MDM MDM-1 FOX, Руководство по эксплуатации самолета

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MDM-1 „FOX” FLIGHT MANUAL
1.3
Issue III
Fuselage :
Monocoque, sandwich structure with integral fin. The seat pans bonded permanently. Two-piece, side
hinged canopy opening sidewards to the right.
In fuselage nose the total pressure port and air intake for air vent are provided, static pressure ports on
the fuselage nose both sides.
The transceiver antenna installed in the fin.
The towing hook installed in the front fuselage part.
The winch-launching hook installed in front of the main undercarriage.
At front seat, on both sides on cockpit floor, the balancing weights are installed.
Pedals at front seat - adjustable with a grip (item 11 in Fig. 7.1)
Back rest of front seat - adjustable by changing the position of back rest support (item 23 in Fig. 7.2)
Tail unit :
Stabilizer, elevators and rudder of sandwich structure, control surfaces aerodynamically-, and mass-
balanced.
Control system :
Elevator and aileron control system - push rod type.
Rudder control system - cable type.
Air brake control system, in wings of push rod type and in fuselage - combined.
The elevator system equipped with a spring trimming device operated with a lever at the control stick
base, at front seat.
Undercarriage :
Fixed undercarriage (with main and tail wheels), faired. Hydraulic disc brake on main wheel, actuation
coupled with air brake.