Stormscope®

Transcription

Stormscope®
Stormscope
Series II
®
Weather Mapping Systems
WX-500
Installation
Manual
This manual contains installation instructions and
recommended flightline maintenance information for the
WX-500 Stormscope®. This information is supplemented
and kept current by revisions, Service Memos and Service
Bulletins.
009-11500-001 (Rev. E)
L-3 Communications Avionics Systems, Inc.
nd
5353 52 Street, S.E.
Grand Rapids, MI USA 49512
23 September 2003
ABOUT THIS MANUAL
Chapter 1 – General Information
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Chapter 2 – Installation
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Chapter 3 – Installation Checkout
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Chapter 4 – Maintenance
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Appendix A – Signal and Cable Characteristics
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Appendix B – Environmental Qualification Forms
Appendix C – Display Interface
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Trademarks
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A
Rev. E
WX-500
Installation Manual
LIST OF EFFECTIVE PAGES
Dates of original and changed pages are:
Original (Rev. A).............................. 18 July 1997
Revison (B) ................................... 10 June 1999
Revison (C) .............................. 20 October 2000
Revision (D) ..........................09 November 2001
Revision (E)..........................23 September 2003
Total number of pages in this publication consists of the following:
Title Page
A Page
i thru vi
1-1 thru 1-10
2-1 thru 2-22
3-1 thru 3-6
4-1 thru 4-14
A-1 thru A-6
B-1 thru B-4
C-1 thru C-2
REVISION E HIGHLIGHTS
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Rev. E
WX-500
Installation Manual
FOREWORD
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L-3 Communications Avionics Systems, Inc.
Attn: Field Service Engineering
5353 52nd Street, S.E.
Grand Rapids, MI USA 49512
Tel. (800) 453-0288 or (616) 949-6600
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L-3 Communications Avionics Systems, Inc.
Attn: Technical Publications
5353 52nd Street, S.E.
Grand Rapids, MI USA 49512
ii
Rev. E
WX-500
Installation Manual
TABLE OF CONTENTS
3DUDJUDSK
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Chapter 1
GENERAL INFORMATION
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INSTALLATION
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iii
Rev. E
WX-500
Installation Manual
TABLE OF CONTENTS
3DUDJUDSK
3DJH
Chapter 3
INSTALLATION CHECKOUT
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MAINTENANCE
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7528%/(6+227,1*(/(&75,&$/12,6( ',6326,7,212))$,/(',7(06 Appendix A
WX-500 INTERFACE SIGNAL & CABLE CHARACTERISTICS
Appendix B
ENVIRONMENTAL QUALIFICATION FORMS
Appendix C
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iv
Rev. E
WX-500
Installation Manual
LIST OF ILLUSTRATIONS
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Rev. E
WX-500
Installation Manual
LIST OF TABLES
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vi
Rev. E
WX-500
Installation Manual
CHAPTER 1
GENERAL INFORMATION
1.1 INTRODUCTION
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NOTE
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Table 1-1. WX-500 Installation Kit P/N 817-11500-001
QUANTITY
PART NUMBER
DESCRIPTION
1
1
1
1
1
78-8060-5979-2
78-8060-5977-6
800-11592-001
805-11590-001
817-11501-001
Antenna Doubler Plate
Antenna Gasket
End Panel
Mounting Tray
Hardware Package (see table 1-2)
Table 1-2. Hardware Package P/N 817-11501-001
QUANTITY
PART NUMBER
DESCRIPTION
2
4
4
2
2
6
1
2
6
2
1
1
1
2
1
2
3
50
101-10091-001
101-10098-001
101-10131-001
18-4712-8275-8
26-1004-1394-2
26-1004-9152-6
26-1004-9316-7
26-1004-9826-5
26-1006-2424-1
26-1010-0057-3
606-10009-001
606-10010-001
614A0022
M24308/2-283F
78-8060-5733-3
MS51957-38
MS51958-61
M39029/63-368
6
101A0003-12
TERMINAL LOCKING BRASS
STOP NUT ELASTIC 10-32 S.S.
SPACER RND FF .375 X .375 ALUM
SCREW 8-32 X 1/2 MACH PAN PHIL SST
WASHER .2 ID X .325 OD S.S.
SCREW 10-32 X 1 1/2 PPH S.S.
STOP NUT ELASTIC 4-40 S.S.
NUT HEX 8-32 NYLON LOCKING SS
STANDOFF HEX 4-40 3/16 X 1/2
SCREW 10-32 X 3/8 TRUS PH S.S.
