In the early days of flight, when air traffic was light and slower moving, pilots were
equipped with all they needed for effective collision avoidance–a sharp pair of eyes to scan
the horizon.
Even today, visual contact is still the surest means of identifying intruder aircraft. But with
more traffic in closer proximity and at higher speeds, today’s pilots need all the help they
can get.
For large commercial airliners, this need led to the development of
TCAS II
(Traffic Alert
and Collision Avoidance System II); but that technology has proved to be too expensive
and complex for most regional airlines, business, and general aviation aircraft.
SKYWATCH
BFGoodrich Avionics Systems, Inc. recognized the need for a viable alternative to
and developed their
business and general aviation aircraft. That’s why
SKY497
The
SKY497
making it practical for small aircraft. In addition, the
comes with the
if you already own a
™
TCAS I
; but even
Traffic Advisory System.
provides most of the capabilities of
STORMSCOPE
WX-1000
®
model
WX-1000
display (part number 78-8060-5900-8). The
TCAS I
has proved to be too expensive for small
BFG
developed the
TCAS I
, but at a significantly lower cost
SKY497
SKYWATCH
can share the display that
so there’s no need to buy another display
SKY497
TCAS II
™
model
can also
display its traffic information on a growing number of multifunction displays from
companies such as Avidyne, Eventide, and Garmin. You can even display
traffic information on a compatible weather radar indicator via the
Computer, model
Proven Experience
RGC250
.
SKYWATCH
BFG
Radar Graphics
BFGoodrich Avionics Systems, Inc. has been involved in the development of collision
warning programs since the early 1980’s. In 1985,
enhanced collision warning system for the U.S. Navy which awarded
BFG
began development of an
BFG
a contract for
systems to be installed in T-34C training aircraft.
Based largely on the success of the Navy project,
specifications for
contract represented another first for
to be
TSO’d
I
TCAS I
under an
ARINC
contract with the
BFG’s TCAS I
, first to receive a full, unrestricted
BFG
was selected to validate the
FAA
. The completion of this
unit, the
STC
TCAS791
; it was the first
, first to fly, and first to be delivered.
TCAS
The BFGoodrich tradition of aerospace innovation dates back to the earliest days of
powered flight when
BFG
supplied tires for the Glenn Curtiss pusher. Since then,
BFG
has
developed a wide range of aerospace products and services including flight instrumentation and avionics.
ASKY497 Pilot’s Guide
Page 3
$12.00 U.S.
Pilot’s Guide
for the
Traffic Advisory System
Model SKY497
Methods and apparatus disclosed and described herein have been developed solely on company funds of
BFGoodrich Avionics Systems, Inc. No government or other contractual support or relationship whatsoever has
existed which in any way affects or mitigates proprietary rights of BFGoodrich Avionics Systems, Inc. in these
developments. Methods and apparatus disclosed herein may be subject to U.S. Patents existing or applied for.
BFGoodrich Avionics Systems, Inc. reserves the right to add, improve, modify, or withdraw functions, design
modifications, or products at any time without notice.
from BFGoodrich Avionics Systems, Inc. is an airborne
TAS
). It monitors the airspace around your aircraft and advises the
flight crew where to look for transponder-equipped aircraft that may pose a collision threat.
The
SKY497
is intended for use by corporate and general aviation aircraft. Figure 1-1 shows
the major components of the
The
SKY497
displays traffic information on a
SKY497
.
BFG WX-1000/SKY497
display and generates
aural announcementson the cockpit audio system. The display can be dedicated to the
SKY497
or shared with a
using a remote
SKYWATCH/STORMSCOPE
STORMSCOPE
Traffic information on the
CRT
®
Weather Mapping System (model
WX-1000
)
mode switch.
display consists of green symbols and text. The traffic
information generally includes the relative range, bearing, and altitude of intruder aircraft.
