Use LEFT and RIGHT arrow keys to navigate between flashcards;
Use UP and DOWN arrow keys to flip the card;
H to show hint;
A reads text to speech;
58 Cards in this Set
- Front
- Back
The primary FMC (FMC2) is located?
|
Transition section
|
|
A Slip Indicator (Ball) is incorporated into the FDs lower frame (T/F)
|
True
|
|
Control of Radio & Internal comms for hoist, C/c, & gunner is provided by
|
CSC
|
|
When the RCU is on it takes control of the selected MFR, regardless of AMC/FMC status (T/F)
|
True
|
|
Primary subsystem of Avionics Subsystem include each except
|
AFCS
|
|
Only input of a backup instrument to DHD & OSI is the BARALT to the
|
IFF
|
|
Each MFR provides each capability except
|
HF
|
|
Which unit allows Pitot &Co/p to control radio and internal comms
|
OCP
|
|
The ILS provides glide slope, LOC, and MkrBkn (dist to runway) (T/F)
|
True
|
|
The Backup flight instruments consist of the following except
|
Stabilator indicator
|
|
The 3 modes of DALS operation are CONT, HOME, & MAN (T/F)
|
True
|
|
DALS provides aircraft w/ the ability to locate downed Fltcrew equipped w/ a
|
compatible survival radio
|
|
CAUTION— Improper shutdown of the FMP may cause data corruption on the
|
PCMCIAs
|
|
Available range scales in the MAP mode are 1, 2, 4, 8, 16, 32, 64, & 128 MN; determined by
|
doubling the value on the inner ring
|
|
Designation of the PKs is such that no function is greater than ___ levels down in PK hierarchy
|
3
|
|
RADALT data is provided up to ___ ft w/ pitch/roll less than ___ deg
|
5000ft,45degrees
|
|
The 1553B data bus is non-redundant (T/F)
|
False
|
|
FMP software performs the following except
|
Flt data recording
|
|
The FFK allowing the P. / C/p to reposition GEOSIT disp centered on HOOK POSN
|
CTR HOOK
|
|
The UCK is used to set the following values except
|
Hover height
|
|
Which bezel key brings up menus for testing individual Avionics Equipment
|
DIAG
|
|
The Interaction Control Key submitting values and changing the system for processing is
|
ENT
|
|
Data Handling System (DHS) initialization begins with placing the ___ switch(es) to ___.
|
CMPTR PWR, ON
|
|
When the bkup FMC is cont the DHS the ___ advisory will appear
|
BACKUP IN CONTROL
|
|
The PCMCIAs are necessary to boot up the FMC1. (T/F)
|
False
|
|
For correct data xfer the PCMCIAs must be inserted ___.
|
prior to turning the CMPTR PWR switches to ON
|
|
Secondary windows appear at the bottom of the primary window and can be moved to the top ½ of the primary window by depressing the ___
|
MOVE WDO KEY
|
|
PCMCIAs are used to load the following except
|
COMSEC codes
|
|
In the event of a problem w/ a PCMCIA, or when 1 is not installed in the DTS, the ___ light will illume on the CMP
|
CARD
|
|
menus to generate a SAR search pattern are accessed by depressing the ___ FFK
|
FTP
|
|
The flight mgmt computer and Flt mission display subsystem pwr requirements are met when the APU gen is on (T/F)
|
True
|
|
To disp the actual pos coordinates of a symbol the P/C/p must hook-select that symbol then depress the ___ FFK
|
HOOK LTLG
|
|
The N/H/T bezel key ___
|
– is available in the MAP mode only
|
|
The max selectable range scale for a geosit disp is ___ NM
|
– 256 NM (min range 0.25 NM)
|
|
Display area 1 displays one operator action alert (two lines) and up to 6 dedicated lines for ___
|
annunciators: -NAV mode -Armament (not currently used; WOW is disp here) -IFF/Mayday (eg. 4AUD OFF) -Countermeasures (not currently used; EXT PWR ON is disp here) -HOOK/HOIST (eg. Hook open) -Guidance (eg. ENROUTE/ENROUTE
|
|
LOAD advisory light on the CMP indicates that ___.
|
power has been successfully applied
|
|
Hover Position Mark Point & Approach Desired Track –
|
green circle w/ a cyan wedge indicating hover pos relative to the fly-to-point & desired approach angle.
|
|
Horizontal Acceleration Cue
|
– white circle indicating bearing & acceleration in reference to the velocity vector. The outer circle of disp represents 6 ft/s sq
|
|
Velocity Vector
|
green, originates from the aircraft symbol, indicating actual helicopter drift. The inner circle of disp represents 10 kts, the outer circle 20 kts
|
|
Altitude Error Box
|
magenta, indicates deviation from the selected hover height. If error box corners touch inner circle, then error = 0. If error box corners touch outer circle, then helicopter ALT is 40 ft less than selected. If error box shrinks to fit within the inner circle, then hover ALT is higher than selected.
|
|
Available ranges in HVR mode are
|
8 NM & 800 yds
|
|
RADALT
|
= white pointer and scale 0-1000 ft
|
|
AFCC ALT caret
|
magenta, indicates the hover height selected on AFCS CONTROL panel. Appears only when approaching a coupled hover / while in a coupled hover.
|
|
AUTO TEST
|
dial indications & digital indication go to 10010 ft & P.s hear 5 beeps in headsets
|
|
VSI in fpm
|
indicated as a rising/descending cyan-filled area originating from 0 index. No digi readout
-Range of 3,000 fpm w/ increments of 100 fpm from 0-1,000 fpm 500 fpm from 1,000-3,000 fpm |
|
There are 7 thermocouples on the TGT harness in the Np section measuring
|
TGT
|
|
There are 2 Np sensors in the engine exhaust section, identical and interchangeable, serving different functions
|
-Left-hand sensor provides Np signal to FD and Np-governing function
-Right-hand sensor provides signal for TQ computation and Np overspeed protection |
|
Nr sensor mounted on
|
right-hand accessory module
|
|
Engine TQ is measured by the right-hand Np sensor in the
|
engine exhaust section
|
|
Xmission Temp data from
|
Temp sensor in Main Module’s Wet Sump
|
|
Xmission psi from
|
Pressure Sensor downstream of Air/Oil Cooler.
|
|
Engine Oil Psi and Temp sensors for respective cautions
|
located downstream of Engine Oil Filter.
|
|
Ng measured by Engine Alternator on
|
front face of Eng Acc Gearbox
|
|
Bkup BARALT
|
-Kohlsman window set 28.10-31.00 in
-CODE OFF warning flag displayed of loss of 115 VAC pwr -Integrated encoder provide digi output of PA in 100 ft increments to IFF xponder (w/ Mode C selected) for automatic ATL xmission |
|
Bkup AI contains internal gyro powered by DC battery bus via a built-in inverter
|
-yellow OFF flag indicate loss of 28 VDC pwr supplied by batt bus
|
|
When in HVR mode the FDs provide the info necessary to maintain the a/c ___.
|
at a fixed pos relative to a point on the earth
|
|
When an a/c component supplying data driving a symbol fails the display object will be decluttered and replaced w/ a series of ___.
|
– red “X”s
|
|
VSI indicated range of +/-___ fpm
|
3,000
|