CLAMP CABLE 3/8"
CLAMP CABLE 7/16"
CONNECTOR 9 PIN FEMALE SUB-D W/CRIMP PINS
CONNECTOR SHELL 25 POSN D-SUB RECEPT
LABEL CIRCUIT BREAKER
SCREW P P 6-32 X 2 SS MS51957-38
SCREW P P 10-32 X .375 SS MS51958-61
CONNECTOR CONTACT D-SUB SOCKET 20-24 AWG
CRIMP
WASHER SPLIT RING #4 ss
1-1
Rev. E
WX-500
Installation Manual
1.2 FUNCTIONAL DESCRIPTION
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NOTICE
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Figure 1-1. Functional Diagram
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1.3 PHYSICAL DESCRIPTION
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1.3.1 Processor P/N 805-11500-001
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1-2
Rev. E
WX-500
Installation Manual
Figure 1-2. Processor Unit (P/N 805-11500-001)
1-3
Rev. E
WX-500
Installation Manual
1.3.2 Antenna P/N 805-10930-001 (White) or P/N 805-10930-002 (Black)
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Figure 1-3. NY-163 Antenna (P/N 805-10930-001)
Figure 1-4. Antenna Doubler Plate (P/N 78-8060-5979-2)
1-4
Rev. E
WX-500
Installation Manual
Figure 1-5. Antenna Cables
1-5
Rev. E
WX-500
Installation Manual
1.4 SPECIFICATIONS
SIZE:
Processor (including mounting tray and pull handle)
5.6 inches (14.22 centimeters) high
2.2 inches (5.59 centimeters) wide
12.0 inches (30.48 centimeters) deep
Antenna
1.00 inches (2.54 centimeters) high
3.45 inches (8.76 centimeters) wide
6.85 inches (17.40 centimeters) deep
WEIGHT:
Processor (including mounting tray)
2.5 lb (1.13 kg)
Antenna (without doubler)
0.84 lb (0.38 kg)
TEMPERATURE:
Processor
-55 to +70 degrees Celsius (-67 to +158 degrees Fahrenheit)
Antenna
-55 to +70 degrees Celsius (-67 to +158 degrees Fahrenheit)
ALTITUDE:
Processor
55,000 feet (Maximum)
Antenna
55,000 feet (Maximum)
RANGE:
200nmi
TSO COMPLIANCE:
Processor
TSO-C110a
Antenna
TSO-C110a, JTSO-C110a
RTCA COMPLIANCE:
Processor Environmental
DO-160C Category (For further details refer to Appendix B - Environmental Qualification Form.)
Processor Software
DO-178B Level D
Antenna
DO-160C Category (For further details refer to Appendix B - Environmental Qualification Form.)
POWER REQUIREMENTS:
Input voltage: 11 to 32 VDC
Current:
0.82 A (Maximum) @ 12 VDC
0.38 A (Maximum) @ 28 VDC
1-6
Rev. E
WX-500
Installation Manual
1.5 MODIFICATIONS & SOFTWARE REVISIONS
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DUHLGHQWLILHGE\DQHQWU\RQWKH61DQG,'WDJ7KH:;V\VWHP6<6VRIWZDUHYHUVLRQLVLGHQWLILHG
LHWX-500 SOFTWARE VER x.xx 016-11502-001RQDODEHOSRVLWLRQHGRQWKHVLGHRIWKHXQLW
Table 1-3. WX-500 Hardware Modifications
MOD
COMPLIANCE
DESCRIPTION
A
Optional
Prevent the possibility of traces shorting together by adding insulating washers between the
analog PCB assembly and the four mounting standoffs. Field units need this modification
only if the WX-500 has been blowing fuses or is causing the Stormscope circuit breaker to
trip. (Refer so Service Bulletin #85.) New production units incorporate this MOD.
B
As required.
Provides additional protection against damage due to an excessive overvoltage condition.
This condition has only been observed with units installed on aircraft with a 28 V power bus
that allows spikes exceeding 50 VDC. Field units need this modification only if the WX-500
has been damaged due to excessive over voltage. (Refer to Service Bulletin #90.) New
production units incorporate this MOD.
C
Optional
A production change that adds additional diode isolation to the heading flag circuitry on the
digital PCB. Refer to Service Bulletin #100.
D
Optional
A productions change to improve the electrical bond between the WX-500 and airframe
ground. Refer to Service Bulletin #119.
E
Optional
A production change to add a surge-voltage transient suppressor across the power input
pins on the analog PCB assembly. Refer to Service Bulletin #120.