TRCDisplay
Figure 1-1. SKY497 Major Components
Transmitter Receiver Computer (TRC)
The
TRC
is the primary unit of the
SKY497
. It contains the circuitry necessary to convert
Directional Antenna
inputs from the directional antenna and from other aircraft systems into an on-screen
representation of intruding aircraft, and if necessary, aural traffic advisories. The
track up to 30 intruder aircraft simultaneously, but to reduce clutter, the
displays the eight most threatening intruders being tracked. The
Test Equipment (
Directional Antenna
BITE
) which detects faults and verifies proper operation.
TRC
also contains Built-In
TRC
SKY497
can
only
The directional antenna transmits omnidirectional mode C interrogations and receives
directional replies from other transponder-equipped aircraft in the vicinity.
Pilot’s Guide1-1
SKY497 Pilot’s Guide
Page 8
System Description
SKY497
Display
The display is a self-contained,
Cathode Ray Tube (
CRT
3-ATI
-sized unit with a high resolution, green monochrome
) display. The bezel contains four momentary contact push-button
switches and an on/off/brightness knob. The display provides control and display
functions for the
SKY497
and for a
WX-1000 STORMSCOPE
(if installed).
The display does not display traffic and storm information simultaneously. The position of
a remote
plays traffic or storm information; however, if you’re in
SKY497
temporarily switch to
SKYWATCH
SKYWATCH/STORMSCOPE
mode switch determines whether the display dis-
STORMSCOPE
mode and the
detects traffic that may pose an immediate threat to your aircraft, the display will
SKYWATCH
screen. Figure 1-3 shows the display with a typical
mode. Figure 1-2 shows the display with a typical
STORMSCOPE
screen.
BRT
+05
-13
+01
+10
NRM
+25
nm
6
Figure 1-2.Display with Typical
Screen
OFF
SKYWATCH
MENU
Figure 1-3.Display with Typical STORMSCOPE
Screen (Optional)
300$
25
CLEAR
Interaction of Major Components
Figure 1-4 shows how the major components of the
SKY497
connect to each other and to
other aircraft systems.
Notes on Figure 1-4:
1.The optional radio altitude input affects the
SKY497
audio inhibit
feature, the ground target filtering feature, and the sensitivity levels
feature. (See chapter 3 for details.)
2.A flight data computer or other Arinc 429 output device may replace
individual analog sensors for supplying barometric altitude & heading.
3.The
SKY497
will work without a heading input, but it will experience
degraded performance during high-rate-of-turn maneuvers.
4.The
SKY497
may be installed on aircraft with fixed landing gear. The
optional landing gear position input affects the sensitivity levels feature.
(See chapter 3 for details.)
100nm
120$
OFF
BRT
1-2 Pilot’s Guide
Page 9
SKY497
System Description
Intruder Aircraft
Aircraft
Audio
System
Diagnostic
Equipment
(Optional)
Data
Recorder
(Optional)
Third-Party
MFD or BFG
RGC250/
Radar
Indicator
(Optional)
7
SKY497
Display
Transponder
Transponder
Aural TA's
Diagnostic Commands
and Status (RS-232)
Flight Data (RS-422)
SKYWATCH
Display
ARINC429
SKYWATCH
Control
Display Power
SKYWATCH
STORMSCOPE
STORMSCOPE
Display
SKYWATCH
Control
or
8
8
or
6
6
Replies
Replies
Transponder
Interrogations
Transponder
Interrogations
TRC
Directional
Antenna
Arinc 429
Radio Altitude
Barometric Altitude
2,3
Heading
TX/RX Inhibit
Landing Gear Position
Audio Inhibit
Weight On Wheels
14 or 28 V dc
SKYWATCH/
STORMSCOPE
Mode Selection
Display Power/
TRC On/Off Control
STORMSCOPE
STORMSCOPE
TRC On/Off Control
When WX-1000 is
Powered Down or
Removed
On/Off Control
1
5
Display
Control
2
4
Arinc 429 Radio
Altimeter or Flight
Data Computer
(Optional)
Encoding Altimeter
Aircraft Compass
System
Aircraft
Suppression Bus
Landing Gear
Switch (Optional)
GPWS (Optional)
Squat Switch
(Optional)
Aircraft Power
SKYWATCH/
STORMSCOPE
Mode Switch
WX-1000
STORMSCOPE
Processor
WX-1000
On/Off Control
WX-1000
Maintenance
Switch
Option
STORMSCOPE
Figure 1-4. SKY497 Simplified Functional Diagram
5. This audio inhibit input is only required if you have a Ground
Proximity Warning System installed.
