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Emergency door operation from inside the cabin is achieved by single action of the emergency exit
operating handle.
EMERGENCY EXIT DOOR
GF0110_036
Two lower hook fittings and two upper latch fittings position the door in the door opening. Three stop
fittings on each side of the door and surround structure react to the pressurization forces of the plug
door type.
HOOK FITTING
LATCH FITTING
HAND HOLD
LATCH MECHANISM
DOOR STOP
BOTH SIDES
GF0110_037
When the door is removed, handling is facilitated by an interior hand grip, flush-mounted within the
door box structure.
AIRPLANE GENERAL
Rev 12, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
01−10−53
EMERGENCY EXIT (CONT'D)
To unlatch the emergency exit door from the interior, the upper door handle is pulled inward. This
motion opens the exterior push plate/vent flap to bleed any residual pressure and disengages the two
latch pins. The door moves inward and pivots on the lower hook fittings. A grip of the upper handle is
maintained while grasping the lower hand grip and the door is lifted inwards away from the door
opening.
QUICK RELEASE
LATCH MECHANISM
HAND GRIP
GF0110_038
To unlatch the emergency exit door from the exterior, the upper push plate/vent flap is depressed to
disengage the latch pins and the door is pushed inwards away from the opening.
PUSH IN FLAP
PUSH DOOR INWARD
GF0110_039
Visual indication of a locked condition of the overwing emergency is the exit door secured in position,
with the interior handle recessed in the surround structure.
AIRPLANE GENERAL
Flight Crew Operating Manual Rev 12, Aug 14, 2006
CSP 700−5000−6
Volume 2
01−10−54
AFT EQUIPMENT BAY DOOR
The unpressurized aft equipment bay is accessed by a maintenance door in the fuselage fairing. The
door is horizontally hinged at it’s forward edge with initial and subsequent opening movements being
downward and outward. When the door is opened, it is restrained from over travel and striking the
belly fairing using two, door-to-fairing mounted lanyards.
The door locking mechanism is capable of operation only from outside of the airplane.
AFT EQUIPMENT BAY DOOR SCHEMATIC
LANYARD
LATCH MECHANISM
GF0110_040
During the closing cycle, two rollers, one on either side of the door, act as guides to locate and centre
the door within its belly fairing aperture.
AIRPLANE GENERAL
Rev 12, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
01−10−55
AFT EQUIPMENT BAY DOOR SCHEMATIC (CONT'D)
Aft Equipment Bay Door Operation
DOOR OPENING − Door opening is accomplished by depressing the trigger and pulling the
handle to the full open position.
DOOR LATCH
HANDLE ASSEMBLY
GF0110_041
DOOR CLOSING − The door latch handle is flush fitting and is secured by an integral push trigger,
which when depressed, releases the handle to the free open position. The door is secured by
returning the handle flush with the door.
Visual indication of secure latching and locking is given by the door, the push trigger and the
external handle all being flush with the fuselage’s surface.
AIRPLANE GENERAL
Flight Crew Operating Manual Rev 12, Aug 14, 2006
CSP 700−5000−6
Volume 2
01−10−56
BAGGAGE COMPARTMENT DOOR
A baggage compartment plug type access door is installed in the fuselage aft section on the left side
forward of the rear pressure bulkhead.
Aft Passenger
Compartment
Bulkhead
Cargo
Compartment
CARGO
DOOR
OPENING
BAGGAGE
COMPARTMENT
INTERIOR
DOOR
HANDLE
GF0110_042
The door is an inward opening plug type and can be unlatched from outside or inside the airplane.
The door is accessible, but not visible, from the passenger compartment and is not an emergency
exit. The door moves inward and upward to a stowed position above and clear of the door aperture.
DOOR HANDLE RECESS
PUSH TRIGGER
OUTER HANDLE
CARGO DOOR OPEN
STOWED POSITION
GF0110_043
The latch mechanism consists of inner and outer handles directly coupled together and mounted on
the forward and aft sides of the door. The handle assembly contains a trigger lock which holds the
handle in the stowed position. The door is latched when the exterior handle is rotated to engage latch
pins and locked when the handle is stowed and latched in its housing recess.
AIRPLANE GENERAL
Rev 12, Aug 14, 2006 Flight Crew Operating Manual
　
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