Table 1-4. WX-500 Software Revisions
VERSION
SYS
Main
Main
Boot
DSP
COMPLIANCE
1.01
1.01
1.01
1.01
----------
Original production release.
1.02
1.02
1.01
1.01
Optional
1.03
1.03
1.01
1.02
Optional
Ensures strikes in Noise Monitor mode are adjusted to correct
(current) heading value.
Reduced processing of strikes beyond 200 nm and increased
accuracy of strike rate calculations.
DESCRIPTION (MAJOR ENHANCEMENTS)
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ZLWKLQWKH:;VHQVRU0DLQ0DLQ%RRWDQG'63VRIWZDUHYHUVLRQVFDQEHYHULILHGE\HQWHULQJ7HVW
0RGHDQGVHOHFWLQJWKH6\VWHP'DWDRSWLRQUHIHUWRSDUDJUDSK
Table 1-5. NY-163 Hardware Modifications
MOD
COMPLIANCE
DESCRIPTION
A
Optional
Indicates that antenna case has passed new testing procedures to verify that the
conductive paint is working properly.
B
Optional
Improves L-Band rejection. Implemented in new production antennas only. Field units
cannot be modified.
1.6 INTERFACE
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1.7 EQUIPMENT REQUIRED BUT NOT SUPPLIED
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1-7
Rev. E
WX-500
Installation Manual
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Table 1-6. Heading Input Cable Vendors
US
COMPANY
WR9'&3RZHU6XSSO\
:;7HVW&DEOH
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1-8
Rev. E
CABLE
P/N
Dallas Avionics
1-800-527-2581
214-320-9776
FAX 214-320-1057
WX-5
(6.84 lbs/100 ft)
1
Electronic Cable
Specialists
1-800-327-9473
414-421-5300
FAX 414-521-5301
3N6607
(7.5 lbs/100 ft)
A.E. Petsche
817-461-9473
FAX 817-277-2887
TZGYR
(6.84 lbs/100 ft)
EDMO Distributors
1-800-235-3300
805-295-6689
FAX 1-800-828-0623
FAX 805-295-6703
WX-1000
SYNCHRO
PIC Wire and Cable
1-800-742-3191
262-246-0500
FAX 262-246-0450
WM25807
(7.2 lbs/100 ft)
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WX-500
Installation Manual
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1.8 INSTALLATION APPROVAL
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1-9
Rev. E
WX-500
Installation Manual
7KLVSDJHLQWHQWLRQDOO\OHIWEODQN
1-10
Rev. E
WX-500
Installation Manual
CHAPTER 2
INSTALLATION
2.1 INTRODUCTION
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CAUTION
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2-1
Rev. E
WX-500
Installation Manual
2.3 PRE-INSTALLATION TEST PROCEDURE
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Figure 2-1. Test Cable
2.3.2 Test Procedure
CAUTION
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2-2
Rev. E
WX-500
Installation Manual
Figure. 2-2 Test Setup
Table 2-1. WX-500 LED Status
COMMUNICATION
LED
NORMAL OPERATION
FAILED OPERATION
DSP
LED 1
ON
OFF
MAIN
LED 7
OFF
ON
LED 8
ON/OFF - ONCE PER SECOND
DOES NOT PULSE ONCE PER SECOND
*For bench test ignore operation of all other LEDs
2-3
Rev. E
WX-500
Installation Manual
2.4 ANTENNA LOCATION
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2-4
Rev. E
WX-500
Installation Manual
2.4.4 Ground Plane
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ACCESS PANEL
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2.4.5 Alignment
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2-5
Rev. E
WX-500
Installation Manual
2.5 ANTENNA AND DOUBLER INSTALLATION
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Figure 2-3. Antenna Mounting Holes
1.
Use the antenna doubler plate as a template to mark hole locations on the aircraft skin.
NOTE
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2.
Attach the doubler plate to the inside of the fuselage as shown in figure 2-4.
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CAUTION
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a.
b.
2-6
Rev. E
For non-pressurized aircraft, use a non-corrosive sealant that meets the physical requirements
of MIL-A-446146 such as General Electric RTV162
For pressurized aircraft, use a sealant that meets the requirements of SAE AMS-S-8802 such
as Flamemaster® CS3204 class B.
