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We now have so much experience with turning out windows, that we this day got loose most of the remaining plexiglass windows on the port side:

• Window – lower – foremost- spun In- II.

• Window – On top – foremost- spun In- II.

• Window – top center- spun In- III.

• Window – lower – rear- spun In- III.

• Window – On top – rear- spant III- IV.

It was also used a lot of time to stick on plastic signs, and describing and photographing mains street extending along the port side.

A part of the main conduit street along the aircraft port side of the cockpit and the nosepiece

The following components were separated and described:

• Breaking (main switch) connected to mains street by spun III.

• Hann Contact for review ahead of spun V. The contact is terminated on the vertical terminal block in frame 2 and are labeled V 30.

• Hunn Contact for review ahead of spun V. The connector is connected to the large terminal block directly behind the ribs 1, and is labeled L-12.

• Contact which are screwed out to the left on the front of the frame V, and are labeled V 40. The wiring from this connector is progressing in mains street. The contact point backwards.

• Switching point / contact with blind plug which is connected to mains street, like ved spant IV
  . Directly above is checked C12 / 11.

• Push button between spun II- III, which is connected to mains gate

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  . The conduit is attached with 2 clip.

One of many switch boxes in the cockpit and nose section

• The remnants of a lamp connected to mains street by spun IV.

• The male connector review backward spun V on the port side. It is marked L 11. The wires from the connector is part of the main line street ahead.

• Terminal block between frames IV- V. The wires of this pass upwardly through spun IV and rearward and down to the lower terminal between ribs 1 – 2. From below, a line straight down and a conduit opening in the main conduit street.

• have contact, labeled V 29, for implementing backward spun V. The contact wires are terminated in terminal block in frame V.

Female connectors labeled V 29

• Hann Contact, labeled V 14, for reviewing spun V of the front. The contact is terminated in terminal block in frame V.

• Lower female connector, labeled V 39, for review from the rear of the frame V. It is terminated in the lower large terminal block behind spunky 1.

• have contact, labeled V 15, is mounted on the back of the frame V, and review the future. The contact was linked to the large terminal block behind spunky 1.

• Switch box terminated in terminal block in frame V.

• Internal contact, for the external temperature sensor, between the ribs 1- 2. It is terminated in the upper terminal between ribs 1 – 2.

• Box having contained two push-button switches, with red indicator. The box is placed between the ribs 2- 3.

• Bosch horn / audible alarm which is located upstairs in front of the pilot's instrument panel.

• Switch m / hatch is placed between the ribs 1- 2, behind the main line street. The mounting bracket is the C-5.

• Switch box terminated in terminal block in frame V.

• Switch placed right up between the ribs 3- 4. It is marked C65 on the track directly behind the switch. The wires to and from this goes back to- and through ribs 4.

• fuse / switch which is arranged in front frame 3a. The wires to and from this goes through this rib.

• Lamp that is mounted on a bracket, nailed in the outer panel between the ribs 3- 3a. On the rail directly above the lamp is marked R 66.

• Press- button that is screwed up between the ribs 3- 3a, next to the pilot's position. It is labeled H 4 on rail, right behind the switch.

  

  Press button next to the port side of the canopy

It was currently working to dismantle parts in many different places in the navigator and cockpit section.

Motor which has operated a pulley, ( this memory of an old speedometer wire similar to those that were previously in use in vehicles ) was dismantled.

Motor standing mounted directly behind the pilot's instrument panel

This engine was located upstairs on the port side, directly in front of the pilot's instrument panel, behind spunky 1
. Stir with wire inside branched off at the front of the frame 1 and forward to frame IV
. It is a 90 degree angle to the pipe with the wire in the
. Inside this angle sits two 45 degree gear that extends force on the wire down.

Motor and pulley

Electrical junction box that is labeled B17 / B18 was dismantled from the frame 6 up on the port side

Bakelittbraketter / pipe penetrations, who has served as supports for pipes that have gone out of wings, was dismantled

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. These were placed passages on both sides of the plane up front ribs 6.

