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Evector EV-97 EUROSTAR SL MICROLIGHT - Lubricating Points; Access Holes for Lubricating & Inspection

Evector EV-97 EUROSTAR SL MICROLIGHT
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EV-97 Eurostar SL Microlight Maintenance Manual GEN/EUR/04 Issue 4 34
7.3 Lubricating Points
Unit
Lubricating point
After the
first
25 hrs.
Every
50 hrs.
Every
100 hrs or
annually
Lubricant
Engine
oil change according to Engine Manual
carburettor control cable at inlet into the
Bowden cable (in engine compartment)
x x x
ACF50
choke control cable at inlet into the
termination (in engine compartment)
x x x
ACF50
Nosewheel
landing gear leg in the area of bushing
x
x
x
oil
landing gear
bearings in pull rod terminals of landing
gear control
x x x
oil
Main landing
gear
Brake pad holding pins
x x
grease
hinges
x
x
oil
Ailerons
control hinge pin
x
grease
bell cranks, inside the wing
x
grease
hinge joint of rods under the wing fillet
x
grease
Flaps
hinges
x
x
x
oil
all movable joints under the quadrant
cover between the seats
x
grease
All movable joints under the baggage
compartment bottom cover
x
grease
Flaps control pins (at a flap root)
x
x
grease
Elevator
Elevator hinge
x
x
oil
Swivel bearing in the elevator control
rod termination
x
grease
Rudder
rudder pivots
x
grease
rudder control cables at attachment to
the rudder
x
grease
adjustable rudder pedal mechanism,
plunger pin and lever.
x
x
oil
Trim tab
trim tab hinge
x
x
x
oil
control cables at inlets to the
terminations
x
grease
Control Stick
All movable joints in the cockpit
x
grease
Rudder
control and
brake pedals
All movable joints in the cockpit
x
grease
Brake system control cables at inlets in
the Bowdens (at brake pedals if right
seat brake pedals are fitted)
x
ACF50
7.4 Access Holes for Lubricating & Inspection
Inspection and access holes are provided as follows:
Access covers on the wings lower surface - access to the aileron control rods and levers
and to the pitot/static installation in the outer half of the wing;
Access cover on the fuselage lower surface under the baggage compartment close to the
fuel tank - access to the fuel tank installation;
Access cover on the fuselage lower surface in the middle of the rear section - access to the
elevator control rods and relay lever;
Wing fillets which cover the space between the fuselage and wing root - access to the wing-
fuselage attachments;
Panel covering the control stick system in the cockpit;
Panel covering the flap & trim control levers in the cockpit;
Baggage compartment floor access to the elevator and flap control linkage.

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