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
285.8
287.6
289.4
291.2
87.8
88.3
88.9
89.4
90.0
190
191
192
193
194
374.0
375.8
377.6
379.4
381.2
−48.3
−47.8
−47.2
−46.7
−46.1
−55
−54
−53
−52
−51
−67.0
−65.2
−63.4
−61.6
−59.8
−20.6
−20.0
−19.4
−18.9
−18.3
−5
−4
−3
−2
−1
23.0
24.8
26.6
28.4
30.2
7.2
7.8
8.3
8.9
9.4
45
46
47
48
49
113.0
114.8
116.6
118.4
120.2
35.0
35.6
36.1
36.7
37.2
95
96
97
98
99
203.0
204.8
206.6
208.4
210.2
72.8
63.3
63.9
64.4
65.0
145
146
147
148
149
293.0
294.8
296.6
298.4
300.2
90.6
91.1
91.7
92.2
92.8
195
196
197
198
199
383.0
384.8
386.6
388.4
390.2
GF0110_047
AIRPLANE GENERAL
Flight Crew Operating Manual Rev 2A, Apr 11, 2005
CSP 700−5000−6
Volume 2
01−10−14
GENERAL AIRPLANE DESCRIPTION
The airplane is a swept-wing monoplane with a pressurized cabin. It is capable of accommodating a
pilot, a copilot, a third crew member and up to 19 passengers. The airplane has two BMW/Rolls
Royce BR 710 turbofan engines.
The airplane structure, in general, is fabricated from aluminum alloys. Alloy steels, stainless steels,
titanium and composites are also used.
FGF0110_001a
LEGEND
Kevlar
Graphite
Hybrid (Mainly Graphite)
Glass
Strict attention is given to surface finishes, protection against corrosion and to external surface
smoothness throughout the airplane. Sealing requirements include environmental sealing, protection
of faying surfaces (similar and dissimilar) against corrosion, pressure sealing and integral fuel tank
sealing.
At sea level, the airplane and its installed equipment is certificated for operation in ambient
temperatures ranging between −30°C (−22°F) and + 50°C (122°F). The airplane pressurization
system is certified for operations up to a maximum pressure altitude of 51,000 feet.
AIRPLANE GENERAL
Rev 12, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
01−10−15
AIRPLANE DIMENSION SCHEMATIC
FGF0110_002
(3.07 m)
94 ft 0 in
(28.65 m)
13 ft 4 in
(4.06 m)
8 ft 10 in
(2.70 m)
42 ft 7 in
(12.98 m)
25 ft 6 in
(7.77 m)
96 ft 9 in
(29.49 m)
83 ft 9 in
(25.53 m)
AIRPLANE GENERAL
Flight Crew Operating Manual Rev 2A, Apr 11, 2005
CSP 700−5000−6
Volume 2
01−10−16
DIMENSIONS AND GENERAL DATA
The data that follows is for general information only and is not to be used for inspection or rejection
purposes. When specific data is required, the applicable illustration should be used.
Overall dimension
Length 96 ft. 9 in. (29.49 m)
Height 25 ft. 6 in. (7.77 m)
Wing
Span 93 ft. 6 in. (28.5 m)
Root chord (BL 47.61) 21 ft. 1 in. (6.43 m)
Tip chord (W/STA 544) 4 ft. 1 in. (1.24 m)
Dihedral of Wing Ref. Plane 2.5°
Spar locations
Front 14.0%
Rear 67.0%
Flaps 3 per side
Single Slotted Fowler Flaps
Slats 4 L.E. segments per side
Ground spoilers 2 per side
Multi-function spoilers 4 per side
Horizontal tail surface
Span 31 ft. 9 in. (9.68 m)
Root chord 10 ft. 5 in. (3.18 m)
Tip chord 5 ft. (1.52 m)
Anhedral 5.0°
Vertical tail surface
Span 13 ft. 8 in. (4.17 m)
Root chord 16 ft. 7 in. (5.05 m)
Tip chord 10 ft. 7 in. (3.22 m)
Fuselage
Diameter 8 ft. 10 in. (2.69 m)
Length 83 ft. 9 in. (23.53 m)
Landing gear
Main gear Nose gear
Wheel size 19 in. 10 in.
AIRPLANE GENERAL
Rev 12, Aug 14, 2006 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
01−10−17
DIMENSIONS AND GENERAL DATA (CONT'D)
Landing gear (Cont’d)
Tire size 38 in. 21 in.
Max loaded tire pressure 172 psi. 154 psi
Main gear track 13 ft. 8 in.
(4.18 m)
Nose gear track 13.14 in.
(33.4 cm)
Wheel base (max.) 40 ft. 2 in.
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Bombardier_Global_000-Airplane_General(9)
