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Bombardier Global Express - Lighting

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Bombardier Global Express - Lighting Bombardier Global Express - Lighting INTRODUCTION The airplane is equipped with a suite of lighting systems covering the direct and indirect illumination of the flight compartment and airplane exterior. The general airplane lighting includes: • Flight Compartment Lighting - Internal lighting is used in the flight compartment for flight instrumentation and general lighting • Passenger Compartment Lighting - Lighting systems for the passenger cabin are not provided, except for the main entrance • External Lighting - External lighting in the form of landing, taxi and airplane identification are used • Service and Maintenance Lighting - Lighting is available to service areas to assist maintenance personnel, in their airplane checks and inspections • Emergency Lighting - Lighting is provided to permit airplane occupants to safely move away from the airplane in an emergency situation DESCRIPTION FLIGHT COMPARTMENT LIGHTING Controls for the flight compartment are located on two panels on the center pedestal. One panel controls the flight compartment flood and display lighting, while the other controls the integral and miscellaneous lighting. There are two types of integral lighting in the flight compartment; electroluminescent (EL) lighting and incandescent lighting. All instrument panels are provided with integral legend/edge lighting. The instrument panels are grouped in an area, with each one having its dedicated dimming control. The electrical power to the integral lighting system is through an ON/OFF or AUTO mode selection of a MASTER switch. When in AUTO mode, to increase the life of the lighting elements (example: daylight or high cockpit light conditions) the system will be turned on or off automatically. This is accomplished through a light sensor circuit, which is dependent upon the ambient lighting conditions in the flight compartment. CRT display, fluorescent flood, integral instrument and instrument panel lights provide instrument lighting. The EMS CDU provides two LAMP TEST positions in order to test the indicator lights, through the electrical management system. Page 1 Bombardier Global Express - Lighting The flight compartment lighting includes the following: • Flight compartment flood lights • Flight compartment floor lights • Flight compartment area lights • Map lights • Flight compartment panels integral lighting • Flight compartment flashlights • Orientation light Page 2 Bombardier Global Express - Lighting FLIGHT COMPARTMENT INTEGRAL LIGHTING AREAS AREA 1 AREA 5 AREA 5 AREA 3 AREA 4 AREA 2 GX_15_001 AREA 1 OVERHEAD PANEL - Electroluminescent lighting or EL AREA 2 CENTER INSTRUMENT PANEL AND PEDESTAL - Mixed lighting; half EL lighting and half incandescent AREA 3 LEFT SIDE CONSOLE (Pilot) - Incandescent lighting AREA 4 RIGHT SIDE CONSOLE (Copilot) - Incandescent lighting AREA 5 CIRCUIT BREAKER/MISCELLANEOUS PANELS - Electroluminescent Lighting (EL) Page 3 Bombardier Global Express - Lighting FLIGHT COMPARTMENT LIGHTING PANELS EXTERNAL LIGHTS NAV BEACON STROBE WING INSP LOGO WHT OFF OFF OFF OFF OFF OON ONO ONO