The B737-800 has a ______ FMC installation? single dual triple.
With the FMC Source Select Switch in the NORMAL position, CDU’s and autothrottles are controlled by the _____ FMC. right center left.
Placing the FMC Source Select Switch to BOTH ON R selects the______ for all FMC operations. The ______ map will annunciate _______. right FMC; Left; “FMC R” right FMC; Right; “FMC L” left FMC; Right; “FMC L”.
On the FANS Multi-Purpose Control Display Units (MCDUs), the _____ key replaces the CLB, CRZ, and DES keys. Selecting this key will display the active performance page for the active phase of flight. Using the PREV PAGE and NEXT PAGE keys allows access to the other performance pages. VNAV ATC FMC COMM.
Flight plan and load sheet information provides performance information to initialize ________. VNAV LVL CHG all answers are correct.
The takeoff phase of the FMC begins with __________ and extends to the thrust reduction altitude where climb thrust is normally selected.
the selection of TO/GA the advancement of the thrust levers the selection of LNAV.
VNAV can perform a descent in either of two modes - ____________________. level change or vertical speed path descent or speed descent all answers are correct.
Pressing the ______ key on the CDU shows the pages for data initialization or for reference data. MENU INIT REF ATC.
Pressing the ______ key on the CDU shows the page to input or change origin, destination, or route. MENU RTE LEGS.
Pressing the ______ key on the CDU shows the page to input or change departure and arrival procedures. DEP ARR ATC LEGS.
Pressing the ______ key on the FANS Multi-Purpose Control Display Unit, MCDU shows currently active performance page (CLB, CRZ, DES) VNAV RTE LEGS.
Pressing the ______ key on the CDU shows the page to create reference points on map display. ATC N1 LIMIT FIX.
Pressing the ______ key on the CDU shows the page to evaluate or modify lateral and vertical route data. LEGS PROG FMC COMM.
Pressing the ______ key on the CDU shows the page to create holding patterns and show holding pattern data. HOLD PROG FMC COMM.
Pressing the ______ key on the CDU shows the page to view dynamic flight and navigation data, including waypoint and destination ETAs, fuel remaining, and arrival estimates. RTE PROG FIX.
Pressing the ______ key on the CDU shows the page to choose subsystems controlled by CDU. MENU N1 LIMIT FIX.
Pressing the ______ key on the CDU shows the page to view or change N1 thrust limits. MENU N1 LIMIT FIX.
Pressing the ______ key on the CDU shows the previous page of related pages (for example, LEGS pages). VNAV PREV PAGE FIX.
Pressing the ______ key on the CDU shows next page of related pages (for example, LEGS pages). ATC NEXT PAGE PROG.
Pressing the ______ key on the CDU makes data modification(s) active, and extinguishes the light. EXEC MENU PROG.
The ________ is illuminated white when active data is modified but not executed. EXEC light FMC P/RST A/T P/RST.
Pressing the ______ key on the CDU is used to view or change climb data. DES CLB PROG.
Pressing the ______ key on the CDU is used to view or change cruise data. DES CLB CRZ.
Pressing the ______ key on the CDU is used to view or change descent data. DES CLB CRZ.
The ______ are the aircraft’s sole source of attitude and heading information, except for the standby attitude indicator and standby magnetic compass. GPSs IRSs FMCs.
During IRS alignment, when the ______ light extinguishes and the ______ light illuminates, the IRS has begun the alignment process. ON DC; FAULT ON DC; ALIGN DC FAIL; FAULT.
If IRS alignment is lost in flight, the navigation mode (including present position and ground speed outputs) is ________________. is in standby for 5 minutes, then may be realigned may be restored provided DC power is available inoperative for the remainder of the flight.
Should either IRS fail, the _________ is used to switch all associated systems to the functioning IRS. FMC display control selector IRS transfer switch.
Should either VOR receiver fail, the _________ enables selection of the opposite VHF NAV receiver for display. FMC VHF NAV transfer switch IRS transfer switch.
Backup power to the _____ IRS is automatically terminated if ___ power is not restored within 5 minutes. right; AC right; DC left; AC.
The TEST position of the display selector on the IRS Display Unit ______________. is inoperative may only be used during alignment may be used any time after alignment.
The TK/GS position of the display selector on the IRS Display Unit displays present true track course in the left window. The right window displays ____________. present ground speed time to next fix eta to destination.
The PPOS position of the display selector on the IRS Display Unit displays ____________. present longitude present latitude all answers are correct.
FMNV6.110.34
The WIND position of the display selector on the IRS Display Unit displays ____________. ground speed information ground wind information inflight true wind direction and speed.
The HDG/STS position of the display selector on the IRS Display Unit displays true present heading in the left window. The right window displays ____________. time to next fix applicable maintenance status codes fuel remaining in pounds X 1000.
The System Display Selector on the IRS Display Unit selects the left (L) or right (R) IRS for __________. Data Display power selection master.
