Piper
Sale price: US $26,000.00 Make an Offer
| Condition: | Used | Make: | Piper |
| Model Year: | 1961 |
Tyler, Texas, United States
Vehicle description
1961 PIPER COMANCHE 250 N7429P PA24-250 S/N: 24-2617 Engine: Lycoming 0-540 AID5 S/N: L-3996-40 Engine TT: 3075.9 TTAF: 4252.9 TSMOH: (TOP): 429.53 (BOT): 1801.9 Certificate of Airworthiness issued: 3/16/1961 by Mr. J.W. McNary, Piper Aircraft Corporation Aircraft Re-Painted in 1977: 817 U White, 48 UH Red, 99 U Black Main Aircraft Logbook #1 Last Entry: Oct. 21, 1977. Moved to Logbook #2. Auto Pilot System removed in June 1977 FAA reports: 04-24-1978 - fuel exhaustion leading to a forced landing with damage Repairs accomplished at Decatur Aviation, Decatur, IL. 6/20/1979 TTAF: 1244.94 FAA 337 dated 5/5/79 & FAA 337 dated 6/20/79 on file 6/1/1979 - AD 74-13-03 – Stabilator Bolts – New Bolts installed Terminating Action of the AD. TTAF: 1233 7/14/1981 – Engine Overhaul accomplished at G&N Aircraft, Griffith, IA. TTAF: 2451.37 5/19/1993 – AD 77-13-21 1,000 hr inspection C/W at TTAF: 3435.8. Next Due at 4435.8 Currently due in 182.9 hrs. 1/04/2001 – Engine TOP O/H Completed at G&N Aircraft, Griffith, IA. ETT: 2646.37 TTAF: 4252.9 TSMOH: TOP: 0 / BOT: 1372.37 FAA reports: 03-27-2009 a gear-up landing and prop strike 9/14/09 - Prop O/H by Sensenich Propellor Service, Gainesville, GA. Prop S/N: A557621 / A57945 Engine Teardown and Inspection performed by Fred Lawshe – FAA IA 1891599 – Pearl River, LA. 12/2010 – New NLG Motor installed 2011 - AIRCRAFT SOLD TO JAMES BARRY BARNETT BY FRED LAWSHE (FAA IA1891599) 2/27/2012 – New Battery installed on Aircraft 6/25/2012 – Replaced ELT Battery, Interior and Baggage Compartment Refurbished 7/12/2012 – Replaced Left MLG Tire and Installed New Sky-Tec Starter Model # 149-NL. 11/15/12 – TTAF: 4200.9 - Replaced both landing lights, Left and Right I/B Fuel Tank Caps, C/W AD77-13-21 by removal and replacement of Bungee Cords 11/1/14 – AD97-18-02 R1 – C/W 5 year inspection on Prop. All work performed IAW Hartzell Specifications. 11/1/14 – 91.411 & 91.413 C/W by Hartzell Aviation TTAF: 4252.9 9/15/2015 – C/W following Airworthiness Directives: AD 77-13-21 – Removed and Replaced Bungee Cords AD 68-13-03 – Fuel Cell Inspections AD 68-05-01 - Ref Para “F” – Exhaust AD 76-07-12 – Switch Op Ck AD 79-20-10 – IAW Piper SL 850 AD 97-01-01 R1 - MLG Brace Studs By Insp
9/5/2016 – The Following Discrepancies were found and corrected during Annual Inspection:
NLG Tire will not hold Pressure: Corrective Action: Replaced NLG tire with new tire. Main Ship Battery Will Not Hold Charge: Corrective Action: Replaced Battery with New Gill Battery RMLG Strut will not hold Pressure: Corrective Action: Replaced Strut Valve: Leak Ck Good. Removed and Replaced All Nav Light Bulbs and rewired worn wing tip ground wires. Pitot Tube Clogged – Blew Out Obstruction in tube. Engine Oil drained and changed adding 10 qts of Aeroshell 10W-50. Fuel Strainer clogged and Gasket worn and Leaking. Cleaned debris and drained and sumped all tanks. Installed new gasket. Leak Ck Good. AD 68-05-01 – Exhaust Mufflers – C/W AD 68-13-03 – Fuel Cells – C/W AD 75-12-06 - Fin Forward Spar – C/W AD 76-07-12 – Bendix Switches – C/W AD 77-13-21 – Bungee Cords by Inspection – C/W AD 79-20-10 – Aileron Nose Rib – By Inspection – C/W All Flight Controls and Pulleys cleaned and Lubed IAW Piper Service Manual. 9/9/2016 – Annual Signed off by David Bogar IA 455216543. All discrepancies C/W. FAA AIRWORTHINESS DIRECTIVE UPDATE: 77-13-21 – 1,000 hour inspection next due in 182.9 hours (TTAF: 4435.8) 97-01-01 R1 – Main Landing Gear Collapse next due 482.1 hours (TTAF: 4735.7) 2012-17-06 – Stabilator Horn Assembly - TTAF at time of Effective Date was TTAF: 4200.9. AD Compliance Time is TTAF: 4300.9.
9/5/2016 – The Following Discrepancies were found and corrected during Annual Inspection:
NLG Tire will not hold Pressure: Corrective Action: Replaced NLG tire with new tire. Main Ship Battery Will Not Hold Charge: Corrective Action: Replaced Battery with New Gill Battery RMLG Strut will not hold Pressure: Corrective Action: Replaced Strut Valve: Leak Ck Good. Removed and Replaced All Nav Light Bulbs and rewired worn wing tip ground wires. Pitot Tube Clogged – Blew Out Obstruction in tube. Engine Oil drained and changed adding 10 qts of Aeroshell 10W-50. Fuel Strainer clogged and Gasket worn and Leaking. Cleaned debris and drained and sumped all tanks. Installed new gasket. Leak Ck Good. AD 68-05-01 – Exhaust Mufflers – C/W AD 68-13-03 – Fuel Cells – C/W AD 75-12-06 - Fin Forward Spar – C/W AD 76-07-12 – Bendix Switches – C/W AD 77-13-21 – Bungee Cords by Inspection – C/W AD 79-20-10 – Aileron Nose Rib – By Inspection – C/W All Flight Controls and Pulleys cleaned and Lubed IAW Piper Service Manual. 9/9/2016 – Annual Signed off by David Bogar IA 455216543. All discrepancies C/W. FAA AIRWORTHINESS DIRECTIVE UPDATE: 77-13-21 – 1,000 hour inspection next due in 182.9 hours (TTAF: 4435.8) 97-01-01 R1 – Main Landing Gear Collapse next due 482.1 hours (TTAF: 4735.7) 2012-17-06 – Stabilator Horn Assembly - TTAF at time of Effective Date was TTAF: 4200.9. AD Compliance Time is TTAF: 4300.9.