Front door to the main fuse board in the cockpit, labeled A 14 to 20, the rest is for corroded to be readable, was removed from the area below the pilot's legs, on the port side.
The hydraulic control device for flaps were removed from their place down between the ribs 3a- 4, on the starboard side.
This was fitted with a front cover, with a sign that has contained an operation description.
A hydraulic pipes that was routed down to the wire gate, and further backwards to the hydraulic control device for flaps, was also dismantled
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. Reaching this tube connected to a nipple that went forward through the frame 1.
Bakelite bracket, for guiding the wire and piano wire, was removed from the area behind the hydraulic control device for flaps.
The rear part of the lid, and rubber seal for a hydraulic tank were dismantled from the mid rib 1, on the starboard side.
Rings with associated gasket for review of Hot air, starboard exhaust manifold, cockpit section was dismantled area between the ribs 5- 6.
Plexiglass window with associated printing plates were disassembled down on the starboard side between the frames I- II.
The following minor components were also taken off the plane:
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and hydraulikkrør, end attachments, were disengaged behind the wing root. The pipe was routed forward down the starboard side, past the hand pump flap, and further forward to frame 3a.
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a hitch, with associated bakelite plate, for pilot Revisikte was dismantled atop, between the ribs 2- 3.
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Lower attachment of the pilot's instrument tray was removed from its location above the starboard side of the frame 2.
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A cover that has protected a pulley which has passed a wire through ribs 1 was dismantled down on the starboard side.