N611WP - 1952 BEECHCRAFT C45H

1952

BEECHCRAFT

C45H

N611WP

AF-875

Used

MN

4863

Only 80 Hours SMOH on Both Engines! Nice Avionics Package, Executive Interior- Ready to Go!

4,863 Hours TTSNEW

Pratt & Whitney R-985 AN-14B Left: 80 hrs SMOH by Covington Engines-2023 Right: 80 hrs SMOH by Covington Engines-2023 Over $200,000 spent on FWF restoration

2 Blade Hamilton Standard 22D30 Left: 1425 Hrs. SPOH AD 81-13-06 R2, completed 3-2026 Right: 1425 Hrs. SPOH AD 81-13-06 R2, completed 3-2026

Yes

Garmin GTN-650 GPS/COM/NAV Garmin GA-35 GPS WAAS Antenna Garmin GI 106A King KX-155A NAV/COM King KMA-24 Audio Garmin GTX-330 Transponder King KT-76A Transponder Century 3 coupled Autopilot Dual Glideslopes WX-8 Stormscope

External Baggage Door All Metal control surfaces Amsafe Seat Belts Airwolf Oil Filters Aerospace Products Spar Kit Engine Sump Drain Kits Shadin Digital Fuel Flow computer Dual panels with 3” gyros All New/ Overhauled Exhaust System Parts All New Hoses Firewall Forward Gill GE-51C 24 Volt Batteries Dual EGT Mirrored Aft cabin bulkhead HISTORY The aircraft was overhauled and converted to C-45H by the Beech Aircraft Factory in the early 50’s for use by the the USAF and operated as a military transport aircraft until release from service and entry into the civilian market in 1961. After extensive updates the aircraft was issued a standard category Airworthiness Certificate. Updates included- Hamilton Certification Kit-STC SA-442 Extended Tailwheel E-18S wingtips Wrap Around windshield Streamlined nose Stabilizer Angle of Incidence Kit Standard cabin windows Hamilton Air Stair door Outside Baggage Door 2-37 Gallon outer wing fuel tanks (6 total tanks) Custom Interior with reclining seats Accordion Cockpit door Late model crew seats Overhead cabin lighting EXTRA ITEMS INCLUDED Extra Top Cowlings, Hot Temperature Modification Spare Main Tires and Tailwheel Tire Extra Windscreen Many Misc. Extra Small Parts Maintenance Manuals

Polished Silver Fuselage with Red Stripes

Six Passenger Executive Interior with tables

Logbooks back to 1961, when it was acquired from the USAF Annual Inspection completed in March 2026 All AD’s in compliance Wing Strap inspection due at 6203 total time Max gross weight: 8750 New empty weight: 6684.67 New useful load: 2065.33