ADG200

Which lights are controlled by the landing lights panel?. wing inspection lights. recognition taxi lights. logo lights. rotating beacon.

Select three control panels associated with flight deck lighting. MISC LTS control panel. EMER LTS control panel. center pedestal control panel. PASS SIGN control panel. pilot lighting panel.

Select three lights that are controlled at the MISC LTS control panel. center pedestal integral lights. EICAS display intensity. overhead panel integral lights. compass light. circuit breaker panel integral lighting.

Which lights are controlled by the center pedestal lights control panel?. flight deck floor lights. FMS display intensity. standby compass lights. navigation lights.

The control for the chart reading light is located on.. center pedestal. overhead panel. pilot chart holder. flight attendant station.

The function of the IND LTS switch is to... control the intensity of indicator lights on the instrument panel. provide a lamp test of instrument panel. enable automatic dimming of instrument panel lights for ambient flight deck light level. allow selection of a blue filter for instrument panel lights for better vision on night approaches.

Identify which lighting has associated EICAS indications... flood lights and boarding lights. boarding lighting. reading lights. seat belt and no smoking lights.

Which lights are controlled at the PASS SIGN control panel?. ceiling and sidewall lights. passenger signs. reading lights. boarding lights.

Which condition will cause the SEAT BLTS sign to illuminate?. flap selection is greater than 0. landing gear is extended. cabin altitude exceeds 10,000 ft. passenger door closes at gate.

Controls for the service compartment lights are located... in the flight deck. in the galley. in each service compartment. in the galley and flight deck.

From the following list, select 3 lights associated with the Emergency Lighting System. floor track lights. ceiling floodlights. sidewall lights. boarding lights. floor level exit signs. seat belt signs. galley lights.

Which power source feeds the Emergency Lighting System?. main aircraft battery for 30 minutes duration. APU battery for 30 minutes duration. independent rechargeable batteries for15 minutes duration. main DC bus for an unlimited duration.

The Emergency Lighting System controls are located on the. overhead panel and flight attendant panel. copilot's and pilot's station. center pedestal. observer's station and flight deck.

Instrument panel and display lighting are controlled at the: pilot's / copilot's lighting control panel. center pedestal control panel. MISC LTS control panel. PASS SIGN control panel.

Passenger compartment lighting is controlled at the: pilot's / copilot's lighting control panel. MISC LTS control panel and forward attendant's panel. PASS SIGN control panel. forward attendant's panel.

The maintenance diagnostic information is displayed when... the MAINT switch behind the pilot is selected to MFD 1 or MFD 2. the data control panel that determines where the information is displayed. the MAINT switch behind the copilot is selected to PFD 1 or PFD 2. the EICAS control panel.

Name the EICAS page that automatically appears on ED 2, if the ED 1 display fails. status. synoptic. primary. menu.

Which control panels allow EICAS information to be shown on other displays?. source selector panel, air data reference panel. reversionary control panels, audio control panel. EICAS control panel, AUDIO WARNING panel. reversionary control panels, source selector panel.

What related indications may accompany a warning message?. amber light on a panel, amber fault on the EFIS or synoptic. red light on a panel, red fault on the EFIS or synoptic. white light on a panel, white system action on a synoptic. green light on a panel, green system status on a synoptic.

Which EICAS messages can be inhibited, if the left and right engine speeds are greater than 79% Ny and there is weight-on-wheels?. EGPWS. caution. advisory. status.

Which EICAS messages can be accompanied by a voice message?. warning. caution. advisory. warning and caution.

What other alerts accompany a red warning message?. single chime aural alert, flashing master warning lights. all associated panel lights flash red. triple chime aural alert, flashing master warning lights. flashing master caution, single chime aural alert.

What level of information does the green advisory messages provide?. status of a system, manually or automatically operated. aircraft configuration for a phase of fligh. most urgent, requires immediate actio. second in order of importance, requiresprompt action.

Which Crew Alerting System (CAS) message is second in order of priority?. advisory, green message. master warning, red message, triple chime. status, white message. master caution, amber message, single chime.

What setting can be changed through the MENU page?. flight plan. waypoints. cabin altitude. reset fuel used.

What type of information do the synoptic pages provide to the pilots?. system schematic data. inhibited system data. communication settings. maintenance diagnostics computer data.

From the list below, click on the four indications that are displayed on the primary page?. trim settings. flight number. engine parameters. brake temperature. warning messages. fuel quantity. APU door operation. advisory messages. cabin (auto mode). caution messages.

Which buttons on the EICAS control panel (EP) remainactive if the ECP computer fails?. STEP, STAT, MENU. PRI, STAT, HYD, FICTL. STEP, CAS, STAT, PRI. STAT, STEP, CAS.

