Pilot's Operating Handbook
Supplement 63
Lavatory compartment
Edition 1 - November 16, 2016
Rev. 3
Page 9.63.19
SECTION 7
Description
Information hereafter supplement or replace those of the standard airplane described
in section 7 Description of the basic POH when the airplane is equipped with the option
Lavatory compartment.
For operation, refer to equipment User's Guide.
The lavatory compartment is installed against right interior upholstery panel, facing
large door. The lavatory compartment is installed at the place of the rear seats,
removed to allow this installation. It is attached to the fuselage structure on the cabin
floor, using the seats tracks with four pads and screws.
The lavatory compartment structure is made of composite panels.
The lavatory compartment assembly is composed of :
-
A chemical toilet,
-
Electrically deployable separating panels (divider),
-
Two (2) actuating switches (DEPLOY, STOW),
-
Two (2) emergency stowing buttons (PUSH TO STOW), accessible from inside
or outside the lavatory compartment,
-
One (1) mirror,
-
One (1) electric power plug,
-
One (1) headset allowing communication between the passenger and the
crew.
When the lavatory compartment is not occupied, the divider is stored unfolded in the
lavatory compartment structure.
A breaker integrated into the lavatory compartment structure protects its electrical
system. The circuit breaker is only accessible when the lavatory compartment is
removed.
Two (2) switches, located on the seat front face, left side, hidden when latching strap
snap fastener is locked, control the deployment/stowing of the moveable parts of the
divider.
Two (2) access doors (Velcro tape attached), located on each side of the fixed part of
the divider, give access to the emergency stowing push button, allowing the
emergency (manual) retraction of the divider, using the application of a vertical force
(by hand) on the upper edge of the divider.
PIM - DO NOT USE FOR FLIGHT OPERATIONS
