-
Detects radials and displays it on the EHSI
VOR receiver
-
VOR stations frequency range
108.0-117.95 MHz
-
VORTAC stations transmit in a _____ scheme
Frequency pairing
-
The VOR signal is received through two combo _____ antennas, mounted where?
- NAV/GS/ILS
- Each side of vert stab
-
VOR signals are passed to and processed by the _____, located where?
- VHF NAV receiver
- Right avionics bay
-
VOR stations are tuned through the _____
RMU
-
Localizer frequency
108.10-111.95 MHz
-
Glideslope frequency
329.15-335.00 MHz
-
Marker beacon frequency
75 MHz
-
Processed through the same antennas on the sides of the vertical fin and by the same receiver in the right avionics bay
Localizer and Glideslope
-
Located on the bottom of the fuselage just in front of the ventral fin
Marker beacon antenna
-
Processed by the navigation receiver in the right avionics bay
Marker beacon
-
The ILS and glideslope signals are received and processed through the same antennas and receiver as the _____ system
VOR
-
_____ must first be selected as the nav data source to properly display localizer on the EHSI
VOR
-
With the localizer frequency active, the _____ replaces the VOR data in the EHSI upper left corner
Localizer distance and TTG
-
What is added to the EADI when LOC is selected on the EHSI
- Glideslope scale and pointer (right)
- Localizer scale and lateral position indicator (bottom)
- Marker beacon annunciator (lower right)
-
DME UHF frequency range
962-1213
-
Error b/t DME display and horizontal distance to the station _____ as the airplane gets closer
Increases
-
DME error is more pronounced with _____ altitude aircraft
Higher
-
DME UHF range
Up to 199 nm depending on altitude
-
DME antenna location
Bottom of aircraft in front of marker beacon antenna
-
DME receiver location
Right avionics bay
-
DME info is provided automatically and is displayed on the EHSI when? (Info included on slide labeled 1)
A nav facility has DME capability
-
1
- Distance (slant range)
- AC GS
- TTG
-
Used when flying an approach to one nav facility that requires DME info from another facility
DMEH
-
DMEH process
- Press DMEH
- Press right mode select button
- Set new frequency in primary nav position
-
When DMEH is activated, the frequency in _____ of the held facility will replace the ground speed readout below the distance field
White
-
TTG when DMEH is active
Blank
-
When DMEH is active, DME HOLD is displayed on the _______
RMU
-
Used to overcome radio wave interruption
Transponder
-
Airborne portion of the ATC radar beacon system
Transponder
-
Transponder AKA
Secondary radar
-
Any aircraft within line-of-sight and equipped with a transponder set to the same code responds _____ by sending back a coded signal
Automatically
-
ATC uses Mode _____ and _____ separate codes for traffic control
-
Unique 4 digit code assigned to each aircraft
SQUAWK
-
Adds automatic altitude reporting to the basic mode "A" ID feature
Mode C
-
Altitude info is provided by the _____ via the _____ for altitude encoding and transmission by the transponder
-
Pilot's cue to switch the transponder to Mode C operation through the RMU
SQUAWK ALTITUDE
-
Transponder location
Right avionics bay
-
Transponder antenna location
Bottom of fuselage just in front of the wing
-
Transponder is controlled through the _____
RMU
-
Transponder code knobs operate which digits?
- Outer - first 2
- Inner - third and fourth
-
How to SQUAWK ALTITUDE
Press mode select switch on right side of field to change from ON to ALT
-
IDT transmits for how long?
20 seconds
-
Transponder will not ident while in the _____ mode
STBY
-
Transponder circuit breaker
XPDR
-
Evaluates collision avoidance data and provides traffic info to the visual and audio displays
NACWS computer
-
NACWS computer location
Left avionics bay
-
NACWS antennas - number and location
- 2
- Top of cowling in front of windscreen; Bottom of fuselage near wing trailing edge
-
NACWS is enabled when aircraft is powered and the switch is
Blank
-
Number of aural tones during NACWS self-test
6
-
NACWS INOP will extinguish and system will begin to operate when?
Airborne and WOW
-
How to perform manual NACWS self-test
Simultaneously press range button while squeezing trigger
-
NACWS activation (manual)
Pull trigger to second detent
-
NACWS info is displayed for how long after trigger pull?