ONO OON LANDING TAXI/RECOG L WINGNLG R WING WINGTIP PULSE PULSE PULSE WINGTIP OFF OFF OFF OFF STEADYS STEADYS STEADYS ONO EXTERNAL LIGHTING PASS SIGNS EMER LIGHTS NO SMKG SEAT BLTS ELT ON ON ON OFF OFF OFF AUTOA AUTOA AARM ON FOR AVIATION EMER USE ONLY ARM/A PASSENGER SIGNS/EMERGENCY LIGHTS UNAUTHORIZED OPERATION PROHIBITED RESETR LIGHT SENSOR - ELT (Optional) COCKPIT LIGHTS INTEGRAL DIMMBR BRT DIMMBR BRT DIMMBR BRT L CTR R ON AUTO OOFF DIMMBR BRT MASTER DIMMBR BRT COCKPIT LIGHTS CB OVHD FLOOD BRT DIM ON DIM ON BBRTO OFFO OFFO OFF PBA EYE REF AR AE FLOOR GX_15_002 OFF BRT OFF BRT OFF BRT L CTR R DISPLAY COCKPIT LIGHTS INTEGRAL/MISC. DIM BRT DIM BRT DIM BRT L CTR R COCKPIT LIGHTS/FLOOD DISPLAY Page 4 Bombardier Global Express - Lighting INTEGRAL LIGHTING There are two types of integral lighting in the flight compartment: electroluminescent lighting consisting of an assembly layered within the panel and powered by AC, and incandescent lighting which is a bulb type lighting and can be AC- or DC-powered. The integral lighting is divided into five control areas as described in the previous illustration. A sensor is provided on the LIGHT SENSOR/ELT Panel in the flight compartment, to turn the integral lighting system on/off for day/night time lighting requirements. Light Sensor ELT ON FOR AVIATION EMER USE ONLY ARM/A UNAUTHORIZED OPERATION PROHIBITED RESETR GX_15_003 LIGHT SENSOR - ELT (Optional) Panel COCKPIT LIGHTS FLOOD/DISPLAY PANEL All flood/display lighting is controlled by switches located on the COCKPIT LIGHTS FLOOD/DISPLAY control panel in the center pedestal. The panel includes rotary knobs for the following areas: • Pilot instrument flood light and display lights • Copilot instrument flood light and display lights, and • Center instrument flood lights and display panels CTR FLOOD Control OFF/BRT – Controls the OFF selection and intensity (BRT) of the R FLOOD Control center instrument panel flood light. OFF/BRT – Controls the OFF L FLOOD Control selection and intensity (BRT) of the OFF/BRT – Controls the OFF right hand instrument panel flood selection and intensity (BRT) light on the copilot side panel. of the left hand instrument panel flood light on the pilot COCKPIT LIGHTS side panel. FLOOD OFF BRT OFF BRT OFF BRT L CTR R DISPLAY DIM BRT DIM BRT DIM BRT L CTR R GX_15_004 L DISPLAY Control R DISPLAY Control DIM/BRT – Controls the intensity DIM/BRT – Controls the intensity of the pilot instrument (primary CTR DISPLAY Control of the copilot instrument (primary flight and multifunctional) displays. DIM/BRT – Controls the intensity flight and multifunctional) displays. of the center instrument (EICAS and system) displays. Page 5 Bombardier Global Express - Lighting FLIGHT COMPARTMENT FLOOD LIGHTS Flood lights are installed at both crew stations for general illumination of the instruments. The flight compartment flood lights comprise: three LH and three RH side console instrument panel lights, and four center instrument panel lights. Dimming and off control of the lights is provided to the left, right and center areas of the flight compartment, using a single OFF/BRT rotary control knob for each area. The rotary control knobs are located on the COCKPIT LIGHTS FLOOD/DISPLAY control panel in the center