T-38C Systems

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The TCAS switch on the AAP controls the transponder power for normal air traffic control functions. A. True B. False: Answer: A
When the mode switch on the the AAP is place in the NORM position, which of the following is true? A. NAV Backup Control Panel is active B. NAB Backup Control Panel is active C. UHF, VHF, VID, and TACAN systems are controlled by the MDP vi: Answer: C
The channel select button on the UHF Backup Control Panel ___. A. Selects the next preset channel when depressed B. Toggles between prest and manual freq selection C. Toggles between the Main and Both modes of operation D. Alternately: Answer: B
Describve the steps to change the freq associated with a channel on the UHF Backup Control Panel.: Answer:
A. Press and hold the channel select button for more than three seconds.
B. Rotate the freq/channel selector to the disired channel. The letter P will be displayed in front of the channel number to indicate that the program mode is active.
C. Press the mode button which will cause the freq row to start flashing.
D. Enter the new freq with the freq/channel selector knob.
E. Momentarily press the mode button to set the new preset. Press the channel select button to exit the program mode.
In the event of MDP failure, the NAV Backup Control Panel can be used to select any ___ frequency. A. VOR or ILS B. VOR, ILS or VHF C. VOR, ILS or UHF D. VOR, TACAN or NDB: Answer: A
When the ON/OFF switch on the NAV Backup Control Panel is in the BRG position, what information is displayed? A. Displays bearing to the selected TACAN station B. Displays bearing to the selected VOR station if received C. Displays bearing: Answer: B
Placing the microphone switch onthe rear cockpit audio panel to the HOT position enables hot mic for that cockpit only. A. True B. False: Answer: B
Placing the TCAS SIL/ACT swith in the SIL position inhibits the aural traffic warning generated by the TCAS. A. True B. False: Answer: A
To quickly return to the primary flight reference (PFR) display on the mFD, press the ___ on the HOTAS. A. Master Mode Switch (MMS) B. Weapon Mode Switch (WMS) C. Default Display Switch (DDS) D. Nose Wheel Steering button (Weight Off: Answer: C
Pressing the PTT in both cockpits at the same time on different radios (i.e. UHF and VHF) will result in transmissions from both pilots on different frequencies simultaneously. A. True B. False: Answer: A
The standby instruments are provided for use as backup flight instruments if the primary flight reference system malfunctions. A. True B. False: Answer: A
With power failure, the standby attitude indicator will provide a minimum of ___ minutes of useful attitude information. A. 3 B. 6 C. 9 D. 15: Answer: C
Each functional display on the EED, such as the EGT indicator is formatted to include an analog scale, moving, digital readout, and color-coded range and limit makers. A. True B. False: Answer: A
When an individual internal EED sensor fails, such as the tachometer RPM sending unit, the pointer and digital readout display are blanked and replace with ___. A. 000 B. ---(dashes) C. FAIL D. OFF: Answer: C
When a RPM or EGT limit is exceeded on the EED, this will be indicated by ___. (Select more than one.) A. The white pointer and display title turning red B. The individual display title flashing C. The center digital number turning red onl: Answer: A,C
The VTR will record the MFD, HUD or both when the following event occurs: A. The VTR tape is inserted in the VTR B. Select the VTR page on the UFCP and toggle from STOP to MFD, HUD, or CMB as desired. C. The landing gear lever is raised: Answer: D
Which of the following is NOT a selectable VTR recording mode? A. HUD B. Front MFD C. Rear MFD D. Front and rear MFD combined: Answer: B
The Data Transfer System (DTS), consisting of the Data Transfer Drive (DTD) and Data Transfer Cartridge (DTC), is used to upload/download mission data stored in the aircraft ___. A. Air Data Computer (ADC) B. Mission Display Processor (MDP): Answer: D
When loading data to or from the MDP and DTC via the DTS menus on the MFD, a data transfer failure is indicted by: A. A red flashing "LOAD" title on the DTS display B. A "NO TRANSFER" message on the DTS display C. A fla: Answer: A
Initiation and termination of MDP data recording are normally automatic, but either crewmember can manually select this option via the MFD. A. True B. False: Answer: B
The UFCP is inoperative if the MDP fails or is off A. True B. False: Answer: A