Tanks and pumps were used for priming of the motors before startup, was dismantled. This equipment was placed on the starboard side, in height in the middle of, between the ribs 2- 3.

Pump priming of the motors before start

Disassembled support for hydraulic tank, with associated fixing bracket for pipes
. The tank has been placed on the starboard side, in height in the middle of, the spunky 1. Simultaneously, also attached to the hydraulic tank dismantled. This consisted of upper and lower bracket with steel bands between.

It was also currently working with unscrewing plexiglass routes. The following windows were dismantled:

• The upper front window on the starboard side, behind spunky In.

• The upper window behind spun II starboard.

• The bottom window behind spun II starboard.

• The upper window behind spun III, on the starboard side.

Unfortunately, we find a lot of salt between the glass and the frame around them, but steel structures behind the glasses is in good condition.

Throttle casing shall be stored dry during the summer, and was greased thoroughly with Lanolin to minimize the risk of further damage.

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.

Equipment for hydraulically lowering or raising of the flap

This was fitted with a front cover, with a sign that has contained an operation description.

Signs that stood mounted on the device
. The picture was taken just after the rise in June 2012

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.

Part of the hydraulic tank that stood mounted on the frame 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.

The hole, between ribs 5- 6, where hot air pipe, from port exhaust manifold, came into the cockpit.

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:

• 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.

• a hitch, with associated bakelite plate, for pilot Revisikte was dismantled atop, between the ribs 2- 3.

• Lower attachment of the pilot's instrument tray was removed from its location above the starboard side of the frame 2.

• A cover that has protected a pulley which has passed a wire through ribs 1 was dismantled down on the starboard side.

A hydraulic opening and closing valve bomb slots, with the bracket, was dismantled down on the starboard side of spun II
. The bracket is complete, but lacks the data plate and has a little rust
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Hydraulic valve for operating the bomb slots bomb sifter had at its right hand right up to the spun II

A plant for the emergency operation of the flaps were removed from the starboard side, between the ribs 3- 4. This consisted of a manual hydraulic pump, which was operated by means of a long handle.

A bracket was removed from the starboard side of the roof between spun II- III
. The bracket has painted text; holder, Bordtasche M.G

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a cover / cap having covered electrical components / conduit street was removed from the wall behind the ribs 1, on the port side.

The following minor components were also taken off the plane:

• A tie with a powered on tube was disassembled down the side of the port side of frame 1.

• A cover and a lid which has been over an electrical component was dismantled down on the port side of frame 1.

• A cover over some pulleys implementation of spunky 1, was dismantled down on the starboard side.

• Some parts of the contact on the starboard side were dismantled up behind ribs 1.

The plane has had a system in emergencies to dump fuel. We dismantled today the manual part of the system

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. A long vertical handle was attached to the same bracket, as control valves for hydraulic flaps control, located on the starboard side between the frames 3a- 4. This gave the pilot the opportunity to start a pumping fuel. Lever is part of a larger manually Arrangement, who ended up behind the ribs 5- 6. Here was this connected to a plate, in which the position is monitored by a limit switch
. From this it is routed wires backwards in direction to an electric pump for pumping fuel.

Equipment for the operation of the system for emergency dumping of fuel

A close window at the top right behind the rib was unclamped and removed.

Pilote control panel points Brett, with the bracket and a roller, was removed from between the ribs 2- 3a. It was also found a pipe lying behind the running board. A wooden board that belonged to the running board was also taken out.

Running boards for pilot

We also took out several smaller parts from plane:

• An outlet which has been connected to the main conduit street down on the port side by spun II.

• A removable rod lying on top of the pilot footboards starboard between ribs 2- 4.

• A device with unknown function that has probably been one valve with handle, Found down on the starboard side between the ribs 5- 6.

• A tubular section that belonged to hot air system, and sticking up and out of the room behind the large fuse box at the pilot port footrest, between the ribs 2- 3.

• More T- links that belonged to the hydraulic system, and has been placed somewhere between the ribs 1- 6, was found lying on the floor.

Today we have taken out a bracket for a fire extinguisher which was mounted below the ribs 3a, next pilot's right leg

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. A tøypakning was placed in the bottom of- and a wrench attached to the bracket.