From the list below, click on 4 pages that can be selected through the EICAS control panel (ECP). primary. FMS map. status. main. synoptic. NAV sector. top. menu.

During normal conditions, caution and warningswitchlights... begin all procedures related to non-normal operations. attract the pilots' attention to warning and caution conditions. inform pilots of the cause of the warning and caution conditions. help interpret the meaning of warning and caution conditions.

What is the function of the lamp driver unit?. interprets the DCU signal and lights theassociated switch lights. dim to bright adjustment of ED 1 and ED 2. supplies electrical power to the panel lighting. backup power supply for ED 1 and ED 2.

What test is performed by selecting the AURAL WARN TEST switch on the miscellaneous test panel?. test of the system's ability to disable anerroneous DCU audio warning. test of all EICAS audio outputs of theDCU. test of only the warning level audio outputs for flight controls. test of GPWS audio outputs only.

What messages are associated with the single chime?. status. advisory. warning. caution.

What do the data concentrator units (DCUs) do?. I concentrate and control display of EFIS data. allow pilot selection of synoptic pages. process and relay data to the propercomponent or EICAS display. control the cooling process of the EICAS displays.

From the list below, click on 5 items that are associatedwith the EICAS System Operation?. reversionary control panel. audio warning disable control panel. master warning and caution glareshields control panel. electrical power services control panel. EICAS control panel. audio control panel. lighting control panel. source select control panel.

How long can the EICAS screens remain operatingwithout cooling air?. 2 minutes. 5 minutes. 8 minutes. 15 minutes.

Which pages display by default on ED 1?. status, synoptic. primary, synoptic. status, menu. primary only.

From the list below, click on each of the 5 functions of theEICAS System, when in normal flight. automatic system monitoring. display of flight management data. integration of system information. tuning of radio navaids. colour logic for minimum / maximumlimits. aural alert warning messages. monitoring of tire pressure. integration of flight instrument systemintormation. reduced pilot workload.

Which control panel is used to set MFD formats, NAV source and bearing pointers and cross-side NAV data?. air data reference panel (ARP). display control panel (DCP). flight control panel. source selector panel.

The purpose of the comparator monitor display is. to ensure that the same data is shown to both pilot's. to calculate inputs from air data and attitude / heading computers to test the availability of reversionary control. to ensure AHRS alignment is complete. to identify valid NAV sources selected at the NAV source knob.

From the list below, click on 3 systems that receive variable air pressure inputs from the Pitot Static System. air data computer. standby compass. Cabin Pressurization System. standby altimeter indicator. display control unit.

IAS reference, overspeed warning and trend vector are all calculated by the... attitude heading computer. air data computer. display control unit. standby altimeter indicator.

The Attitude Heading Reference System calculates... attitude and synthetic magnetic heading and acceleration information. high integrity 3-axis rate and acceleration information. information for all the Air Data Reference Systems. cross-tracking of the air data computers.

Which MFD formats do NOT display weather radar or EGPWS terrain information?. navaid sector and HSI. FMS plan map and TCAS. HSI and FMS plan map. navaid sector and TCAS.

What standby instruments are available in the CRJ 200 flight deck?. compass, standby attitude indicator and air data computer. standby PFD, standby airspeed and MFD. standby attitude indicator, standby radio, standby HSI. standby altimeter indicator, standby attitude indicator, standby airspeed indicator and compass.

What type of data does the standby altimeter display?. indicated airspeed and altimeter. localizer and glide slope data. true airspeed indications. slip / skid data.

Which clock mode runs only with aircraft weight-off wheels?. LOC. ET. GMT. CHR.

Marker beacon identification is selected on the... air data reference panel (ARP). audio control panel (ACP). radio tuning unit (RTU). display control panel (DCP).

The amber 'H' displayed on the PFD and MFD indicates: navigation information is not available. DME hold function is selected on. marker beacon data is not available. HSI display is not available.

What is the restriction to FMS when in DME hold?. FMS cannot be manually tuned. FMS cannot be autotuned. no terminal DMEs can be selected. navigation is limited to within 100 miles of the DME station.

Bearing pointer #2 is selected as a: VOR. ADF. FMS.

Identify the two controls used for frequency selection and display of ADF: BRG switch on the display control panel. CRS knob on the flight control panel. standby tune control panel. radio tuning unit.

From the following list, select the 3 MFD formats that can display the ADF pointers. FMS plan. radar map. navaid sector map. TCAS. HSI. FMS map.

Altitude request' is an interrogation response provided by the transponders in... mode A. standby mode. Mode C.

Select the controls used to set ATC Mode A codes and the active ATC unit: RTU and ATC SEL knob on standby tune control unit. standby control unit and ATC SEL knob. FMS. mode A codes are preset for each aircraft by jumpers in ATC installation.

