曝光臺 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費(fèi)者

the pilot’s and copilot’s Electronic Flight Instrument System (EFIS)
control panels. The glareshield panels also contain the pilot’s and
copilot’s display unit reversion panels and master warning/caution
annunciator/reset switch.
The main instrument panel, in the middle tier area, is identified by four
8 x 7 inch high resolution color Cathode Ray Tube (CRT) displays. Display
Units (DUs) on the pilot’s side include both a Primary Flight
Display (PFD) and an Engine Indicating/Crew Alerting System (EICAS).
DUs on the copilot’s side include a multi-function display (MFD)
and a second PFD. The standby instruments (Airspeed, Attitude
Indicator and Altimeter) are located between the EICAS and copilot’s
MFD. The Crew Warning Panel (CWP) and Radio Management Unit
(RMU) displays are located below the standby instruments and
between the EICAS and copilot’s MFD. The angle-of-attack indicators
(if installed), digital chronometers and audio control panels for both the
pilot’s and copilot’s side are located near the outboard ends of the main
instrument panel.
The pilot’s subpanel contains the reversion control panel, electrical
control panel and the Attitude Heading Reference System (AHRS)
control for AHRS 1. It also contains the pilot’s side crew lighting panel
and rudder pedal adjustment switch. The copilot’s subpanel contains
the cabin pressurization and oxygen control panel, the environmental
control panel and cockpit voice recorder control panel. It also contains
the AHRS control for AHRS 2, the crew lighting panel and the rudder
pedal adjustment switch. The anti-ice panel, aircraft light control panel
and landing gear/hydraulic panel are all installed near the center of the
subpanel (center switch subpanel), directly above the forward side of
the throttle quadrant.
Pilot’s Manual
PM-132A 7-3/7-4 (Blank)
F40-070000-001-01
1. Pedestal
2. Throttle Quadrant
3. Air Outlet (ankle)
4. Fire Extinguisher (mounted on crew chair)
5. Smoke Goggle Storage
6. Pilot's Circuit Breaker Panel
7. Air Outlet (armrest level)
8. Pilot's Mic/Phone Jack Panel
9. Map Light
10. Pilot's and Copilot's Subpanels
11. Pilot's Control Column & Wheel
12. Glareshield Panels
13. Cockpit Speakers
14. Pilot's Primary Flight Display (PFD) (DU-1)
15. Engine Indicating and Crew Alerting
16. Dome Light
17. Sunvisor
18. Overhead Air Outlet
19. Eye Reference Locator
20. Assist Handle
21. Magnetic Compass
22. Crew Warning Panel
23. Multi-Function Display (MFD) (DU-3)
24. Copilot's Primary Flight Display (PFD) (DU-4)
25. Copilot's Control Column & Wheel
26. Instrument Panel
27. Copilot's Mic/Phone Jack Panel
28. Cabin Lighting Control
29. Copilot's Circuit Breaking Panel
30. Access for hanging plumb bob
1
3 2
5 4
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22 23
24
25
26
27
28
29
30
System (EICAS) (DU-2)
7
18
16
13
9
7
5
3
4
GENERAL ARRANGEMENT — COCKPIT
Figure 7-1
Pilot’s Manual
PM-132A 7-5
The pedestal is typically equipped with a single Flight Management
System (FMS), a trim control panel, a weather radar control panel, an
Emergency Locator Transmitter (ELT) switch, and an engine/fuel control
panel. Optional equipment in the pedestal may include a second
(dual) FMS, a high frequency communication control head, a SELCAL
control panel, and a 12-vdc cigarette lighter.
An inflatable harness type oxygen mask with an integral microphone is
stored on the outboard side of each crew seat. Smoke goggles are stored
in the left and right lower sidewall storage compartments. Hand-held
fire extinguishers are installed on the crew seats directly behind the
pilot’s and copilot’s legs. Life vests are stowed inside plastic holders
which are mounted to cabinets located directly behind each crew seat.
A magnetic compass is installed on the windshield center post near the
top of the windshield. The headliner houses a dome light, air outlets,
an assist handle and an access for a plumb bob location for leveling the
aircraft. The sunvisors are also attached to the headliner. No switches,
instruments or placards are located overhead. Circuit breaker panels
are located on the pilot and copilot upper sidewall panels. A flexible
map light is attached to the upper sidewall above the circuit breaker
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：BOMBARDIER_Learjet_0-Interior_Equipment(3)