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Question 1

The IRS display unit is located on the ____.

a. Center Instrument Panel
b. Aft Electronics Panel
c. Captain`s Side Panel
d. Aft Overhead Panel

Answer 1

d. Aft Overhead Panel

Question 2

How long does a full IRS alignment take?

a. Approximately 5 minutes
b. Approximately 10 minutes
c. Approximately 15 minutes
d. From 5-17 minutes depending on latitude

Answer 2

d. From 5-17 minutes depending on latitude.

Question 3

A steady white ALIGN light on the IRS Display Unit means ____.

a. an alignment fault is detected
b. the present position is inaccurate
c. alignment is progressing normally
d. the system is fully aligned

Answer 3

c. alignment is progressing normally

Question 4

A flashing white ALIGN light means ____.

a. no present position entered
b. unreasonable present position entry
c. both A and B are correct
d. alignment complete, ready for NAV

Answer 4

c. both A and B are correct

Question 5

How long can the Right IRS operate without AC electrical power?

a. 5 minutes
b. 30 seconds
c. 5 seconds
d. 30 minutes

Answer 5

a. 5 minutes

Question 6

If the amber FAULT light illuminates on the IRS Display Unit, it indicates the ____.

a. IRS has switched to ATTITUDE automatically
b. present position is inaccurate
c. ADIRU is in a self-test mode
d. related IRS system has detected a fault

Answer 6

d. related IRS system has detected a fault

Question 7

In flight, attitude information may be restored following a fault by selecting ____.

a. ATT
b. ALIGN
c. NAV
d. OFF

Answer 7

a. ATT

Question 8

The VOR course is set on the ____.

a. Mode Control Panel
b. EFIS Control Panel
c. Aft Electronics Panel
d. FWD Overhead Panel

Answer 8

a. Mode Control Panel

Question 9

The VOR identification is displayed on the ____.

a. VHF Navigation Control Panel
b. PFD
c. on-side FMC
d. Navigation Display

Answer 9

d. Navigation Display

Question 10

The right VOR information can be displayed and flown on the left ND by changing the ____.

a. VOR Standby Switch on the Aft Electronics Panel
b. IRS Switch on the FWD Overhead Panel
c. VHF NAV Transfer Switch on the FWD Overhead Panel
d. AUX NAV Switch on the Aft Overhead Panel

Answer 10

c. VHF NAV Transfer Switch on the FWD Overhead Panel

Question 11

DME frequencies are normally _____ tuned by the _____ as necessary for aircraft position updating.

a. manually/VOR
b. manually/pilot
c. automatically/GPS
d. automatically/FMC

Answer 11

d. automatically/FMC

Question 12

____ ILS receiver(s) is/are installed on the B737.

a. 1
b. 2
c. 3
d. 4

Answer 12

b. 2

Question 13

ILS course and glidepath are displayed on the pilots PFDs and ____.

a. Nav Display in MAP mode
b. Upper Multi-Function Display
c. Standby Attitude Indicator
d. Lower Multi-Function Display

Answer 13

c. Standby Attitude Indicator

Question 14

Marker beacon information is displayed on ____.

a. the PFD or ND
b. the PFD only
c. both the PFD and ND
d. the ND only

Answer 14

b. the PFD only

Question 15

____ GPS receivers are installed in the B737.

a. 1
b. 2
c. 3
d. 4

Answer 15

b. 2

Question 16

GPS provides position updates to the ____ and other aircraft systems.

a. FMC
b. IRS
c. ILS
d. VOR

Answer 16

a. FMC

Question 17

The white ALIGN light will flash to indicate ____.

a. an error in initial position information
b. the IRS Mode Selector has been moved to OFF
c. normal alignment
d. alignment complete, ready for NAV

Answer 17

a. an error in initial position information

Question 18

The right (IRS #2) ON DC light has illuminated. What is/are the possible causes?

a. All choices are correct
b. AC Main Bus 1 has failed.
c. The left IRS is being powered by the DC Standby Bus.
d. The airplane is on standby power

Answer 18

d. The airplane is on standby power

Question 19

This indication occurs at the gate because external power dropped off line and the aircraft is now on standby power. SELECT ALL of the indications (below) that would also be applicable.

a. The Master Caution and IRS annunciator lights illuminate
b. The ground call horn in the nose wheel well sounds.
c. The BAT DISCHARGE light illuminates
d. TRANSFER BUS OFF and SOURCE OFF lights illuminate

Answer 19

All 4 are correct

Question 20

In this situation, the indication occurs in flight. Assuming no corrective action is available, which statement about the operation of each IRS is correct?

a. The left IRS is inoperative. The right IRS is operating on battery power.
b. The left IRS will operate on battery power once the right IRS shuts down after 5 minutes.
c. The left IRS is operating normally. The right IRS will shut down in 5 minutes.
d. The right IRS will operate for 30 minutes and the left IRS will shut down in 5 minutes.

Answer 20

c. The left IRS is operating normally. The right IRS will shut down in 5 minutes.