Holder for a fire extinguisher which was located below the pilot's right leg.

Attached to the rudder pedal on the port side, by spun 2, was screwed out.

Pilot port footrest, consisting of steel with a sheet of plywood on top, were detached from the area between the ribs 2- 3a.

A double bracket, which is disposed below the port frame 6 was dismantled.

Bracket for port rudder pedal.

Today we got taken out trottelkassen with pipes and transfers. The box is the circumstances in a good condition.

Engine and propeller control

A sign showing the outline of the contents of the fuse box, under the pilot's footboards on the port side, are in a poor condition. We therefore decided to dismantle this even if the fuse box will be standing for a while.

A box which was located in the area between trottelkassen and pilot port footboards / footrest, was taken out. The box has served as a junction point where various chains are connected to wires. There are also several air chains. The box is in poor condition while the chains seem to have managed stay at fjord better.

A pulley mount bracket was removed from the area between the ribs IV- V down the starboard side

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. There was a wire from the basket and into the chain case, mounted a bit further up on the same side.

A Cover, and bank / channel chains and wire, which was on the bottom between the ribs IV- V on the starboard side, was dismantled.

A box was removed from the bulkhead upper starboard between frames IV- V.

An adjustable fastening, with the bracket, Navigator folding seat, was removed from the starboard side, between ribs IV- V.

Trottelkasse with associated røroverføringer

Today we have also taken out some minor parts:

• A bracket was positioned behind the folding seat, and which may have been used to hold the seat in its upright ( in use ) position.

• A bracket may have served as securing Navigator folding seat when it has been left in its upright ( not in use ) position.

• A hoop with an underlying plate which was riveted to the bulkhead, up on the starboard side, between ribs IV- V, was dismantled
  . At each end of the bracket was riveted leather strap.

It was today taken out a box that contained several dimmer switches

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. This was located a little way up on the port side, between the ribs 3- 4. The box is in poor condition and will disintegrate.

Automatic light adjustment

An exterior hatch is located on the port side, between ribs III- IV, just below the rear plexiglass pane, was dismantled.

An instrument with a chain drive, with associated covers, and that may have worked as a position indicator for an equipment, was dismantled from below on the starboard side by spun IV.

It was also taken various smaller parts:

• A plate has been left behind a switch that was located in the midst of the starboard between ribs III- IV, was dismantled.

• Like other days, it has also today appeared some loose small parts with unknown function and location

  . These are valued and recorded with the information we have available.

Today we have dismantled starboard support for the pilot's seat which was placed between the ribs 4- 5.

Support for the pilot's seat

Meanwhile, a hydraulic cylinder up between the ribs 4- 5, dismantled

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. This was used to adjust the seat height of the pilot's seat.

Hydraulic cylinder for adjusting the pilot's seat height

A hinged window was also removed from the starboard side, the bottom between the ribs in- II

A plywood armrest for navigator was dismantled from the area behind the rib, on the port side

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. This was in use when the navigator was lying on his mattress brand promotion in the nose.

A plexiglass window at the bottom of the starboard, promotion at frame I, was unscrewed.

Some of the equipment which is located on the starboard side between the ribs 1- 4.

Attachment for bombsight promoting the bottom between the ribs in- II was unscrewed.

A bracket with 2 pressure switches were removed from the area between the frames I- II, on the starboard side.

Two three bricks, on the port side of the hatch down to the bomb shelter from the cockpit, was dismantled.

Two slots in the floor below the pilot's legs were removed
. They are built in a timber, and is provided with a release handle
. Upon activation of the handle before the hatches is still open.

A part of the auxiliary controller was removed from the area directly behind the ribs 1, on the starboard side.

Various switches and fuses on the port side just behind the pilot's instrument panel

A plexiglass window, with hinges, was dismantled from below on the starboard side, between frames In- II.

It was also picked out some small parts of the plane:

• A fire extinguisher, which was located at the bottom right Pilot legs, was taken out.

• a hot air pipes, which was routed back along the port side of the cutting edge of the cockpit, was taken out.