7 seconds
-
The NACWS system normally operates in the _____ mode
Passive
-
NACWS system uses known location of a ground secondary surveillance radar station along with aircraft gps position and AHRS heading info to triangulate aircraft position of up to _____ aircraft
-
The T6 cannot ID aircraft that are not equipped with a _____
Transponder
-
NACWS shows location and altitude of up to _____ of the most threatening aircraft
8
-
NACWS range includes traffic advisories down to the _____ NM display
3
-
NACWS upward pointing triangle
Traffic b/t 400-900 ft above present altitude
-
NACWS + or - sign
Vertical separation
-
NACWS rectangle
Traffic within 300 ft of aircraft altitude
-
NACWS flashing and filled rectangle
Traffic advisory
-
NACWS downward pointing triangle
Traffic b/t 400-900 ft below present altitude
-
NACWS upward or downward triangle with no altitude tag
1000-2700 ft off altitude
-
NACWS white circle
Traffic unknown altitude
-
NACWS any yellow filled and flashing symbol
Traffic considered a collision danger
-
NACWS - any white, open, non-flashing symbol
No threat
-
NACWS system interrogates other aircraft transponders w/in a 6 NM radius and calculates their range ad relative altitude
Active mode
-
NACWS active mode transponder radius
6 NM
-
NACWS active mode - number of threatening aircraft displayed
6
-
Only traffic displayed in active mode
Traffic NACWS considers possible conflicts
-
-
-
NACWS enroute mode protection zone
+/- 500 ft vertically w/a 1 NM radius
-
Aircraft detected within _____ seconds of protection zone will cause ______ flashing symbol and _____ slow aural tones
-
When is NACWS in landing mode?
When range is set to 1.5 NM
-
Landing mode protection zone
+/- 500 ft vertically with a radius of .1 NM
-
NACWS landing mode protection zone - aircraft detected within _____ seconds
10
-
A Normal/Below/Above pushbutton selector switch is located on the _____ and used to select the _____
- Control stick
- Airspace volume limits
-
TAS - Normal mode, traffic is displayed b/t _____ ft
2700 above and below
-
TAS above mode
- Used during climb
- 8700 ft above
- 2700 ft below
-
TAS below mode
- Used on descents
- 8700 ft below
- 2700 ft above
-
-
TAS green range ring represent a ____ mile radius
2
-
Greater range = _____ range ring
Smaller
-
Range rings disappear at _____ NM
40
-
TAS is not a _____ function, and must be independently selected from each cockpit
Tandem
-
TAS receives altitude and speed data from
ADC
-
TAS antennas (# and location)
- 2
- upper - top of engine cowling
- lower - bottom of fuselage ahead of speed brake
-
TAS tracks w/in a _____ NM radius and within _____ ft above or below the aircraft
-
TAS warnings
- Proximate traffic
- Traffic advisory
-
Intruders that do not qualify as either proximate or TA
Other traffic
-
TAS filled white diamond
Aircraft within +/- 1200 feet relative altitude and 5 NM range
-
Displayed to indicate whether traffic is climbing or descending relative to your aircraft
Trend arrow
-
TAS filled yellow circle
Intruding aircraft considered potentially hazardous
-
TAS displays TA when the time to closest point of intruder aircraft approach is _____ seconds
15-30
-
TAS audio messages are inhibited when
Landing gear is extended
-
TAS is in sensitivity level "A" when
Landing gear is extended
-
TAS level "A" issues TA when...
- Vertical separation of less than 600 ft will occur in 20 seconds; Closing rate of intruder is maintained
- Vertical separation less than 600 ft and horizontal sep less than 0.2 NM
- Horizontal sep from non-altitude reporting intruder is within 15 seconds or 0.2 NM
-
TAS is in sensitivity level B when...
Landing gear is retracted (up)
-
TAS open white diamond
- Intruder's relative altitude is greater than 1,200' relative altitude OR
- Distance is beyond 5 NM
-
TAS - half of the traffic symbol
Aircraft beyond selected display range
-
TAS test indications - Yellow filled circle will appear at the ____ o'clock position at ____ NM range, _____ ft below and climbing
-
TAS test indications - solid white diamond appears at the ____ o'clock position at ____ NM, ____ ft below, descending
-
TAS test indications - Open white diamond will appear at the ____ o'clock position, _____ NM range, and ____ ft above and in level flight
-
TAS yellow filled circle
TA
-
TAS solid white diamond
Proximity traffic
-
TAS is displayed on the
VSI
-
GPS antenna location
Top front edge of vert stab
-
For either GPS to be used, what must be on and functioning properly?
Front cockpit unit
-
GPS data is displayed on the
-
Info on the left side of the GPS (always the same)
-
If TEST FAIL replaces ANNUN ON display, _____
Recycle power to the unit
-
GPS date and time are stored in _____ memory
Battery-backed
-
How to accept self test results
Turn right outer knob to put cursor over APPROVE?, then press enter
-
Default page for the left side of the display
NAV 2
-
On initial activation, data on the NAV 2 page may be replaced with dashes until _____
Satellite signals are required
-
When the cursor is on, a ____ replaces the page name in the ____ corner screen segments
-
Used to select the page types for the left and right sides of the screen respectively
Outer knobs
-
First step in making any change (GPS)
Ensure you are on the correct GPS page
-
Alerts you that there is a situation which may require your attention (GPS)
Flashing MSG
-
Used to create a user-defined waypoint at your current position
SAVE button
-
Allows you to define the course to the active waypoint
OBS
-
GPS capability used most
Flight plan
-
GPS can store up to _____ flight plans in memory
25
-
Each flight plan may contain up to _____ waypoints
30
-
Active flight plan is always labeled _____
FPL 0
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