Report Date: May 1, 2005
Report No: 3
The New England Air Museum (NEAM) preservation effort is aimed at preventing or slowing the deterioration of outside display aircraft. The A-26C preservation effort was started in November 2003. The main preservation plan focuses on external aircraft surfaces and component repairs, tires, corrosion inhibition, painting and preparing the aircraft for public viewing. A parallel effort is focused on adding to the current NEAM historical records of the aircraft and crew during its World War II service.
The NEAM A-26C (43-22499) was built by Douglas Aircraft Company in Tulsa, Oklahoma in 1944 and delivered to the 416th BG (L), 671st BS in November 1944 while the unit was stationed in Melun, France. Jack Buskirk, a pilot on the aircraft, visited the museum in 1994. Photos and other documents show our aircraft flew with the name “Reida Rae”. The aircraft was named for the wife of Ground Crew Chief Raymond Rohrdanz. The following people are known to have flown or maintained the aircraft during 1944-45.
· John (Jack) A. Buskirk, Pilot
·
Robert
C. Hanna, Bombardier/Navigator
· C. Houston Corbitt, Engineer/Gunner
· Claude J. Brown, Pilot
· James E. Kerns, Bombardier/Navigator
· Herbert E. Sunderland, Engineer/Gunner
· Raymond R. Rohrdanz, Ground Crew Chief
· Hartzell O. Stephens, Ground Crew
· Elton R. Olmstead, Ground Crew
Buskirk, Hanna and Corbitt also flew the A-26C, “Disagreeable 4” shown in the progress report header. The NEAM aircraft was struck off US Air Force inventory in 1957 and the aircraft was used commercially until the late 1960’s. The NEAM acquired the aircraft from the City of Bridgeport, CT in August 1971.
General
· Three wheel stands were designed and build. They are designed to hold the aircraft several inches off the ground to eliminate flats, save tire material and to provide a means for eventually lagging the aircraft to concrete slabs.
· The aircraft was mounted on the stands.
· Plugs were placed in the oil cooler inlets in the wing leading edge to prevent future bird nesting.
· Painting of the front 1/3 of both engines was completed.
· The rear portions of the engines were spayed with a corrosion inhibitor.
· Two large corroded holes on the left engine cowl were cut out and patched with sheet metal.
· The left engine cowl was re-installed. The right engine cowl was left off while preparation is made to fix the right nacelle corrosion.
· Plugs were place in the air inlet openings to prevent future bird nesting when the aircraft is outside.
· The word “Bootie” was painted on the outside of the left nacelle. Bootie was the nickname of Hartzell O. Stephens’ wife.
· The right side of the right engine nacelle has a skin corrosion hole of about 1 square foot. The right main 300 gallon fuel tank must be removed in order to get access to the corroded panel from the inside. This is necessary so that repair rivets can be bucked from the inside.
· The right wing was shored up to remove all weight from the right main landing gear.
· The fuselage, just aft of the gunner compartment, was shored up to prevent any sideways motion of the aircraft while the nacelle sheet metal work is done.
· As of May 1, most stress panels and fuel tank connections were removed. The fuel tank should be removed in May or early June and work can proceed on replacing the corroded nacelle structural panel and, possibly, some damaged nacelle longitudinal stringers.
· A new loop antenna was installed behind the gunner compartment.
Flaps
· Inboard and outboard flaps were removed. Linkages and bearing were freed up. Exposed aluminum surfaces were corrosion inhibited and painted, where appropriate.
· Several flap linkage straps were completely corroded. The machine shop fabricated replacements.
· Heavy surface oxidation was removed and the surfaces treated with protective coatings.
· Gear boxes were greased and the flap actuation tube bushings were corrosion inhibited with lubricating penetrant.
· The flap wing wells were sprayed with corrosion prevention sprays.
· The right and left inboard and outboard flaps were re-installed and the flap system was actuated to ensure non-binding operation.
· Work was started to prepare the rudder, elevators and ailerons for fabric covering. Some of the access panels on the surfaces had missing or damaged nut plates. In some cases, access panels were missing. New nut strips with the proper spacing could not be located, so fabrication procedures were devised for making new nut strips and these procedures were applied successfully to the rudder refurbishment. When all nut plates and nut strips are re-installed in all the empennage and all missing access panels fabricated, fabric covering will commence.