NORTH AMERICAN T-28C N28941 s/n: 140553
$399,000
Airframe:
9765 Hrs TTSNEW
Engine(s):
Curtiss-Wright R-1820-86B
765 Hrs SMOH by Precision Engines
Complete Firewall Forward in conjunction with Engine rebuild
Avionics:
Garmin SL-40 COMM
Garmin GA-35 WAAS
Garmin GTN-750XI Touch GPS/NAV/COMM
Garmin GNC-355A GPS/COMM (REAR)
Garmin GNC-355A GPS/COMM (FRONT)
GI-275 HSI (FRONT AND REAR)
(2) Garmin GI-275 (FRONT)
(2) Garmin GI-275 (REAR)
Garmin GFC-500 Autopilot
KR-22 Marker Beacon
King KN-69 DME
Stormscope
Garmin GTX-345D ADS-B Out Transponder
ELT 345
Equipment:
Large Nose Wheel Assembly
Pre-Oiler
Cleveland Brakes
Custom Seat Cushions
Oil Scavenge System
Dual Rotating Beacons
Smoke System-10 Gallon Tank
Oil Shut-off System with starter interlock
Whelen Strobes
New Poly Carbonite Windscreens
Hooker 5 point Harness system
Reiff Oil Tank and Cylinder Heater System
New Oxygen System
MX tracking logbooks in planelogix.com
All T-28 Maintenance Manuals from NATA included
Propeller(s):
Hamilton Standard 43D50 with Super B Blades
765 Hours SPOH, AD 81-13-06R2 next due 3/2024

Aircraft Profile:
Miscellaneous:
Annual Inspection Completed May 2022
VFR Transponder inspection completed July 2022
IFR Certified
Exterior:
Jet-Glo Navy Gray with White undersides in good condition, NATC (Naval Air Training Command) colors
Interior:
Total Restoration, Finished in Light Gray Epoxy in Excellent Condition
DETAILS OF RESTORATION:
General:
Aircraft Completely Disassembled
Aircraft Paint Stripped Inside and Out
All Wiring, Hardware, Brackets etc. Removed
Aircraft Inspected for Corrosion
Wings Rework and Overhaul:
Overhauled Fuel Cells and Tank Hardware Installed
All Flexible Fuel lines & Fittings Replaced with New
Aircraft completely Re-wired using all New Wire and Cannon plugs
Inboard Wing Attach Points and Joining Lugs Inspected for Cracks using DPI inspection method
Top Trailing Edge Skins and Trailing Edge Extrusion Replaced between Sta.28.2 to Sta.153.9
Leading Edge Skins Replaced Sta.28.8 to Sta.153.9 left and right hand
Wing Sections Joined together with New NDI, Inspected Bolts I.A.W. T.O. IT-28B-2
Fuel Quantity Senders and Computer Calibrated and Installed
Main Landing Gear and Hydraulic Components Overhauled and Installed
Fuselage:
Fuselage Primed Inside and Out
Fuselage Re-wired using all new Wiring and Cannon Plugs
All New Control Cables, Pulleys and Hardware Installed
Engine Control Push Rods Rebuilt and Installed using all New Hardware and Rod End Bearings
Tail Cone Mated to Fuselage Using New Attach Hardware
Vertical Stabilizer Installed
All Hydraulic Components Overhauled, Bench Tested and Installed
All Airframe Fluid Carrying Hoses Installed
Nose Gear and Components Overhauled, Painted and Installed
Wings Mated to Fuselage Using New Hardware per T.O. IT-28B-2
Bearings Replaced as Necessary
Flaps Reskinned and New Trailing Edge Extrusion Installed
Ailerons Painted and Balanced and Installed with New Hardware
Rudder Painted and Balanced and Installed with New Hardware
All Flight and Engine Controls Rigged per T.O. IT-28B-2
New Static Dischargers Installed
Aircraft located in Freeport, IL.
SPECIFICATIONS SUBJECT TO VERIFICATION UPON INSPECTION