What does the [down arrow] symbol indicate when it is displayed next to a window item? A. The function/setting is active or selected B. A menu page is below the current level which can be accessed by pressing the adjacent OSB C. The select: Answer: B
The U BRT rocker switch on the UFCP controls the brightness of the panel window displays, LED, OSBs, and all function and control keys. A. True B. False: Answer: B
In which of the following cases must the ENT key on the UFCP be pressed to complete the data entry? A. After the last character is entered fillin a fixed length field B. After the last character is entered filling a non-fixed length field: Answer: C
What is teh indication that you have entered invalid data on the UFCP? A. The invalid data display flashes B. The data display will change to all dashes in the field C. The last valid data will reappear and flash D. The data will be e: Answer: A
If a typing error is made on the UFCP before all of the data has been entered, pressing ___ will clear the field and display dashes again for reentry of the correct data. A. The RTN key B. The ETN key C. any function key D. the adjace: Answer: D
Which of the following methods can be used to return from a function display's primary page to the basic display? A. Press the RTN key B. Press the current function key again C. Wait approx 20 seconds, and return will be automatic from all: Answer: D
The function displays are manually selected by pressing the applicable function key and are enabled regardless of the current display or operating range. A. True B. False: Answer: A
The normal ATC transponde codd (IFF squawk) is set or changed on the ___. A. EGI function display B. SET function display C. IFF function display D. FPL function display: Answer: C
If the MDP is powered down and back up during flight due to an electrical malfunction, the current (barometric press) altimeter setting will need to be reentered if it is other than the default setting of 29.92. A. True B. False: Answer: A
The primary flight display (PFR) can be selected directly from any MFD display using either the PFR/HSD MOSB or default display switch on the control stick. a. True b. False: Answer: A
Which of following MFD controls/displays is used to select the course displayed in the CRS window? a. Numeric menu display MOSBs b. Course menu display MOSBs c. Course select rocker d. Manual heading select rocker: Answer: C
Which of the following actions is the correct procedure for selecting the single letter â€œBâ€ on the alphabetic menu? (Refer to Figure 4-3) a. Press ML-1 once b. Press ML-1 once followed by MB-6 (NEXT) c. Press ML-1 twice delaying a: Answer: D
Which of the following methods can be used to clear/correct an invalid data entry or option selection that continues to blink after the validity test? a. For cyclical option selections, press the MOSB again to select another (valid) option.: Answer: D
The â€œarmâ€ extending from the Nadir and Zenith symbols on the EADI always point in the direction of the nearest horizon, except at exactly 90Â° dive/climb angle when they point towards the ghost horizon line. a. True b. False: Answer: A
What do the minimum and maximum G values that are displayed with oversized ticks on the G meter scale indicate for a clean aircraft? a. The absolute minimum/maximum G limits that remain unchanged during the flight. b. The current minimum/m: Answer: B
Which type of intruder aircraft does the red square [ â– ] symbol represent on the EHSI/HSD TCAS display? a. Threat aircraft at RA level b. Threat aircraft at TA level c. Proximity aircraft d. Non-threat aircraft: Answer: A
Which of the following TCAS display scales (range in NM) is the default setting? a. 2.5 NM b. 5.0 NM c. 10 NM d. 20 NM e. None of the above: Answer: C
Which of following is true when a PFL failure is detected? a. A flashing AVIONICS caution message is displayed on the HUD and MFD. b. The detected failure is recorded on both the PFL and MFL, which can be viewed via the MALF display. c. Th: Answer: D
Which of the following flight reference displays are available on the MFD backup display with MDP failure? a. EADI and EHSI b. Indicated airspeed c. Pressure altitude d. All of the above: Answer: A
How many Training Zones can be downloaded from the DTC and available for display on the MFD HSD? a. 5 b. 10 c. 20 d. 40: Answer: B
What information does the Divert modes Range (RNG) profile display? a. The flight profile for an optimum climb/cruise best range airspeed and altitude to the currently selected steer point using minimum fuel. b. The flight profile intended: Answer: D
