The Airplane Factory Sling 4, Руководство по обслуживанию

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DOCUMENT No.: REVISION: 1.2 DATE: 2014/11/10
DC-MAM-001-X-C-2 Page 42
DOCUMENTATION:
Verify that the documents required by the current national regulations are present, correct and up to
date.
PLACARDS, LABELLING AND INSTRUCTIONS:
Inspect for the presence and correctness of any placards or notices which are required by the
current national regulations.
Inspect for the proper labelling of equipment, switches and control levers.
2.2. INSPECTION PANELS
Inspection points/ locations that are not in plain view may be accessed through specific inspection
holes and inspection hatches and / or by the removal of panels or fairings, as detailed below:

Inspection hatches on the wing underside provide access to the aileron bellcrank and flap
torque tube and pushrod.

Covers on the underside of the wing and at the wing to-fuselage connection points provide
access to engine fuel supply and return line connections to the tank, tank level sender, tank
level sender-wiring connectors, flap and aileron control pass-throughs and rear spar
connections (the front spar connection is accessed inside the cabin).

Small round tail cone side holes provides access to the elevator control horn and pushrod
end.

The vertical and horizontal tail nacelle / fairings provide access to vertical and horizontal tail
mounting and connections.

The elevator left lower (under elevator) inspection panel allows access to trim tab motor and
trim tab pushrod.

Inspection panels on the ventral rear fuselage allows for inspection of the elevator cable
guides.

A rear cabin central floor inspection panel provides access to the brake line T-piece divider,
brake lines; the elevator control system pushrod.

Baggage compartment floor inspection panels provide access to the cables for rudder
control.

Cabin longitudinal divider side inspection hatches provide access to fuel lines, rudder
cables, throttle cables and fuel filters.

The instrument panel cover provides access to the aircraft instrumentation and the related
wiring and pneumatic connections.

The engine cowling provides access to the engine and related systems, access to the
components of the electrical system located forward of the firewall and access to the nose
gear strut and steering assembly mechanism.

The propeller spinner provides access to the propeller hub.

A clear lens in each wing provides access to the landing and taxi lights.