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Equivalent wing area (including ailerons,
flaps spoilers and area within the fuselage)
1022 sq. ft. (94.95 sq. m)
Horizontal tail area (Gross) 245 sq. ft. (22.76 sq. m)
Vertical tail area (Gross) 186 sq. ft. (17.28 sq. m)
Doors
Passenger door (LH. fwd)
Height to sill (one step below the floor line) 6 ft. 2 in. (188 m)
Width 3 ft. (0.91 m)
Height to sill (at floor line) 5 ft. 4 in. (163 m)
Baggage compartment door (LH, aft)
Height 2 ft. 9 in. (0.84 m)
Width 3 ft. 7 in. (1.09 m)
Height to sill (floor line) 6 ft. 7 in. (2.01 m)
AIRPLANE GENERAL
Flight Crew Operating Manual REV 51, Aug 14, 2006
CSP 700−6
Volume 2
01−10−18
ANTENNA LOCATION SCHEMATIC
TCAS
(Directional)
MODE
MODE
S 1
S 2
DME
#1
DME
#2
MARKER
BEACON
TCAS
OMNI
VHF COMM #2
MODE S
1 & 2
VHF COMM #1
GPS #1
ADF #1
ADF #2
ELT (Optional)
VOR/LOC
RAD ALT
RAD ALT
RAD ALT
RAD ALT
#1 TX
#2 TX
#1 RX
#2 RX
HF
(LH AND RH)
incorporated). (If installed)
GF0110_003
VHF COMM #3
(On airplanes with
SB 700−23−002
SATCOM
WARNING
Personnel should not stand nearby or in front of the radar antenna
when it is transmitting.
GLIDESLOPE
WEATHER RADAR
RADAR 5 mW/cm
PERSONNEL DANGER AREA
366 cm (12 ft.)
Refer to Pilot’s Manual Pub. No. A28−1146−056−02
GF0110_004
2
AIRPLANE GENERAL
REV 51, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−6
Volume 2
01−10−19
VISUAL EYE REFERENCES FOR GROUND OPERATION
GF0110_005
AIRPLANE GENERAL
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
01−10−20
STEERING RADII
Steering radii are shown below.
STEERING RADII SCHEMATIC
GF0110_006a
43 ft 0 in
(13.10 m)
56 ft 6 in
(17.24 m)
128 ft 2 in
(39.07 m)
14 ft 0 in
(4.26 m)
68 ft 0 in
(20.73 m)
53 ft 2 in
(16.23 m)
45 ft 2 in
(13.78 m)
20 ft 8 in
(4.23 m)
7 ft 4 in
(2.3 m)
MINIMUM
PAVEMENT
WIDTH
180° TURN
NOTE
Maximum steering
Symmetrical and idle thrust
No differential braking
75° steering angle
3° slip
Dry runway
Slow continuous turn
Max A/C weight
AFT CG.
AIRPLANE GENERAL
REV 51, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−6
Volume 2
01−10−21
TURNING RADII
Minimum paving width for 180° turn − 68 ft. (20.76 m)
TURNING RADII SCHEMATIC
AIRPLANE GENERAL
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
01−10−22
JET EXHAUST SINGLE ENGINE GROUND IDLE THRUST
GF0110_008
AIRPLANE GENERAL
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
01−10−23
JET EXHAUST SINGLE ENGINE TAKE-OFF THRUST
GF0110_009
AIRPLANE GENERAL
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
01−10−24
JET EXHAUST TWO ENGINE GROUND IDLE THRUST
GF0110_010
AIRPLANE GENERAL
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
01−10−25
JET EXHAUST TWO ENGINE TAKE-OFF THRUST
GF0110_011
AIRPLANE GENERAL
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
01−10−26
AIRPLANE JACKING
Three jacking points are provided, one on the forward fuselage and one on each wing rear spar for
jacking the complete airplane.
JACKING POINTS SCHEMATIC
TYPICAL JACK
JACK
REAR FUSELAGE SUPPORT
NYLON PLUG JACK PAD
JACKING POINT
SUPPORT BEAM
REAR FUSELAGE SUPPORT
LEGEND
GF0110_012
The nose jacking point is located on the fuselage centerline. Gear jacking points are also provided for
tire/wheel/brake changes. Jacking procedures are located in the Aircraft Maintenance Manual
(Chapter 07).
AIRPLANE GENERAL
REV 51, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−6
Volume 2
01−10−27
TOWING
A fitting for towing or pushing the airplane is located on the nose landing gear.
During towing, nose wheel swivel through the range of ±75° each side of center is possible, without
disconnecting the nose wheel steering torque links. The Aircraft Maintenance Manual (Chapter 09)
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