MDM MDM-1 FOX, Руководство по эксплуатации самолета

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MDM-1 „FOX” FLIGHT MANUAL
7.2
Issue III
7.1 Introduction.
This Section provides description and operation of the glider and its systems. Refer to Section 9 for
details of optional equipment.
7.2 Cockpit controls.
General view from glider front and rear seat is shown in Figs. 7.1 and 7.2.
All controls are operated conventionally.
The wheel brake is coupled with air brake, the control lever (item 16 in Figs. 7.1 and 7.2) is located on
the cockpit left hand side.
The elevator spring trimming device is operated with a grip on left hand side of the control stick base,
at front seat only (Fig. 7.1 item 18).
The canopy panels are opened with the white lever (item 14 6 in Figs. 7.1 and 7.2) located on the left
hand side.
The emergency jettison of canopy is activated by simultaneously pulling, with both hands, the red lever
(item 15 in Figs. 7.1. and 7.2.) on canopy right hand side, and canopy opening lever (item 14 in Figs.
7.1. and 7.2.) on the left hand side. Jettison of each canopy panel independently from front and rear seat.
The adjustment of rudder pedals at front seat - on ground only - by means of pedals adjustment handle
(Fig. 7.1. item 11) located under the instrument panel. No pedals adjustment provided at rear seat.
The front seat pilot’s back rest adjustable at its support (Fig. 7.1. item 23), accessible from rear seat.
Adjust the height of the rear seat by means of hard cushions.
The tow release control tension member terminated with a yellow hand-grip (item 9 in Figs. 7.1 and 7.2)
located as follows:

at front seat, on the left hand side, and

at rear seat, on the left hand portion of front seat back rest tube.
The air venting control tension member (Fig. 7.1 item 8) is located on the right hand side of instrument
panel, at front seat.
Two balancing weights (Fig. 7.1. item 13), 5,5 [kG] each, are installed with clamps in the floor at front
seat.
All levers are provided with the appropriate information pictographs.