1943 Beechcraft G17S Staggerwing

Airframe Overhaul 21/07/2001 by Edward L. Gann

Disassembled aircraft,removed fabric covering and inspected all major components. Prop removed for OH by Precision Propeller. Engine removed for OH by Covington Aircraft Engines Inc. Tubular airframe stripped, inspected, primed with two coats DP50 epoxy primer, and painted with two coats PPG Durethan-II white. The airframe was then reassembled using all new wood, wiring, circuit breakers and switches, instruments, radios, new windshields, new interior and new Ceconite 101 fabric covering IAW AAR Cooper Aviation STC SA1657GL and System II finish. New battery installed. Control surfaces rigged for proper operation and deflection and turnbuckles safetied. Landing gear doors adjusted and retraction test performed. Flying and landing wire rigged. New seatbelts installed for all seats, new shoulder restraints installed for pilot and co-pilot seats.New interior installed using approved aircraft fabric. Fuel system checked for proper operation and leaks. Engine oil system checked using installed engine pre-oiler. Electrical system and alternator checked for proper operation during engine run. New Cleveland wheels and brakes checked during engine run-up. Aircraft weighed with all equipement in place and full oil. New equipment list prepared and added to aircraft records. FAA form 337's filed for all special equipment, radios and auto-pilot system installed. Complete details of all work performed may be found in aircraft records on AERO J CORP WORK ORDER NO 484011994. AD's checked through T-DATA Rev.2001-12.