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.46.7 .52 .61.6 .18.9 .2 28.4 8.9 48 118.4 36.7 98 208.4 64.4 148 298.4 92.2 198 388.4
.46.1 .51 .59.8 .18.3 .1 30.2 9.4 49 120.2 37.2 99 210.2 65.0 149 300.2 92.8 199 390.2
GF0110_047
Volume 2 Flight Crew Operating Manual Rev 2A, Apr 11, 2005
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.
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.
FGF0110_001a
Rev 12, Aug 14, 2006 Flight Crew Operating Manual Volume 2
AIRPLANE GENERAL
AIRPLANE DIMENSION SCHEMATIC
83 ft 9 in
(25.53 m)
96 ft 9 in
(29.49 m)
FGF0110_002
Volume 2 Flight Crew Operating Manual Rev 2A, Apr 11, 2005
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 Height 96 ft. 9 in. 25 ft. 6 in. (29.49 m) (7.77 m)
Wing
Span Root chord (BL 47.61) Tip chord (W/STA 544) Dihedral of Wing Ref. Plane 93 ft. 6 in. 21 ft. 1 in. 4 ft. 1 in. 2.5° (28.5 m) (6.43 m) (1.24 m)
Spar locations
Front 14.0%
Rear 67.0%
Flaps Slats Ground spoilers Multi-function spoilers 3 per side Single Slotte4 L.E. segm2 per side 4 per side d Fowler Flaps ents per side
Horizontal tail surface
Span Root chord Tip chord Anhedral 31 ft. 9 in. 10 ft. 5 in. 5 ft. 5.0° (9.68 m) (3.18 m) (1.52 m)
Vertical tail surface
Span Root chord Tip chord 13 ft. 8 in. 16 ft. 7 in. 10 ft. 7 in. (4.17 m) (5.05 m) (3.22 m)
Fuselage
Diameter Length 8 ft. 10 in. 83 ft. 9 in. (2.69 m) (23.53 m)
Landing gear
Wheel size Main gear 19 in. Nose gear 10 in.
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