L 3 Communications Avionics Systems TRC497 Operators Guide

Page 1
$12.00 U.S.
Pilot’s Guide
for the
Traffic Advisory System
Model SKY497
Page 2

EYES THAT NEVER BLINK

Early Traffic Advisory Systems
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.
A SKY497 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.
© Copyright 1997, 2000
BFGoodrich Avionics Systems, Inc.
SKYWATCH
,
EYES THAT NEVER BLINK
, and
STORMSCOPE
®
are trademarks of
BFGoodrich Avionics Systems, Inc.
Designed and manufactured in the United States of America by
Page 4

Safety Summary

These warnings and cautions appear later in this guide and are repeated here for emphasis:
(page 2-4)
To avoid power surges that could damage the optional
WX-1000
, start your engines before turning on the
(page 2-8)
SKY497
and the
SKY497
.
If the
SKY497
is in
SKYWATCH
matically switch into storms or
WATCH
STORMSCOPE
/
STORMSCOPE
thunderstorms or
The
SKY497
relies on information obtained from transponders in
nearby aircraft. The
STORMSCOPE
STORMSCOPE
SKY497
are not equipped with an operating
The
SKY497
does not track intruder aircraft approaching at a
mode, the display will not auto-
mode to display thunder-
errors: You must use the remote
SKY-
mode switch to periodically check for
errors.
(page 2-8)
does not detect or track aircraft which
ATCRBS
transponder.
(page 2-8)
closure rate greater than 900 knots.
(page 2-8)
Some traffic within the chosen display range may not be displayed due to traffic prioritizing or antenna shielding.
(page 2-8)
Optimum
SKY497
performance is realized when intruder aircraft are reporting their altitude (via a mode C or other altitude reporting transponder).
(page 2-9)
Do not attempt evasive maneuvers based solely on traffic informa­tion shown on the
SKY497
display. Information on the display is provided to the flight crew as an aid in visually acquiring traffic; it is not a replacement for
ii SKY497 Pilot’s Guide
ATC
and See & Avoid techniques.
Page 5

Table of Contents

Page
List of Illustrations............................................................................iv
List of Tables....................................................................................iv
Chapter 1 System Description.........................................................1-1
General Description.............................................................................................1-1
Transmitter Receiver Computer (TRC)..................................................................1-1
Directional Antenna.............................................................................................1-1
Display.................................................................................................................1-2
Interaction of Major Components.........................................................................1-2
Functional Description.........................................................................................1-4
Features...............................................................................................................1-4
Chapter 2 Operating Instructions....................................................2-1
Controls & Indicators..........................................................................................2-1
Turn On the SKY497...........................................................................................2-4
Run the Operator-Initiated Self Test......................................................................2-4
Switch Between Standby and Normal Operating Mode..........................................2-6
Change the Display Range....................................................................................2-6
Change the Altitude Display Mode.......................................................................2-7
Switch Between SKYWATCH™ and STORMSCOPE® Modes (Optional)............2-8
Observe the Display..............................................................................................2-8
Respond to Traffic Advisories...............................................................................2-9
Turn Off the SKY497 and the Optional WX-1000................................................2-9
Failure Response...................................................................................................2-9
Operate the Optional WX-1000 When the SKY497 is Removed.........................2-10
Operate the SKY497 When the Optional WX-1000 is Removed.........................2-10
Chapter 3 Principles of Operation....................................................3-1
Introduction........................................................................................................3-1
Sensitivity Levels..................................................................................................3-1
Sensitivity Level A............................................................................................3-2
Sensitivity Level B.............................................................................................3-2
Audio Inhibit, SKY497.........................................................................................3-2
Audio Inhibit, GPWS...........................................................................................3-4
TA Symbol Duration............................................................................................3-4
Ground Target Filtering........................................................................................3-4
Chapter 4 Display Interpretation.....................................................4-1
Introduction........................................................................................................4-1
Chapter 5 Specifications.................................................................5-1
Chapter 6 Warranty Information.....................................................6-1
Introduction........................................................................................................6-1
Warranty Statement..............................................................................................6-1
Related Policies and Procedures.............................................................................6-2
SKY497 Pilot’s Guide iii
Page 6

List of Illustrations

Figure Title Page
1-1 SKY497 Major Components.....................................................................1-1
1-2 Display with Typical SKYWATCH Screen.................................................1-2
1-3 Display with Typical STORMSCOPE Screen (Optional).............................1-2
1-4 SKY497 Simplified Functional Diagram....................................................1-3
1-5 Altitude Display Modes and Traffic Zones..................................................1-5
2-1 SKY497 Controls and Indicators...............................................................2-1
2-2 BFGoodrich Screen...................................................................................2-5
2-3 SKY497 Standby Screen............................................................................2-5
2-4 In-Flight Traffic Screen..............................................................................2-5
2-5 SKY497 Failed Screen...............................................................................2-5
2-6 Operator-Initiated Test Screen...................................................................2-5
2-7 Traffic Screen Set on 6 nmi Range.............................................................2-6
2-8 Traffic Screen Set on 2 nmi Range.............................................................2-6
2-9 Altitude Display Modes.............................................................................2-7
3-1 TA Zones If Your Aircraft Has a Radio Altimeter........................................3-3
3-2 TA Zones If Your Aircraft Has No Radio Altimeter, But Does Have
Retractable Landing Gear..........................................................................3-3
3-3 TA Zones If Your Aircraft Has Fixed Landing Gear and No Radio Altimeter3-4
4-1 Traffic Advisory and Other Traffic.............................................................4-1
4-2 Out-of-Range Traffic Advisory....................................................................4-1
4-3 Non-Altitude-Reporting Traffic..................................................................4-2
4-4 SKY497 Standby Screen............................................................................4-2
4-5 SKY497 Failed Screen...............................................................................4-2

List of Tables

Table Title Page
2-1 SKY497 Controls and Indicators...............................................................2-1
3-1 Ten Situations in Which a Traffic Advisory Will Occur..............................3-1
5-1 Transmitter Receiver Computer (TRC497) Specifications...........................5-1
5-2 WX-1000/SKY497 Display Specifications.................................................5-2
5-3 NY164 Directional Antenna Specifications................................................5-2
iv SKY497 Pilot’s Guide
Page 7
SKY497
System Description
Chapter 1
System Description

General Description

The
SKYWATCH
Traffic Advisory System (
model
SKY497
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 announcements on 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.
Pilots Guide 1-1
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 Guide 1-3
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
1-4 Pilots 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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