ABAA
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3. DESCRIPTION (Figure 1)
A. Fuel system replenishment point
The fuel system replenishment points (1 per wing) allow to replenish the structural fuel tanks located into the wings of the aircraft. They are plugged by means of one-quarter rotation filler caps and are located on the upper surfaces of the wings between ribs N8 and N9.
B. Oil system replenishment point
The oil system replenishment point allows to replenish or to top up the engine oil casing. It is located on the upper casing of the engine, and plugged by means of a dipstick/filler cap. This replenishment point is accessible through inspection door 122, located on the upper engine cowling.
C. Brake hydraulic system replenishment point
The brake hydraulic system replenishment point allows to replenish or to top up the hydraulic fluid reservoir which supplies fluid to the braking system. It is located on the R.H. side of the firewall and is accessible after removal of the upper engine cowling 121.
D. Replenishment point of the electrohydraulic generator reservoir
The replenishment point of the electrohydraulic generator reservoir allows to replenish or to top up the reservoir with hydraulic fluid used for the landing gear maneuver. This replenishment point is located on the top of the electrohydraulic generator reservoir and is plugged by means of a dipstick/filler plug. It is accessible through inspection door 238, located beneath the rear bench seatpan.
E. Refrigerant replenishment point (option)
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