Question 21

In flight, the Master Caution Lights and the IRS Annunciation light illuminate. These indications also occur (on the left IRS annunciations) which means that the _____.

a. Left IRS has failed and the unit is inoperative.
b. Battery Bus has failed since it is the DC power source for the left IRS
c. DC power source for the left IRS is not normal but the left IRS is still powered by the AC Standby
d. left IRS should continue to operate for 5 minutes and then fail

Answer 21

c. DC power source for the left IRS is not normal but the left IRS is still powered by the AC Standby

Question 22

Assuming no other IRS lights are illuminated, normal IRS operation can be restored by ____.

a. moving the left IRS Mode Selector to ALIGN and then back to NAV after 30 seconds
b. No action is possible. The left IRS will fail after 5 minutes
c. moving the left IRS Mode Selector to ATT and update the aircraft heading in line 5R in POS INIT Page 1/3 of the CDU
d. No action is required. The IRS is operating normally

Answer 22

d. No action is required. The IRS is operating normally

Question 23

What is the back-up DC power source for the Left IRS?

a. The Switched Hot Battery Bus
b. The Hot Battery Bus
c. The DC Standby Bus
d. A 24-volt DC battery separate of the aircraft battery that has a 30-minute life span

Answer 23

a. The Switched Hot Battery Bus

Question 24

The aircraft is in level flight at FL 350 when this indication is observed. The left IRS Transfer Switch is in the NORMAL position. In this situation, the Left IRS is not providing accurate _____.

a. information to the Captain’s instruments and the left IRS must be turned OFF
b. Attitude and heading information to the Captain’s instruments. To restore attitude information, select ATT on the #1 IRS Mode Selector and maintain wings level and constant airspeed tor 30 seconds
c. Information to the Captain’s instruments. To restore the system, select ALIGN on the #1 IRS Mode Selector, then select NAV after the ALIGN Light extinguishes (approximately 30 seconds)
d. Heading and attitude information to both the Captain’s and First Officer’s instruments. Move the IRS Transfer Switch to BOTH ON R to restore the FO’s information

Answer 24

b. Attitude and heading information to the Captain’s instruments. To restore attitude information, select ATT on the #1 IRS Mode Selector and maintain
wings level and constant airspeed tor 30 seconds

Question 25

The QRH directs you to place the #1 IRS Mode Selector to ATT. Once in this mode, the left IRS does not calculate. Select the most correct answer. a. acceleration or vertical speed, thus MAX deceleration should be selected on AUTO BRAKE Select Switch b. Position, ground speed, track, or winds. Heading is available after the ALIGN light is extinguished (approximately 30 seconds) c. acceleration, vertical speed, ground speed, track, position, heading, and winds d. All statements are correct.

Answer 25

c. acceleration, vertical speed, ground speed, track, position, heading, and winds

Question 26

To continue operations with the IRS Mode Selector Unit in this configuration, you must a. Monitor aircraft heading using a different source and periodically enter corrected heading in the CDU POS INIT Page or by selecting HDG/STS on the IRS Display Unit. b. Do nothing. The CDU will update corrected heading automatically from the ISFD c. Monitor aircraft heading using a different source and periodically reset corrected heading in the CDU POS INIT page. Also, select BOTH ON R with the IRS Transfer Switch d. Shut the left IRS off. Heading Information cannot be updated

Answer 26

a. Monitor aircraft heading using a different source and periodically enter corrected heading in the CDU POS INIT Page or by selecting HDG/STS on the IRS Display Unit.

Question 27

With the indications in flight on the left IRS panel, you should place the #1 IRS Mode Selector to ___. a. ALIGN while maintaining wings level for approximately 30 seconds, then move the selector back to NAV to regain attitude information b. ATT while maintaining wings level for approximately 30 seconds, then move the selector back to NAV to regain attitude information c. OFF momentarily, then move the selector back to NAV and maintain wings level and constant airspeed for approximately 30 seconds to regain attitude information d. ATT while maintaining wings level and constant airspeed for approximately 30 seconds and leave the IRS in ATT mode

Answer 27

d. ATT while maintaining wings level and constant airspeed for approximately 30 seconds and leave the IRS in ATT mode

Question 28

30 seconds after placing the #1 IRS Mode Selector to ATT the FAULT Light extinguishes. Mag compass heading is 127. To enter and regain current aircraft heading the crew should enter ______. a. 127 degrees in Line 5R (SET IRS HDG) of POS INIT Page 1 of the CDU b. 117 degrees in Line 5R (SET IRS HDG) of POS INIT Page 1 of the CDU c. the corrected Latitude and Longitude provided from the operating IRS in Line 1 R (LAST POS) of POS INIT Page 1 of the CDU d. the Reference Airport in line 1 L (REF AIRPORT) of POS INIT Page 1 of the CDU

Answer 28

a. 127 degrees in Line 5R (SET IRS HDG) of POS INIT Page 1 of the CDU

Question 29

In this scenario, which statement below most accurately describes flight limitations with the aircraft in this configuration? a. Cat II and/or Cat Ill approaches are not authorized. b. Neither autopilot can be engaged. c. Alternate brakes are not available. d. Land ASAP before the backup DC power source from the Switched Hot Battery Bus depletes (minimum 30 minutes).

Answer 29

a. Cat II and/or Cat Ill approaches are not authorized

Question 30

What information can be concluded by these indications while the aircraft is at the gate? a. The left IRS is not affected by this failure, however backup DC power has failed. b. The left IRS is being powered by the Switched Hot Battery Bus. c. The right IRS has failed after being powered by the Switched Hot Battery Bus for more than 10 minutes. d. Not enough information has been provided on the status of the left and right IRS Units.

Answer 30

b. The left IRS is being powered by the Switched Hot Battery Bus.

Question 31

While still at the gate you confirm that external power is connected. What additional conclusion can be made based on the indications shown for the left IRS panel? a. The right IRS is unpowered. b. The ground-call horn in the nose wheel well will not activate since normal AC power is on the busses. c. The left IRS is powered by the AC Standby Bus. d. AC power to the number 1 IRS has failed

Answer 31

d. AC power to the number 1 IRS has failed

Question 32

While the aircraft is still parked at the gate, another possible explanation for the indication above would be that _____. a. the ELEC Light is also illuminated due to a fault in the DC power system b. this is a normal momentary indication during an IRS alignment self-test c. the Battery Switch is OFF d. the STANDBY POWER Switch is in BAT

Answer 32

b. this is a normal momentary indication during an IRS alignment self-test