If the IRS Mode Selector (Left or Right) is placed in the OFF position ___________. respective IRS alignment is lost the respective system is rebooted after 5 minutes after 30 seconds, placing the switch to NAV will realign the IRS in flight and regain navigation function.
When placing the IRS mode selector to ALIGN for initial alignment, the aircraft must be ________. stationary on the ground straight and level.
With the IRS mode selector in _________, the IRS provides full data to aircraft systems for normal operations. ATT NAV ALIGN.
With the IRS mode selector in _________, the IRS provides attitude and heading only. ATT NAV ALIGN.
An illuminated flashing ALIGN Light on the Aft Overhead Panel indicates that alignment cannot be completed due to IRS detection of __________. a significant difference between previous and entered positions or an unreasonable present position entry no present position being entered all answers are correct.
The _______ light illuminates when a system fault affecting the related IRS ATT and/or NAV modes has been detected. FAULT DC FAIL ALIGN.
The _______ light illuminates when DC power for the respective IRS is not normal. FAULT DC FAIL ALIGN.
The B737-800 has ______ independent GPS receiver(s). one two three.
An illuminated amber GPS light indicates ______________. failure of both GPS sensor units standby GPS operation GPS alignment is occurring.
An illuminated amber ILS light (as installed) indicates ______________. failure of both ILS sensor units standby ILS operation ILS alignment is occurring.
An illuminated amber GLS (as installed) light indicates ______________. failure of both GLS sensor units standby GLS operation GLS alignment is occurring.
Placing the transponder selector to 1 selects ___________. transponder No. 1 transponder No. 2 transponder No. 3.
The Air Traffic Control (ATC) Code Indicator is shown on the transponder and the code is set via the ___________. FMC ROTATE knob FMC or ROTATE knob.
Pushing TEST on the Transponder Mode Selector ________________. tests the SEL CAL starts an ATC transponder functional test all answers are correct.
Placing the Transponder Mode Selector to ALT RPTG OFF (altitude reporting off) ________________. operates the transponder without altitude reporting operates the transponder with altitude reporting off until airborne all answers are correct.
Placing the Transponder Mode Selector XPNDR (transponder) ________________. operates the transponder with altitude reporting operates the transponder with altitude reporting off until airborne operates the transponder in ground mode.
Pushing the Identification (IDENT) switch the Transponder Panel ________________. sends an emergency signal tests the transponder on the ground transmits an identification signal.
How is a transponder malfunction indicated? an illuminated master caution light along with the IRS system annunciator an illuminated master caution light along with the IRS system annunciator only on recall an illuminated transponder (XPNDR) FAIL light on the transponder panel.
Placing the altitude (ALT) SOURCE selector to 1 enables ___________. altitude reporting from AHRS No. 1 altitude reporting from air data computer No. 1 altitude reporting from air data computer No. 2.
Does the weather radar automatically limit the detection of turbulence regardless of the selected range? Yes No.
A displayed color of magenta on the radar indicates ___________ . strong returns hail heavy turbulence.
A displayed color of red on the radar indicates ___________ . strong returns, areas of heaviest rainfall intense to extreme turbulence medium returns, moderate rainfall.
A displayed color of yellow on the radar indicates ___________ .
strong returns, areas of heaviest rainfall intense to extreme turbulence medium returns, moderate rainfall.
A displayed color of green on the radar indicates ___________ strong returns, areas of heaviest rainfall intense to extreme turbulence light returns, light rainfall.
If the RGT (right) tilt on the weather radar panel is inoperative, pushing the right ________ will transfer the other (left) map display selections to the related (right) map. MAP TFR IDNT.
Pushing the WX/T (turbulence) switch on the weather radar, displays __________. weather radar returns and turbulence weather radar returns turbulence.
Pushing the WX switch on the weather radar, displays __________. weather radar returns and turbulence weather radar returns turbulence.
Pushing the MAP switch on the weather radar, displays __________. weather radar returns at selected gain level ground returns at selected gain level the opposite MAP display.
Pushing the IDNT switch on the weather radar, __________. identifies the operational weather radar suppresses ground return in WX and WX/T modes transmits an identification signal.
Pushing the TEST switch on the weather radar, __________. tests weather radar system operation without transmitting if on the ground with and the thrusts levers are not advanced for takeoff, tests the predictive windshear system all answers are correct.
To tilt the radar antenna up, rotate the TILT Control ________. clockwise counterclockwise.
On the VHF Navigation Control, pushing the TEST switch with a VOR frequency tuned and a course of _________ selected will display a VOR fail flag. 000 180 090.
On the VHF Navigation Control, pushing the _________ moves the frequency in the standby window to the active frequency window. mode switch test switch transfer switch.
The illumination of a Gain Uncalibrated (GAIN UNCAL) light, indicates ______. the related radar requires recalibration by maintenance the related gain control is in an uncalibrated position the related weather radar is inoperative.
On the VHF Navigation Control, rotating the frequency selector manually selects the ________ frequency. active standby.
Each pilot has a set of marker beacon lights that show the outer marker (OM) as cyan, middle marker (MM) as amber, and the inner marker (IM) as _______. magenta green white.
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