In the NAV master mode with the landing gear retracted, the Fâ€“16 HUD velocity scale and indicator can be changed on the UFCP to display GS, TAS, or CAS. a. True b. False: Answer: A
Which of the following statements is true regarding the Fâ€“16 HUD display when the landing gear handle is lowered? a. The TD box is removed with destination point 326 selected. b. The AOA symbol, 2.5Â° pitch/dive line, and VVI are display: Answer: D
Which of the following statements is true concerning the commanded airspeed indication on the HUD? a. With the gear handle up, the commanded airspeed marker indicates the maximum range airspeed at the current altitude as computed by the MDP.: Answer: D
The bearing arrow and radial readout on the Fâ€“16 HUD always display information to the selected VOR station whenever a valid signaled is received. a. True b. False: Answer: B
What would be indicated by the value â€œB+1000â€ in the second row of the digital fuel data block on the HUD? a. The total fuel remaining is 1000 pounds. b. The BINGO fuel setting is 1000 pounds. c. The amount of fuel remaining above BING: Answer: D
Which of following conditions would result in a blank RALT display on the HUD? a. The RALT system is OFF. b. A malfunction of the RALT system. c. The aircraft altitude is out of the RALT limits. d. Any of the above conditions may resu: Answer: D
Which of the following is true about the CDI display on the HUD? a. A maximum of two dots are displayed at any time. b. No dots are displayed when the deviation is less than one-half dot. c. For a deviation greater than two dots, the CDI a: Answer: D
Which of following is true about the visual WARNING, CAUTION and ADVISORY alerts displayed in the HUD message window? a. All alert messages are displayed boxed and flashing on the HUD for 15 seconds and then are removed. b. If more than on: Answer: D
When the declutter function is selected with the DCL key on the UFCP, on which of the following displays will the preselected items be removed from? a. HUD only b. MFD only c. HUD and MFD d. HUD, MFD, and EED: Answer: A
The RA symbol generated by the TCAS on the HUD, displays the vertical zone that the pilot needs to enter to avoid the traffic conflict (i.e., climb/descend so that the FPM is inside the displayed zone). a. True b. False: Answer: B
Which of the following statements is true about the Tâ€“38C warning/caution/advisory system when the MDP fails or is OFF? a. The warning/caution/advisory system would not be affected at all. b. The entire warning/caution/advisory system wo: Answer: D
The visual ALTITUDE, STALL, and GEAR warnings displayed on the HUD/MFD are also accompanied by aural warning tones. a. True b. False: Answer: A
Which of the following statements is true about the visual and aural GEAR warning indications when activated? a. All landing gear warning indications can be removed by pressing the silence button next to the gear handle. b. All landing gear war: Answer: C
A blinking CAUTION appears on the HUD and MFD whenever the MASTER CAUTION light illuminates, and is removed when the MASTER CAUTION light is pressed. a. True b. False: Answer: A
Which of the following EGI advisory messages on the HUD is displayed during a GC alignment on the ground to indicate the EGI is still in the coarse alignment phase, and that the aircraft should not be moved? a. WAIT b. ATT c. DEGRADED: Answer: A
Only the most recent alert is displayed on the HUD/MFD when there is more than one alert activated at a time. a. True b. False: Answer: B
configurations would be correct if you want to operate the UHF radio only? a. Turn battery switch ON, AAP mode switch to UHF B/U position, and UHF backup panel knob to ON. b. Turn battery switch ON, ACP audio amplifier switch to B/U, and UHF ba: Answer: A
With just battery (DC) power (i.e., AC generators and transformer rectifier units are inoperative), electrical components on the non-essential DC bus are not powered, to include both UFCPs. a. True b. False: Answer: A
Which of the following key avionics components would be inoperative with a total MDP failure? a. HUD and UFCP b. MFD c. EED d. All of the above.: Answer: A
Which of the following statements is true when the RPM or oil pressure exceeds the operating limits or the EGT displays an overtemperature? a. a.The MASTER CAUTION light is illuminated and an avionics alert is activated on the HUD/MFD. b.: Answer: B

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