pedestal. Variable controls enable the lights to change intensity gradually from off to full bright. DISPLAY LIGHTING Display lighting is provided for illumination of the pilot, copilot and center instrument panels. The L and R DISPLAY knobs control the Electrical Management System/ Control Display Units (EMS/CDU), Primary Flight Displays (PFDs) and the Multifunctional Displays (MFDs) for the pilot and copilot respectively. Right Side Console Control COCKPIT LIGHTS FLOOD OFF BRT OFF BRT OFF BRT L CTR R GX_15_005 COCKPIT LIGHTS FLOOD The CTR DISPLAY controls the EICAS primary display and the system display. This illumination is provided with a single switch DIM/BRT control. The left, right and center areas of the flight compartment have dimming control. These three rotary control knobs are located on the COCKPIT LIGHTS FLOOD/DISPLAY control panel in the center pedestal. Page 6 Bombardier Global Express - Lighting COCKPIT LIGHTS FLOOD/DISPLAY SCHEMATIC FLOOD LIGHTS COCKPIT LIGHTS FLOOD OFF BRT OFF BRT OFF BRT L CTR R MASTER MASTER WARNING/CAUTION WARNING/CAUTION HUD ROLL SPLRS ROLL SPLRS ROLL WARNING WARNING ROLL SEL SEL PLT CAUTION CAUTION CPLT ROLL ROLL DIM BRT OFF PLT CONT CPLT CONT Honeywell Honeywell Honeywell Honeywell Honeywell Honeywell THRUST HDGAP1 ASEL ATT 2 THRUST HDGAP1 ASEL ATT 2 MAG2 NO TAKEOFF CKPT (°C) FWD AFT CAB ALT 1300 MAG2 VAPP VNAV ADC 3 10400 HDG FMS1 PARK/EMER BRAKE ON HDG FMS1 VAPP VNAV ADC 3 10400 360 1.64 1.64 CABIN (°C) CABIN (°C) P 360 10500 315 END 30 0.00 315 10500 220 AT1 220 AT1 1.02 20 20 22 22 CAB RATE 0 9500 1.02 9500 20 20 19 20 20 LDG ELEV 20 20 210IAS F1 VTA N 10 0 N 210IAS F1 VTA ALT KKLM T/O KKLM ALT ATT 3 OXYGEN 90 % 3 ATT 200 33 TOC EPR 10 1 2 33 TOC 200 10 10 KABC -02 KABC -02 10 10 20 1906 LE 20 LUF 98.5 98.5 OUTFLOW VALVES LUF 1906 LE 20 185 10000 KGHJ 6 30 120 0 KGHJ 6 185 10000 180 F3 G 80 30 25.4 25.4 30 180 F3 G 80 4 S OPEN OPEN 4 S 10 10 KDEF +09 KDEF +09 10 10 170 RAD -04 13%% 13 1 2 -04 170 RAD 2 +12 N1 +12 2 300 300 160 M -02 OILQTY (QTS) -02 160 M 20 20 55 GEAR 55 20 20 LOC FL 11.5 ENG 11.5 FL LOC 150 EICAS 9500 150 EICAS 9500 NO BEARING BELOW 443 443 DN DN DN APU 5.2 NO BEARING BELOW HDGT HDG2 HDG 29.92 HDGT HDG2 HDG 29.92 0.450M RA 9 . 8NM +13 TCAS TEST 10 0 FEE RA 9 . 8NM +13 TCAS TEST 0.450M 0 T RES 6.0 TA 4 . 5NM -04 12 . 5NM IN 9 1 TA4.5NM-04 12.5NM FMS1 I I 4 FMS1 3 ET KDVT G ITT G 8 1 3 000 2 APU DOOR 11.2° ET KDVT 3 N 2 N DTK LOC1 33 3 00:10 0.05L ETE 1+36 N N 00:10 0.05L ETE 1+36 DTK LOC1 33 3 2 RPM100 EGT 650 2 360 WX TOC KKLM 7 3 WX TOC KKLM 360 6 SAT -56 START START mb/hPa ALT IN HG SAT -56 6 30 0 BRAKE TEMP 30 1 61.4 N2 61.4 10 1 3 6 4 29 9 2 1 KDEF KGHJ TAT -40 – TRIMS – 5 KDEF KGHJ TAT -40 E FL180 690 FF (PPH) 690 NU 03 06 03 03 FL180 E W 0 TAS 234 75 OIL TEMP 80 AIL TAS 234 W 0 4000 4000 4000 4000 1 12 OIL PRESS GSPD 345 51 49 220200180 250 GSPD 345 2 24 VOR 1 24 1 LX LX VOR 1 1 15 1 TERR 6.0 TERR 1 5 KNOTS 21 2 IAS S ADF 2 S ADF 2 2 INHIB LWD RWD BARO INHIB 2 HDG TOTAL FUEL (LBS) 25750 HDG 3 12950 0 12800 ND 3 330 0 STAB NL RUDDER NR 330 AIRSPEED LIMITS - (INDICATING SPEEDS) AIRSPEED LIMITS - (INDICATING SPEEDS) VSE(SLATSOUT,0°FLAPS)............225 VMO (BELOW8,000FT).............
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