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时间:2010-05-17 21:37来源:蓝天飞行翻译 作者:admin
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

the internal handle cover and the handle. The red band across the handle and cover clearly shows
the handle in the locked position. A safe indication is indicated by the alignment of the two red
lines.
Effectivity:
• Airplanes 9002 to 9095 not incorporating Service Bulletin:
• SB 700−52−22, Passenger Door − Internal Handle Indication Improvement.
LIFT ARM
VENT
FLAP
FORWARD
"G" LOCK
AFT "G"
MECHANICAL
INDICATOR
GREEN
LOCKED
OPEN
LOCKING
HANDLE
GF0110_031
LOCK
Visual indication of latching and locking is given by an indicator arm that is driven directly by the
last motion of the internal handle. The indicator, in the form of a green line, lines up with a green
line on the airstairs only after the door latches and detents are engaged. The indication is viewed
through a window cutout in the internal handle cover. A safe indication is indicated by the
alignment of the two green lines. A window in the handle exposes a red fixed plate when the
handle is out of the safe locked position.
AIRPLANE GENERAL
Flight Crew Operating Manual REV 51, Aug 14, 2006
CSP 700−6
Volume 2
01−10−50
PASSENGER DOOR OPERATING HANDLES
The external handle is set into a box in the lower door structure. It is connected by push/pull rods
inside the door to the lockshaft, at the forward end.
position until the handle moves to
the full down position.
LOCKSHAFT
GF0110_032
The door is not in the fully closed
EXTERNAL HANDLE
NOTE
As the lockshaft reaches its fully locked position, the handles are held in position with spring tension.
When the handles are moved out of the locked position, the spring assists in lifting the door and
reduces the load on the handles.
The internal handle is a lever on the forward side of the door directly attached to a lockshaft and to
the forward door lift arm.
(stowed) position. The door is not
in the fully closed position until
the handle moves fully down.
GF0110_033
NOTE
Handle shown in the locked
INTERNAL HANDLE
AIRPLANE GENERAL
REV 51, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−6
Volume 2
01−10−51
PASSENGER DOOR SWITCHES
The internal door operating switch is controlled on and off by the “DOOR” switch installed internally in
the door frame, next to the main passenger door.
INTERNAL SWITCH
(view looking from inside
the airplane)
EXTERNAL SWITCH
NOTE
Both switches are guarded
but not shown.
GF0110_034
The external door operating switch is controlled on and off by the “DOOR” switch installed next to the
main passenger door.
EXTERNAL DOOR SWITCH ACCESS PANEL
DOOR OPERATING
SWITCH
DOOR OPERATION
PUSH IN FLAP TO
GRASP HANDLE
LIFT HANDLE FULL UP
PULL DOOR OUT
1. OPERATE SWITCH TO
ROTATE DOOR FULLY
INTO DOOR APERTURE
2. PULL HANDLE
DOWNWARDS TO STOW
TO OPEN TO CLOSE
NOTE: DO NOT RE−CYCLE HANDLE DURING
CLOSING OPERATION WITHOUT RE− OPENING
DOOR SUFFICIENTLY TO RE−ARM DOOR
UPLOCK LEVER
Operating
Instructions
GF0110_035
AIRPLANE GENERAL
Flight Crew Operating Manual REV 51, Aug 14, 2006
CSP 700−6
Volume 2
01−10−52
PASSENGER DOOR OPERATION
The following examples are intended to familiarize the operator with events which occur when
moving the passenger door from either the open or closed positions. The door operations are
described in detail and should be followed as per Aircraft Maintenance Manual Chapter 52.
External Door Operation
To open the passenger door externally:
• PUSH IN FLAP TO GRASP HANDLE
• LIFT HANDLE FULL UP
• PULL DOOR OUT
To close the passenger door externally:
NOTE
Do not re-cycle the handle during closing operation without
re-opening door sufficiently to re-arm door uplock lever.
• DISENGAGE HANDRAIL LOCK
• PRESS AND HOLD DOOR CLOSE SWITCH
• PULL HANDLE DOWNWARDS TO STOW
Internal Door Operation
To open the passenger door internally:
• OPERATE DOOR HANDLE FROM THE LOCKED POSITION
• DOOR MOVES INWARD AND UPWARD
• PUSH DOOR OUT TO OPEN
To close the passenger door internally:
• PUSH FOOT PEDAL (to disengage handrail lock)
• PRESS AND HOLD DOOR CLOSE SWITCH
• MOVE DOOR HANDLE FULLY DOWN
• CHECK GREEN VISUAL INDICATION IN THE HANDLE
Manual Closing
A rope wound around a pulley on the aft end of the torque shaft must be unwound sufficiently to be
 
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