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disconnecting the nose wheel steering torque links. The Aircraft Maintenance Manual (Chapter 09)
has a detailed description of towing operations.
NOTE
Disconnecting the nose wheel steering torque links is recommended for
all towing operations.
TOW BAR ATTACHMENT SCHEMATIC
TOW BAR ASSEMBLY
GF0110_013
AIRPLANE GENERAL
Flight Crew Operating Manual Rev 3, Apr 25, 2005
CSP 700−5000−6
Volume 2
01−10−28
TOWBARLESS SCHEMATIC
FGF0110_013
WINCH STRAP
TOW VEHICLE
WINCH CUT−OFF
SWITCH PLATE
STRUT−STRAP
NOSE LANDING
GEAR
TOWBARLESS
REAR GATE CRADLE
Ground Locking Safety Pins
Ground safety locks are provided for the nose and each main gear, gear doors and for the Ram Air
Turbine (RAT). Refer to the applicable chapter for the safety pin installations.
AIRPLANE GENERAL
Rev 3, Apr 25, 2005 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
01−10−29
MOORING
Fittings are provided on the fuselage and on the wing jacking points for mooring the airplane.
Mooring procedures are located in the Aircraft Maintenance Manual (Chapter 10).
MOORING ATTACHMENT POINTS SCHEMATIC
MAIN AND NOSE AREAS
TAIL AREA
MOORING ADAPTER PLATE
JACKING PAD
TIE DOWN RING
GF0110_014
30.25° 30.25°
AIRPLANE GENERAL
Flight Crew Operating Manual Rev 3, Apr 25, 2005
CSP 700−5000−6
Volume 2
01−10−30
SEAT ASSEMBLY
The crew seats provide adjustments fore and aft, inboard/outboard lateral adjustment (“J” track),
height and armrest position.
GF0110_015a
AIRPLANE GENERAL
Rev 12, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
01−10−31
SEAT ASSEMBLY (CONT'D)
Seat Egression
Make sure the seat is in the fully upright position, then pull on the fore/aft lever and move the seat
to its fully aft position.
NOTE
The lateral tracking is now automatically enabled.
CAUTION
Do not try to move the seat laterally with the fore/aft lever in the up
position. This could cause damage to the mechanism.
Release the fore/aft lever.
Move the seat to its fully outboard position to facilitate egress from the seat.
Moving the Seat Forward
CAUTION
If the seat is moved forward when it is not in its fully inboard position,
it can jam.
After getting back onto the seat, before touching the fore/aft lever, move the seat laterally to its
fully inboard position.
NOTE
There is no mechanical lock to keep the seat in its position until you
move it forward.
Keeping the seat in its fully inboard position, raise the fore/aft lever to move the seat forward. The
seat must be moved forward at least one inch (2.54 cm) before the lateral tracking latch is
automatically locked. Release the lever when the desired forward position is reached.
NOTE
When the seat moves forward, the lateral tracking mechanism is
disabled, and the seat should not move laterally.
CAUTION
If the seat jams or moves laterally when it is not in its fully aft
position, do not attempt to reset it using force, as damage to the
mechanism may occur. Call a maintenance technician for
troubleshooting and repair.
AIRPLANE GENERAL
Flight Crew Operating Manual Rev 13, NOV 10, 2006
CSP 700−5000−6
Volume 2
01−10−32
EYE LOCATOR-SEAT ADJUSTMENT
An eye locator is mounted on the centre windshield post to enable seat adjustment for correct
eye-to-wheel height.
TOP VIEW FRONT VIEW
The support bracket is not shown.
GF0110_016
PILOT’S
SIGHT LINE
COPILOT’S
SIGHT LINE
NOTE
AIRPLANE GENERAL
Rev 12, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
01−10−33
CONTROL WHEEL
The pilot and copilot control wheels contain the following switches:
• Master disconnect.
• Pitch Trim Switch.
• Autopilot/Flight Director Touch Control.
• Radio Key.
Master Disconnect
The Master Disconnect switch disengages the autopilot, deactivates the stick pusher and the pitch
trim. When released, the stick pusher and the pitch trim system are immediately reactivated but
the autopilot remains disengaged.
Pitch Trim Switch
The Pitch Trim Switch enables the pilot/copilot to control the trim from each control wheel.
Autopilot/Flight Director (Touch Control)
The Touch Control Switch (TCS) is located on the control wheel. It enables the pilot to maneuver
　
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