FLIGHT MANAGEMENT AND NAVIGATION Flashcards

1
Q

What information do the IRSs provide?

A

Attitude, heading and position information (including groundspeed)

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2
Q

Are they (IRSs) dependent on, or independent of, external navigation aids?

A

Independent

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3
Q

How is the GPS activated and what does it provide data for?

A

GPS is always on when aircraft is powered

provides an accurate aircraft geographical position to the FMC
Clock
Transponder

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4
Q

With the FMC SOURCE select switch in NORMAL, which FMC is primary and what does it control?

A

L FMC is PRIMARY and provides information for CDUs and autothrottles

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5
Q

Describe the criteria for airports included in the nav database`

A

5000x100ft runway and IFR Approach

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6
Q

When using the Autothrottle system, how are reference thrust limits calculated, and how is thrust equalization maintained?

A

reference thrust limits calculated by the FMC

thrust equalization maintained through the electronic engine controls (EEC)

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7
Q

How are the FMCs operated?

A

Uses flight plan information entered by the Crew into the MCDU
Left is master
Left shares data with the Right Controls the A/T
Provides information to the Display Units

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8
Q

Where do the FMCs receive their inertial data from?

A

The IRS through the ADIRU from the corresponding side (ex left ADIRU to FMC 1). If the on-side ADIRU malfunctions or it is in the ATT or ALIGN mode, the FMC uses the data from the other ADIRU.

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9
Q

What does the FMC use to determine position?

A

In this order:
GPS
—>IRS
——->Ground based navaids (except for ADF)

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10
Q

If GPS data is not available, how does the FMC calculate the present position?

A

IRS then ground based navaids If GPS data is not available, the FMC calculates the present position based on IRS data.

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11
Q

FMC position updates from navigation sensor positions are used in what priority order?

A

FMC position updates from navigation sensor positions are used in the following priority order:
- GPS
- two or more DME stations
- one VOR with a co-located DME
- one localizer and co-located DME - one localizer
NOTE: DME updating is defaulted OFF

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12
Q

How does the FMC calculate a descent path during a VNAV PTH descent?

A

Starts at the bottom of descent and works backward, taking into account altitude and speed constraints and restraints for an idle descent, factoring in winds and anti ice

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13
Q

How can you further reduce a derated takeoff?

A

Select a derated setting in FMC and use an assumed temp to further derate

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14
Q

What is the lateral navigation (LNAV) intercept criteria?

A

Inside 3 miles it will automatically intercept
Outside 3nm you must be:
- Intercept angle less than 90deg to the course with a valid TO waypoint

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15
Q

When does IRS position and ground speed information become available and up to how long could it take

A

after it is aligned
Alignment time varies from 5 to 17 minutes depending on the aircraft latitude
High latitude could take up to 17 minutes

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16
Q

When does an ALIGN (white) light illuminate steady?

A

Respective IRS is in:
ALIGN mode
Initial ATT mode, or
Shutdown cycle

17
Q

What does a flashing ALIGN light (white) on the IRS panel during preflight indicate?

A

Fault in alignment process
Gross error with position entry
No Position has been entered

18
Q

If IRS AC power has failed, how long can the right IRS operate?

A

5 minutes then you’ll still have 60 min on the left IRS You would see an ON DC light

19
Q

If a system fault affecting the related IRS ATT and/or NAV modes has been detected, what indication will you get?

A

FAULT light

20
Q

On the Boeing 737-NG, how many GPS receivers are installed?

A

2 GPS receivers

21
Q

What will happen if both ON DC lights (amber) lights illuminate?

A

Both systems automatically switch to backup DC power from the Switched Hot
Battery Bus
After 5 minutes, right IRS will be powered off and left will stay powered for 60 minutes

22
Q

What could cause the call horn in the nose wheel well to sound while the aircraft is on the ground?

A

IRS is on battery power alerting that a battery drain condition exists

23
Q

If position information while programming the FMC CDU on the ground is contradictory, what indication, if any, will alert the crew to this?

A

Flashing white ALIGN light