A TCAS resolution advisory indicates the: conflict has been resolved and the normal flight path is resumed. flight crew is to monitor the intruding aircraft. autopilot is capable of altering the flight path of the aircraft. flight crew must respond to intruder by altering flight path.

In order to view the TCAS display, the pilot must select the TFC button on the.... air data reference panel (ARP). audio control panel (ACP). radio tuning unit (RTU). display control panel (DCP).

The area highlighted on the PFD on the right, indicates the pilot is to... maintain the vertical speed range. perform a TCAS system test. visually confirm intruding aircraft. flyout of, or not enter the vertical speed range.

Identify the meaning of the indication highlighted on the TCAS display on the right. non-threat airplane. threat airplane at TA. threat airplane within 1200 feet. threat airplane at RA.

Aircraft ground clearance, glideslope deviation, and sink rate are monitored by the... EGPWS. TCAS. GPS. FMS.

From the list below, select 3 areas where EGPWS visual warnings are displayed. primary flight display (PFD). multifunction display (MFD). EICAS display 1 (ED 1). radio tuning unit (RTU). glareshield. control display unit (CDU).

Windshear warnings take priority over all EGPWS warnings except: below glideslope. unsafe terrain clearance. stall. excessive closure rate.

To generate the highlighted indication on the MFD, the pilot uses the... mode select switch. gain control. ground clutter suppression knob. tilt control.

A PAC alert on the radar screen of the multifunction display warns the pilot of: areas of the screen where the weather target is possibly incorrect. other aircraft in the flight path scanned by the radar. precipitation windshear. inaccuracies in a MAP mode display.

The GPS System provides navigation information to: VOR. AHRS. FMS. RTU.

From the list below, click on the 3 main components of the Flight Management System. control display unit. back up tuning unit. two servo motors. flight management computer. headphones. microphone. EFIS displays. marker beacon receivers.

The flight management computer... responds to signals from various ground stations. provides rate and acceleration information to the Attitude Heading and Reference System. provides information to the Air Data System. processes and generates navigation sensor information for display and autopilot control.

An amber data base date indicates: the FMS has malfunctioned. the flight plan has not been inputted into the FMS. the data base 28 day cycle has expired. the time zone has changed.

From the list below, click on the 4 displays and pages on which FMS data can be presented. primary flight display. multifunction flight display - FMS map. ED 1. status page. menu page. multifunction flight display - plan map. flight control synoptic page. multifunction flight display - HSI. multifunction flight display - FMS text pages.

Why is an initialization process required by the FMS?. to engage initial power up. to determine its present position. to set radio frequencies. to activate DMEOR sensors.

Based on the flight plan, FMS legs sequencing.. proceeds to each TO waypoint and generates steering commands to the new TO waypoint. determines the aircraft's present position. performs aircraft engine parameter and fuel quantity calculations for the next TO waypoint. calculates performance data.

Engine thrust limits, fuel management calculations and advisory vertical navigation. are functions that cannot be performed by the FMS. are engine and aircraft performance characteristics calculated by the FMS. are inputs required by the flight management computer. are essential to FMS operation.

Measured fuel management calculations use: data from aircraft performance tables relating to the flight plan. data from current fuel flow and ground speed indications. cannot be calculated by the FMS. inputs from the navigation data base.

The navigation sensors integrated by the FMS for aircraft positioning are: Attitude and Heading Reference System, DME/OR sensors. global position sensors, DEVOR sensors. total air temperature sensors, pitot / static probes and global position sensors. DME/VOR sensors only.

From the list below, select the 4 functions of the FMS. navigation sensor management. traffic collision advisory. radio tuning. flight planning. autopilot and flight director guidance. windshear conditions monitoring. aircraft identity reporting.

Which of the following statements best describes FMS VNAV?. provides advisory vertical navigation information for each phase of flight but no coupled steering. uses the flight management computer calculations of current winds, airspeed and heading to minimize overshoot. accomplished using data from aircraft thrust tables that relates to the flight plan. can provide coupled steering when the autopilot control is engaged by the FMS.

Where can the verification of automatic tuning be confirmed?. CDU and primary flight display. FMS plan map and CDU. CDU and radio tuning unit (RTU). CDU only.

What is the function of the scratchpad line?. clears the last character entered. show specific information related to the selected data. used to access specific data on different pages. displays information entered by the alphanumeric keys.

What is the function of the line keys?. used to recall messages from the FMC. used to select the function shown on the display line. used to show the current page title and number. used to adjust the vertical position of text fields.

Which statement best describes the POS INIT page?. appears on initial power up. displays FMS position information. provide menu of FMS functions. provides list of segments that make up the flight plan.

Which statement best describes the status page?. accessed through the PERF function key. acts as an alternative-tuning head for the listed frequencies. used to enter flight plan in the FMS. appears on power-up displaying navigation and performance data base information.