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EMS Circuit Protection................................................................................................ 1-47
For Training Purposes Only
Sept 04
1-1
P I LOT T R A I N I N G GU I D E
AIRPLANE GENERAL
INTRODUCTION
The BD-700 Global 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 BR710 turbo fan engines.
The airplane structure, in general, is fabricated from aluminum alloys. Alloy steels,
stainless steels, titanium, and composites are also used.
Attention and strict processes are given to surface finishes, protection against
corrosion and to external surface smoothness throughout the airplane. Sealing
requirements include environmental sealing, protection of facing 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 certificated for operations up to a maximum pressure
altitude of 51,000 feet.
GX_01_001
Elevators
Horizontal
Stabilizer
Thrust Reverser
Doors
Outer Skin
Rudder
Flaps Aileron
Winglets
Fairing
Fwd Equipment
Compartment Doors
Radome
Cabin Floor
Multifunction
Spoilers
Vertical Stabilizer
Fairing
Engine Cowl
Ram Air Turbine
Compartment
Door
Bird Strike
Barrier
Wheel
Bins
Belly
Fairings
MLG Doors
(inner)
Vertical Stabilizer
Leading Edge
Side Panels
Dorsal
Fairing
Glass
LEGEND
Hybrid (Mainly Graphite)
Graphite
Kevlar
1-2 For Training Purposes Only
Sept 04
P I LOT T R A I N I N G GU I D E
AIRPLANE GENERAL
AIRPLANE DIMENSION SCHEMATIC (Global 5000 – see Appendix 1)
1
NOTE
For A/C 9002 to 9126 pre
SB 700-23-001. Measurement
at manufacturer’s
empty.
For A/C 9002 to 9126 post
SB 700-23-001 and A/C 9127
and subs. Measurement at
manufacturer’s weight empty.
weight
23 ft 6 in
(7.16 m) 13 ft 4 in
(4.06 m)
6 ft 0 in
(1.83 m)
7 ft 4 in
(2.24 m)
13 ft 4 in
(4.06 m)
94 ft
(28.65 m)
10 ft 1 in
(3.07 m)
31 ft 9 in
(9.68 m)
21 ft 1 in
(6.43 m)
4 ft 1 in
(1.24 m)
8 ft 10 in
(2.70 m)
GX_01_002
3 ft
(0.91 m)
86 ft 5 in
(26.34 m)
5 ft 10 in
(1.78 m)
99 ft 5 in
(30.30 m)
24 ft 10 in
(7.57 m)
25 ft 6 in
(7.77 m)
1
2
PASSENGER COMPARTMENT
INTERIOR DIMENSIONS
Length
Width (floor line)
Height
Volume
Floor area
Width centreline
48 ft 4 in
6 ft 11 in
6 ft 3 in
2100 ft³
335 ft²
8 ft 2 in
(14.73 m)
(2.11 m)
(1.91 m)
(59.47 m³)
(31.10 m²)
(2.49 m)
1
2
42 ft 7 in
(12.98 m)
For Training Purposes Only
Sept 04
1-3
P I LOT T R A I N I N G GU I D E
AIRPLANE GENERAL
DESCRIPTION
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 99 ft. 5 in. (30.30 m)
Height 24 ft. 10 in. (7.57 m)
Wing
Span 93 ft. 6 in. (28.50 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)
(Global 5000 – see Appendix 1)
1-4 For Training Purposes Only
Sept 04
P I LOT T R A I N I N G GU I D E
AIRPLANE GENERAL
Fuselage
Diameter 8 ft. 10 in. (2.69 m)
Length 86 ft. 5 in. (26.34 m)
Landing Gear
Main Gear Nose Gear
Wheel Size 19 in. 10 in.
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