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13.5 m
3
2
3
2
AIRPLANE GENERAL
Sep 13/2004 Flight Crew Operating Manual Volume 2
REV 1 CSP 100-6 01-02-05
ANTENNA LOCATION SCHEMATIC
SATCOM
(IF INSTALLED)
VOR/LOC
(LH AND RH)
HF
ELT
(OPTIONAL)
VHF COMM #3
(IF INSTALLED)
MARKER
BEACON
RAD ALT
ADF #1
ADF #2
VHF COMM #1
TCAS
(DIRECTIONAL)
GPS #1
GPS #2
ATC
DME #1
TCAS
OMNI
VHF COMM #2
DME #2
ATC
TELECOM
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.
WARNING
WEATHER RADAR
GLIDESLOPE
CFO0101002_005
LIGHTNING
SENSOR
(OPTIONAL)
AIRPLANE GENERAL
Volume 2 Flight Crew Operating Manual Sep 13/2004
01-02-06 CSP 100-6 REV 1
VISUAL EYE REFERENCES FOR GROUND OPERATION
WITH HEAD MOVED
0.3 ft (91 mm)
OUTBOARD
PILOT'S EYE
POSITION
PILOT'S EYE
POSITION
APPROACH VISIBILITY
10.5 ft
(3.2 m) 19°
17°
7.7 ft
(2.3 m)
26.6 ft
(8.1 m)
8.7 ft
(2.6 m)
MAXIMUM 139° VISION AFT
WITH HEAD ROTATED
1.8 ft
(0.54 m)
PILOT'S EYE
POSITION
51°
32°
17°
20°
51°
17°
20°
32°
CL
NOT FOR LANDING
AIRPLANE GENERAL
Sep 13/2004 Flight Crew Operating Manual Volume 2
REV 1 CSP 100-6 01-02-07
STEERING AND TURNING RADII
Steering and turning radii are shown below.
STEERING AND TURNING RADII SCHEMATIC
CFO0101002_006
NOTE
MAXIMUM STEERING
SYMMETRICAL AND IDLE THRUST
NO DIFFERENTIAL BRAKING
65° STEERING ANGLE
3° SLIP
DRY RUNWAY
SLOW CONTINUOUS TURN
MAX A/C WEIGHT
AFT CG
27.8 ft
(8.4 m)
r 37.4 ft
(11.3 m)
95.5 ft
(29.1 m)
58.0 ft
(17.7 m)
MIN PAVEMENT
WIDTH 180° TURN.
WITH 5 ft MARGIN
OF SAFETY.
21.0 ft
(6.4 m)
r 20.0 ft
(6.10 m)
r 31.5 ft
(9.6 m)
r 38.4 ft
(11.8 m)
65.0°
AIRPLANE GENERAL
Volume 2 Flight Crew Operating Manual Sep 13/2004
01-02-08 CSP 100-6 REV 1
DANGER AREAS
CFO0101002_019
WEATHER RADAR
5 ft
(1.5 m)
15 ft (4.5 m)
FROM INTAKE
15 ft (4.5 m)
FROM INTAKE
APU EXHAUST
500 °F (260 °C)
19 ft (5.8 m)
200 ft (60.9 m) FROM TAILPIPE
200 °F (93.3 °C)
NOTE:
EXHAUST DANGER AREA
SHOWN FOR IDLE RPM.
VALUES APPROXIMATELY
DOUBLE FOR TAKEOFF
RPM.
AIRPLANE GENERAL
Sep 13/2004 Flight Crew Operating Manual Volume 2
REV 1 CSP 100-6 01-03-01
AIRPLANE JACKING
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).
CFO0101002_012
TYPICAL JACK
NYLON
PLUG
JACK
PAD
JACKING
POINT
SUPPORT
BEAM
REAR FUSELAGE SUPPORT
JACK
REAR FUSELAGE
SUPPORT
LEGEND
REV 1
AIRPLANE GENERAL
Volume 2 Flight Crew Operating Manual Sep 13/2004
01-03-02 CSP 100-6 REV 1
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
CFO0101002_010
TOW BAR
ASSEMBLY
REV 1
AIRPLANE GENERAL
Sep 13/2004 Flight Crew Operating Manual Volume 2
REV 1 CSP 100-6 01-03-03
MOORING
Fittings are provided on the fuselage and on the wing jacking points for mooring the airplane. Use chocks on all wheels
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Bombardier 300 airplane general(3)
