seats
6
Interior Notes
• 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.
Inspection Status
Inspection Status
ANNUAL DUE: February 1, 2026
BI-ANNUAL IFR (91.411 AND 91.413) CHECKS DUE: November 22, 2025
ELT BATTERY DUE: January of 2026
USEFUL LOAD: 1455.8 Pounds / (GW 3400 Pounds)
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).
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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