Flight Management Systems Flashcards
The FMC receives inputs from many sources. Which of the following inputs are used?
a. ADIRU and GPS
b. VOR/DME and ILS receivers
c. airplane systems
d. All of the above
d. All of the above
With only one FMC available, the system is capable of calculating data accurately.
a. Yes
b. No
a. Yes
The FMCs are completely independent and do not transfer or compare information between each unit.
a. True
b. False
b. False
With the FMC source select switch in NORMAL, the right CDU is controlled by the _____.
a. left FMC
b. right FMC
c. FMC on the side with the MA light
a. left FMC
When both FMCs are operating normally, each unit independently calculates its navigational position.
a. True
b. False
a. True
The two control display units (CDU) allow pilots to input data only to their respective FMCs if the RNP value exceeds the ANP value.
a. True
b. False
b. False
Which of the following is not used by the FMCs to determine position?
a. IRU
b. GPS
c. VOR/DME
d. ADF
d. ADF
With the loss of all navigational inputs to the FMC and GPS data is not available, how will it determine its position?
a. Computed off its last known position until landing.
b. Navigational position is lost.
c. Will compute off its last known position for 5 minutes.
d. IRS inputs only
d. IRS inputs only.
Will the FMC use a combination or a single source to determine its actual position?
a. Single source
b. Combination
b. Combination
The FMCs select a combination of inputs from navigation receivers to determine the position estimate. Which input has the highest weighted priority?
a. IRU
b. VOR radial/DME
c. Scanning DME
d. GPS
d. GPS
During a VNAV PATH descent, the FMC will calculate a descent path based on _____.
a. airspeed and altitude constraints only
b. altitude constraints, airspeed, and end of descent point
c. airspeed and end of descent point only
d. airspeed only
b. altitude constraints, airspeed, and end of descent point
During a derated takeoff, a further reduction by an assumed temperature can be taken.
a. Yes
b. No
a. Yes
The STA switch on the Displays Control Panel will display all ____ on the nav display.
a. NAVAIDs in the database
b. high and low altitude NAVAIDs if the range is selected to 40 miles or less
c. NAVAIDs but LOC and NDB
d. high altitude NAVAIDs
b. high and low altitude NAVAIDs if the range is selected to 40 miles or less
The IDENT page is accessed from the ____.
a. PROG key.
b. MENU page.
c. INIT/REF page, INDEX page, IDENT prompt, or at ground power-up.
d. FIX key.
c. INIT/REF page, INDEX page, IDENT prompt, or at ground power-up.
Initial position can be entered on the POS INIT page by which of the following?
a. GPS position
b. Reference airport, with or without specific gate
c. Manually entered lat/long
d. All of the above
d. All of the above
The PERF Performance Initialization (PERF INIT) page provides the means to enter aircraft weight, temperature, and wind parameters. What are the minimum parameters that must be input for the FMC to operate?
a. All boxed prompts
b. Aircraft weights
c. All blank lines
d. Cruise altitude
a. All boxed prompts
The selected approach reference speed will automatically update as aircraft weight changes.
a. True
b. False
b. False
On the approach/reference (APP/REF) page, current gross weight can be manually entered.
a. True
b. False
a. True
In addition to the approach reference speed displayed on the APP/REF page, which additional information is displayed?
a. Go-around N1
b. Runway length in feet
c. Approach freq, ident, and course
d. B and C are correct
d. B and C are correct
When multiple waypoints or NAVAIDs with the same identifier are in the database, the FMC will automatically display all waypoints.
a. True
b. False
a. True
Which page is used to display SIDs and STARs?
a. ROUTE
b. ARR/DEP
c. MENU
d. INDEX
b. ARR/DEP
When the final load closeout is received, the pilot must check that the _____ has been entered on the PERF page for FMC calculation.
a. fuel and ZFW
b. gross weight
c. takeoff weight
d. ZFW
d. ZFW
Thrust limits for takeoff, climb, cruise, and go-around must be selected manually.
a. True
b. False
b. False
The thrust reduction altitude, where automatic thrust reduction from takeoff to climb limit occurs, is fixed at 1000 feet AGL, and cannot be changed.
a. True
b. False
b. False