题目内容

Fuel flow and drag factors are displayed on the PERF FACTORS page in FMCS BITE. These factors are:

A. initialized to 0.0 at power up
B. computed by the FMC for each flight
C. manually inserted on the PERF FACTORS page
D. automatically updated during the nav data base load

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The FMCS BITE SENSOR STATUS page:

A. appears automatically when a sensor fails
B. stores sensor failures during flight
C. is blank if all sensors are functioning properly
D. shows current status of the sensors associated with the FMC

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The VHF navigation receivers and DME interrogators can be automatically tuned by the:

A. MCP
B. FCCs
C. FMC
D. IRUs

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AN FMC failure is shown by:

A. the message ‘FMC FAIL’ in the CDU scratch pads
B. red ‘FAIL’ lights on the CDUs
C. blank displays on the CDUs
D. ‘FMC’ displayed on the CDUs, amber ‘FAIL’ lights on the CDUs, and the ‘FMC’ light illuminated on each autoflight status annunciator

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The amber ‘FMC’ light on the autoflight status annunciators will illuminate if there is:

A. a CDU or FMC failure
B. an alert message or FMC failure
C. an advisory message
D. an entry error advisory message

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Fuel flow and drag factors are displayed on the PERF FACTORS page in FMCS BITE. These factors are:

A. initialized to 0.0 at power up B. computed by the FMC for each flight C. manually inserted on the PERF FACTORS page D. automatically updated during the nav data base load

The FMCS BITE SENSOR STATUS page:

The VHF navigation receivers and DME interrogators can be automatically tuned by the:

AN FMC failure is shown by:

The amber ‘FMC’ light on the autoflight status annunciators will illuminate if there is:

A. initialized to 0.0 at power up
B. computed by the FMC for each flight
C. manually inserted on the PERF FACTORS page
D. automatically updated during the nav data base load