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:
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Window – lower – foremost- spun In- II.
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Window – On top – foremost- spun In- II.
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Window – top center- spun In- III.
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Window – lower – rear- spun In- III.
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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:
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Breaking (main switch) connected to mains street by spun III.
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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.
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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.
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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.
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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
• The majority of patients assessed to be at low orinjectable alprostadil and bleeding sildenafil side effects.
. The conduit is attached with 2 clip.
- One of many switch boxes in the cockpit and nose section
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The remnants of a lamp connected to mains street by spun IV.
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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.
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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.
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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
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Hann Contact, labeled V 14, for reviewing spun V of the front. The contact is terminated in terminal block in frame V.
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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.
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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.
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Switch box terminated in terminal block in frame V.
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Internal contact, for the external temperature sensor, between the ribs 1- 2. It is terminated in the upper terminal between ribs 1 – 2.
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Box having contained two push-button switches, with red indicator. The box is placed between the ribs 2- 3.
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Bosch horn / audible alarm which is located upstairs in front of the pilot's instrument panel.
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Switch m / hatch is placed between the ribs 1- 2, behind the main line street. The mounting bracket is the C-5.
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Switch box terminated in terminal block in frame V.
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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.
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fuse / switch which is arranged in front frame 3a. The wires to and from this goes through this rib.
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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.
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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
