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A/T1
VTA
SPD VAPP ASEL
M
0.856M
DTK
360
HDG
330
SRP
1000
VS 1000
54
MSG 0
1
2
3
1
2
3
9500
10500
10000
VOR 1
VOR 2
ATT2
ADC3
20 20
10 10
10 10
20 20
1300
200
185
6
4
10400
20
00
80
60
95
N
33
30
W
24
21
S
15
12
E
6
3
H23.4NM
FMS1
VOR1
Honeywell
AIRSPEED LIMITS - (INDICATING SPEEDS)
VSE (SLATS OUT, 0°FLAPS) . . . . . . . . . . . .
VFE (SLATS OUT, 6°FLAPS) . . . . . . . . . . . .
VFE (SLATS OUT, 16°FLAPS) . . . . . . . . . . .
VFE (SLATS OUT, 30°FLAPS) . . . . . . . . . . .
VA (MANEUVERING)
(AT SEA LEVEL @ 96,000 LB) . . . . . . . . . . .
(AT 20,000 FT @ 78,600 LB) . . . . . . . . . . . . .
VMO
VMO
MMO
MMO
MMO
MMO
VLO
VLO
VLE
(BELOW 8,000 FT) . . . . . . . . . . . . . .
(8,000FT TO 30,267 FT) . . . . . . . . . .
30,267FT TO 35,000 FT) . . . . . . . . . .
(AT 41,000 FT) . . . . . . . . . . . . . . . . .
(AT 47,000 FT) . . . . . . . . . . . . . . . .
(AT 51,000 FT) . . . . . . . . . . . . . . . .
(EXT) (L/G EXTENSION) . . . . . . . . .
(RET) (L/G RETREACTION) . . . . . .
(L/G EXTENDED) . . . . . . . . . . . . . . .
225
210
210
185
254
250
300
340
0.89
0.88
0.858
0.842
200
200
250
AIRSPEED LIMITS - (INDICATING SPEEDS)
VSE (SLATS OUT, 0°FLAPS) . . . . . . . . . . . .
VFE (SLATS OUT, 6°FLAPS) . . . . . . . . . . . .
VFE (SLATS OUT, 16°FLAPS) . . . . . . . . . . .
VFE (SLATS OUT, 30°FLAPS) . . . . . . . . . . .
VA (MANEUVERING)
(AT SEA LEVEL @ 96,000 LB) . . . . . . . . . . .
(AT 20,000 FT @ 78,600 LB) . . . . . . . . . . . . .
VMO
VMO
MMO
MMO
MMO
MMO
VLO
VLO
VLE
(BELOW 8,000 FT) . . . . . . . . . . . . . .
(8,000FT TO 30,267 FT) . . . . . . . . . .
30,267FT TO 35,000 FT) . . . . . . . . . .
(AT 41,000 FT) . . . . . . . . . . . . . . . . .
(AT 47,000 FT) . . . . . . . . . . . . . . . .
(AT 51,000 FT) . . . . . . . . . . . . . . . .
(EXT) (L/G EXTENSION) . . . . . . . . .
(RET) (L/G RETREACTION) . . . . . .
(L/G EXTENDED) . . . . . . . . . . . . . . .
225
210
210
185
254
250
300
340
0.89
0.88
0.858
0.842
200
200
250
GX_01_022
1. Airspeed Placard
2. Primary Flight Display
3. Multifunctional Display
- MAP Format
- PLAN Format
- WX Radar
- TCAS Traffic
Indicates Chapter in which information on item may be found.
7 16
1
2 3
CREW LIFE VEST
UNDER SEAT
7 16
For Training Purposes Only
Sept 04
1-39
P I LOT T R A I N I N G GU I D E
AIRPLANE GENERAL
CENTER INSTRUMENT PANELS
STATIC GROUND OPERATION
PROHIBITED BETWEEN 66-80% N1
20
10
30
20
10
30
0
9
8
7
6
5
4
3
2
1
100 FEET
ALT
1 000 32
4
10 13
mb/hPa
29 9 2
IN HG
IAS KNOTS
180 200 220 250
BARO
GX_01_023
Engine Indication and Crew Alerting
System (EICAS) Primary Display
Note
• Engine Instruments
• Caution and Warning Annunciator
• Fuel Quantity
• Flap/Slat and Spoiler Status
• Landing Gear Status
• Flight Control Trims
For Global 5000 see Appendix 1.
Standby Altimeter/
Airspeed Indicator
Standby Attitude
Indicator
17
7
10
10
EICAS Systems Display
11
10
14
10
Indicates Chapter in which information on item may be found.
13
3
6
11
10
12
• Airplane Status information
and the following synoptic pages
• Bleed System
• Anti-Ice
• Hydraulics
• Electrical System (AC and DC)
• Fuel System
• Flight Controls
L ENG FLAMEOUT
FUEL LO QTY
FUEL IMBALANCE
YD OFF
GLD MANUAL ARM
PARK/EMER BRAKE ON
<– FUEL XFER ON
TOTAL FUEL (LBS) 415OO
1.54
146OO 1OOOO 146OO
N2
FF (PPH)
OIL TEMP
OIL PRESS
93.4
575O
115
81
1.65
　
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本文鏈接地址：Bombardier Global AIRPLANE GENERAL(17)