Consolidated Vultee BT-13A N93BT s/n 273

1995 Restoration



5000 Hours since new
1145 Hours Since Restoration (1995)


Pratt and Whitney R-985-AN1
500 Hours SMOH by Tulsa Aircraft Engines


Terra TX 760D Nav/Comm
Terra TRD 250D Transponder
Terra AT-3000 Encoder
AmeriKing 450 ELT


24 Volt System
2 Concorde RG25 Batteries-new 2018
Landing Lights and Strobe Light
Solid Tailwheel


350 SPOH, Hamilton Standard 2D30-6101A-12 Blades


Annual inspection completed August 2020
Current VFR Transponder inspection
Exhaust system overhauled 2002


US Army Paint Scheme, in Stits Poly Tone Paint (1995)


Black Cockpits-Stock Military Condition


Installed Pratt and Whitney R-985 Engine and Hamilton Standard 2D30-61A. Outboard wing panels to facilitate repair to center section (337), Removed rudder ailerons, elevators and wing flaps to facilitate recovering (337) Reinstalled wing center section, outboard wing panels and all control surfaces following repair. Removed both main and tail wheel landing gear assemblies. Cleaned assemblies, replaced all seals, inspected brakes, replaced all tires and reinstalled. Removed cleaned and inspected Brake Master Cylinders. Replaced all seals and reinstalled. Removed and replaced all aluminum tubing throughout the he aircraft. Removed and replaced all aircraft control cables, guides, fairleads and pulleys and tensioned to appropriate value., Installed two new Concorde RG25 batteries. Replaced call engine and flight instruments with overhauled units. Installed Hour meter and oil pressure switch, Hour meter indicates 0 hours. Cleaned, stripped and repainted the aircraft using Stitts Poly Tone paint. Aircraft lubricated throughout. Complied with AD 49-07-03 by installation of placard. Complied with AD 49-27-01 be installation of new fuel selector support bracket. Elevator Tubes modified as specified in TC Spec A-2-571.

All electrical wiring, cable ends, cable ties and fairleads were removed and replaced with new AN Milspec wire and electrical equipment. The aircraft electrical system was changed from 12 volt to 24 Volts. The electrical systems are the same in design. The Battery, Generator, Starter, Ignition Induction Vibrator and Light Bults were the only electrical units that required replacement. All wire sizers were in accordance with AAF Technical Order 01-50BB-2. New fairleads, ties and cable ends were installed. All wiring was accomplished in accordance with the aircraft wiring diagram and meets the requirements and standards. System was operationally checked satisfactory.

Aircraft located in Rockford IL. Contact Courtesy Aircraft to schedule a showing!