6. The position of the
mines whether the display displays
SKYWATCH/STORMSCOPE
SKYWATCH
mode switch deter-
or
STORMSCOPE
information. The switch also determines whether the buttons on the
display control the
7. The optional
addition to the standard
8. The flight data
are not required for normal
Pilot’s Guide1-3
MFD
or
SKYWATCH
RGC250
or
/radar indicator can be in place of, or in
WX-1000/SKY497
RS-422
output and the diagnostic
SKY497
STORMSCOPE
display.
operation.
system.
RS-232
input/output
Page 10
System Description
Functional Description
The
SKY497
is an active system that operates as an aircraft-to-aircraft interrogation device.
The
SKY497
interrogates transponders in the surrounding airspace similar to the way that
ground-based radar interrogates aircraft transponders. When the
SKY497
SKY497
receives replies
to its interrogations, it computes the responding aircraft’s range, bearing, relative altitude,
and closure rate. The
SKY497
then plots the traffic location and predicts collision threats.
Figure 1-5 shows the
SKY497
altitude display modes (look up, look down, and normal).
The figure also shows the traffic zones around your aircraft and the traffic symbols that
appear on the display when intruding aircraft enter one of those zones.
A solid circle is the visual part of the Traffic Advisory (TA) that the
SKY497
generates when
it predicts that an intruder aircraft may pose a collision threat. The aural part of the TA,
“traffic, traffic,”is annunciated over a cockpit speaker or headset. An open diamond
represents traffic that does not pose an immediate collision threat.
The
SKY497
uses either sensitivity level A (
when to display a TA. In general,
SLB
SLA
) or sensitivity level B (
SLB
) to determine
is used during the in-flight phase and
SLA
is used
during takeoff and landing. Sensitivity levels and other factors affecting the display of traffic
symbols are discussed in detail in chapter 3. Look up, look down, and normal altitude
display modes are described in chapter 2.
Features
• Tracks up to 30 intruder aircraft (displays the 8 most threatening)
• Tracks intruder aircraft approaching at closure rates up to 900 knots
• Fraction of the cost of a
TCAS I
or
II
• Does not require a mode S transponder
• Two horizontal display ranges (6 nmi and 2 nmi)
• Three altitude display modes: normal (±2,700 ft), look up (–2,700 ft to +9,000 ft), and
look down (–9,000 ft to +2,700 ft)
• Generates visual and aural advisories of aircraft that may pose a collision threat
• Automatic and pilot-initiated self test functions
• High-resolution, green monochrome,
CRT
display
• Can transmit interrogations from the ground as well as from the air
• Can share a display with the
• Can display its traffic information on a compatible weather radar indicator (via a
) or on a third-party multifunction display in addition to, or in place of the
RGC250
BFG
display.
• Automatically switches back to the
STORMSCOPE WX-1000
SKYWATCH
screen from the
BFG
STORMSCOPE
screen when a TA is issued
• Uses only one antenna
• Display fits in a standard
3-ATI
cutout in the cockpit panel
1-4Pilot’s Guide
Page 11
SKY497
System Description
Look Up (ABV)
Normal (NRM)
Look Down (BLW)
6 nmi
6 nmi
0.55 nmi
0.2 nmi
S
e
n
s
i
t
i
A
l
e
v
e
v
L
ity
*
*
*
+9000 ft
Intruder Aircraft
+2700 ft
+800 ft
+600 ft
0 ft
–600 ft
–800 ft
–2700 ft
Not To Scale
–9000 ft
*15 seconds for non-altitude reporting intruder aircraft
**20 seconds for non-altitude reporting intruder aircraft
Refer to chapter 3 for details. CPA means Closest Point of Approach.
Figure 1-5. Altitude Display Modes and Traffic Zones
Pilot’s Guide 1-5
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