CDC 2A354C Volume 1. F-16 Attack Control Systems
The F-16 fighting falcon is a single engine fighter jet initially developed for the American Air Force. CDC 2a354c Volume 1. F-16 Attack Control Systems is specifically designed to test your knowledge on this fighter jet. All the best and enjoy.
- 1.The most important responsibility of the EEFCC is to integrate the entire F-16 avionics system by serving as the
- A.
Backup bus controller for the serial digital buses
- B.
Primary bus controller for the serial digital buses
- C.
Backup bus controller for the parallel buses
- D.
Primary bus controller for the parallel digital buses
- 2.The fault gathering and reporting center of the weapons control system is the
- A.
Heads-down display
- B.
Heads-up display
- C.
Stores management system
- D.
Enhanced expanded fire control computer (EEFCC)
- 3.As directed by the EEFCC OFP, all arithmetic calculations are performed by the
- A.
Core memory unit
- B.
Serial-digital interface
- C.
I/O unit
- D.
CPU
- 4.What is the core memory size of the EEFCC
- A.
256K
- B.
512K
- C.
256M
- D.
512M
- 5.Where are MUX bus transformers located and what's their purpose?
- A.
In the EEFCC; communicates with slave terminals
- B.
On MUX matrix assemblies; provides impedance matching and short-circuit protection
- C.
In the EEFCC; provides impedance matching and short-circuit protection
- D.
On MUX matrix assemblies; communicates with slave terminals
- 6.When the EEFCC determines if a transmitted word is good or bad, what type of bit aids in this?
- A.
Identity
- B.
Response
- C.
Odd Parity
- D.
Even Parity
- 7.Which statement best describes the self-test of the EEFCC?
- A.
The EEFCC only utilizes BIT
- B.
It's run only when commanded by the operator
- C.
It's a self-running test and when complete, starts over again
- D.
It's performed only once at GAC power-up
- 8.What type of battery does the MMC contain, and what is the battery's purpose?
- A.
An alkaline 3.6 volt, C size batter; it provides a back-up capability in the event of failure, removal, or recharging of the aircraft battery.
- B.
A lithium 3.6 volt, D size battery; it provides a back-up capability in the event of failure, removal, or recharging of the aircraft battery.
- C.
An alkaline 3.6 volt, C size battery; provides primary power to the MMC
- D.
A lithium 3.6 volt, D size battery; it provides primary power to the MMC
- 9.If you want standby power to all SMS stores stations that have inventory loaded in memory, which switch would you use?
- A.
MMC power switch
- B.
SMS standby power switch
- C.
MMC master switch
- D.
Stores station switch
- 10.The two internal MMC buses that provide communication between modules are the
- A.
Parallel intermodule/ serial digital test and maintenance bus
- B.
Parallel intermodule/ serial digital test and evaluation bus
- C.
Discrete digital data bus/ parallel test and maintenance bus
- D.
Discrete digital data bus/ parallel test and evaluation bus
- 11.The EEFCC and MMC MUX bus architecture is basically the same except the
- A.
MMC doesn't use the A-MUX or B-MUX
- B.
EEFCC doesn't use the A-MUX or B-MUX
- C.
MMC has two additional buses; the C-MUX and F-MUX
- D.
EEFCC has two additional buses; the C-MUX and F-MUX
- 12.Which two scenarios will generate a MMC auto restart when the MMC fails?
- A.
Software failures and hardware failures
- B.
Software failures and slave terminal failures
- C.
Hardware failures and slave terminal failures
- D.
Hardware failures and MUX bus failures
- 13.How many MFL memory locations does the MMC contain?
- A.
15
- B.
16
- C.
17
- D.
18
- 14.The MMC BIT is
- A.
Interruptive, meaning the normal operation of the subsystem is maintained during the actual BIT
- B.
Nointerruptive, meaning that normal operation of the subsystem is maintained during the actual BIT
- C.
Interruptive, meaning that normal operation of the subsystem is not available until the BIT has been completed
- D.
Noninterruptive, meaning that normal operation of the subsystem is not available until the BIT has been completed
- 15.Which F-16 ADIS component contains a microprocessor, firmware, interface electronics, power supply, and other electronics necessary to manage data transfer?
- A.
DTU
- B.
DTC
- C.
DTCP
- D.
DTS/DTC
- 16.Which F-16 ADIS component is a transportable, nonvolatile memory, which interfaces aircraft systems through the DTU
- A.
DTD
- B.
DTC
- C.
DTCP
- D.
DTDU
- 17.Considered the heart of the UFC system, this component is a programmable computer that controls and interfaces the UFC
- A.
CDEEU
- B.
MMC
- C.
MFD
- D.
DEEU power supply
- 18.On what F-16 would you find a PFLD
- A.
F-16 A/B block 15
- B.
F-16 C/D block 40 only
- C.
F-16 C/D block 40 and up
- D.
F-16 C/D blocks 25 through 32
- 19.If the PFLD fails but the UFC set is still functioning, the PFLD data can be displayed on the
- A.
HUD
- B.
DED
- C.
MFD
- D.
MFDS
- 20.Identify the four priority override keys which are located across the top of the ICP and IKP
- A.
COM 1, COM 2, INS, LIST
- B.
COM 1, COM 2, IFF, LIST
- C.
COM 3, COM 4, INS, LIST
- D.
COM 3, COM 4, IFF, LIST
- 21.All of the following are functions provided by the DCS except
- A.
Page title option access
- B.
SOI selection
- C.
Positioning the DED asterisks
- D.
Frequently accedded data pages
- 22.On the F-16 UFC, which page is more or less a continuation of the LIST page?
- A.
BNGO page
- B.
STPT page
- C.
MISC page
- D.
CNI page
- 23.UFC priority functions are made available through the priority function keys, only when the
- A.
CNI page is displayed on the DED
- B.
MISC page is displayed on the MFD
- C.
MISC page is displayed on the DED
- D.
CNI page is displayed on the MFD
- 24.When do the UFC provide the capability to enter numeric data through the ICP/IKP?
- A.
After the NUMERIC key is depressed
- B.
Only when entering navigation coordinates
- C.
Anytime a DED page is displayed
- D.
When the asterisks are positioned about a numeric data field
- 25.When the CNI page is displayed, how many function values can be changed using the increment/decrement switch?
- A.
Two
- B.
Three
- C.
Four
- D.
Five
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