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WIDTH CENTERLINE 7 ft 2 in 2.18 m
HEIGHT 6 ft 1 in 1.85 m
VOLUME 896 ft 3 25.37 m 3
FLOOR AREA 146 ft 2 13.5 m 2
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Volume 2 Flight Crew Operating Manual Sep 13/2004 CSP 100-6 REV 1
01-02-04
VOR/LOC VHF COMM #3 (LH AND RH)
WARNING
Personnel should not stand nearby and in front of the radar antenna when it is transmitting. When the antenna is not scanning, the danger increases.
GLIDESLOPE
Sep 13/2004 Flight Crew Operating Manual Volume 2 REV 1 CSP 100-6
01-02-05 VISUAL EYE REFERENCES FOR GROUND OPERATION
PILOT'S EYE POSITION
10.5 ft
19°
(3.2 m)
PILOT'S EYE
NOT FOR LANDING APPROACH VISIBILITY
C
L
Volume 2 Flight Crew Operating Manual Sep 13/2004 CSP 100-6 REV 1
01-02-06 STEERING AND TURNING RADII
Steering and turning radii are shown below.
STEERING AND TURNING RADII SCHEMATIC
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Sep 13/2004 Flight Crew Operating Manual Volume 2 REV 1 CSP 100-6
01-02-07
DANGER AREAS
200 ft (60.9 m) FROM TAILPIPE 200 °F (93.3 °C)
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Volume 2 Flight Crew Operating Manual Sep 13/2004 CSP 100-6 REV 1
01-02-08
Three jacking points are provided, one located forward on the fuselage, and one on each wing at the rear spar for jacking the complete airplane.
Gear jacking points are also provided for tire/wheel/brake changes. Jacking procedures are located in the Aircraft Maintenance Manual (Chapter 7).
SUPPORT BEAM
JACKING POINT
TYPICAL JACK JACK REAR FUSELAGE SUPPORT LEGEND NYLON PLUG JACK PAD REAR FUSELAGE SUPPORT
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Sep 13/2004 Flight Crew Operating Manual Volume 2 REV 1 CSP 100-6
01-03-01 TOWING
The aircraft maybe towed, with the torque links connected and the Steering Control System de-energized, up to a limit of 120° of nosewheel angle. Should the nosewheel angle exceed this value a NWS LIMT EXCEEDED CAS message (C) will be displayed. At approximately 123°, the indicator pins on the NLG will be sheared off to provide a physical indication that damage may have been done to the feedback linkage and surrounding area.
For special hangar operations, the torque links may be disconnected to allow towing at any angle, provided the shock strut extension exceeds the dimension in inches of chrome showing, provided on a warning plate. The warning plate is mounted on the nose landing gear to indicate to the ground crew the operational limits for towing. For further towing information refer to the Aircraft Maintenance Manual (chapter 9).
TOWING BAR ATTACHMENT
TOW BAR ASSEMBLY
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Volume 2 Flight Crew Operating Manual Sep 13/2004 CSP 100-6 REV 1
01-03-02
Fittings are provided on the fuselage and on the wing jacking points for mooring the airplane. Use chocks on all wheels when mooring the airplane. Mooring procedures are located in the Aircraft Maintenance Manual (Chapter 10).
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