WX-500
Installation Manual
Figure 2-4. Antenna and Doubler Installation
2-7
Rev. E
WX-500
Installation Manual
2.6 PROCESSOR LOCATION
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2.7 HEADING INPUT & STABILIZATION
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2-8
Rev. E
WX-500
Installation Manual
2.8 MATING CONNECTORS
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2-9
Rev. E
WX-500
Installation Manual
2.9 CONFIGURATION JUMPERS
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Table 2-2. Configuration Jumpers
FUNCTION
CONFIGURATION JUMPER
ANTENNA
J3-3
BOTTOM POSITION
(OPEN)
TOP POSITION
(JUMPER)
HEADING INPUT
J3-1
J3-2
NONE
(OPEN)
(OPEN)
SYNCHRO
(JUMPER)
(OPEN)
STEPPER
(OPEN)
(JUMPER)
RS-232 or RS-422
(JUMPER)
(JUMPER)
HEADING FLAG SENSE
J3-4
(JUMPER)
> 5 VOLT ON J2-24 RELATIVE
TO J2-25 INDICATES HEADING
INFO IS VALID
(OPEN)
< 1 VOLTS ON J2-24 RELATIVE
TO J2-25
INDICATES
INFO IS VALID
HEADING
• Configuration ground is available at J2 pins 6,7,8,18,19,20 and 21
• Configuration jumpers wired to configuration ground when jumper is required
•
•
Only one heading input should be enabled
Figure 2-11 shows the WX-500 heading validation circuit along with a typical connection of a
navigational system (such as the King KCS55) that provides a heading valid signal to the WX500
2.10 CABLE REQUIREMENTS AND FABRICATION
NOTES
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2-10
Rev. E
WX-500
Installation Manual
Figure 2-6. Interconnect Wiring
2-11 (page 2-12 blank)
Rev. E
WX-500
Installation Manual
2.10.1 Antenna Cable P/N 803-10950-( ) or P/N 803-10952-( )
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Figure 2-7. Antenna Cable
Figure 2-8. Antenna Cable Preparation
2-13
Rev. E
WX-500
Installation Manual
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SDVVHGWKURXJKLQGLYLGXDOO\PXVWEHXVHG7KHDQWHQQDFDEOHPXVWQRWVKDUHDEXONKHDG
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7KHDQWHQQDFDEOHPD\WLHWRRWKHUHOHFWULFDOFDEOHVDWULJKWDQJOHV
7KHDQWHQQDFDEOHRYHUDOOVKLHOGLVWHUPLQDWHGDWWKHDQWHQQDHQGRQO\
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Table 2-3. Antenna Cable Connections
SIGNAL
X_LOOP
+12V
SENSE
ANTREF
-12V
Y_LOOP
ANT_TEST
ANT_COM
WIRE COLOR
ORANGE
RED
BROWN
BLACK
YELLOW
GREEN
BLUE
DRAIN
CONNECTOR PIN NUMBER
WX-500
ANTENNA
J2-3
C
J2-16
D
J2-17
B
J2-2
J
J2-15
F
J2-4
G
J2-14
H
J2-1
A
5HIHUWRSDUDJUDSKIRUDQWHQQDDQGGRXEOHULQVWDOODWLRQ
2.10.2 Power Cable
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EUHDNHU7KHQHJDWLYHZLUHFRQQHFWVWRDLUIUDPHJURXQG,IDLUIUDPHJURXQGLVQRWDYDLODEOHUXQD
VHSDUDWHZLUHWRSRZHUJURXQGDWWKHEDWWHU\
CAUTION
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2-14
Rev. E
WX-500
Installation Manual
2.10.3 Heading Input Cable
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NOTE
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Figure 2-9. Heading Input Cable
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Figure 2-10. Heading Input Cable Preparation
2-15
Rev. E
WX-500
Installation Manual
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Figure 2-11. Heading Flag (KCS55) Connection
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NOTE
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2-16
Rev. E
WX-500
Installation Manual
Table 2-4. Stepper Input Connections
(KI-525 Indicator)
WIRE COLOR
SIGNAL
DRIVE MOTOR 1
HDG FLAG +
HDG FLAG UNREG +15
DRIVE MOTOR 3
SUB-CABLE
WHITE
WHITE
WHITE
ORANGE
ORANGE
BLUE
BLUE
WIRE
WHITE
BLUE
ORANGE
WHITE
BLUE
WHITE
BLUE
SIGNAL GND*
WX-500
PROCESSOR
PIN NUMBER
J2-10
J2-11
J2-23
J2-24
J2-25
J2-13
J2-12
KI-525
INDICATOR
N/C
N/C
P2-A (BOTTOM)
FLAG +
FLAG P1-v (TOP)
P2-H (BOTTOM)
CASE GND
P1- j (TOP)
*Connect outer shield at KI-525, P1- j (TOP)
Table 2-5 Synchro Connections to Mating Connector
SYNCHRO CONNECTION TO WX-500 MATING CONNECTOR
SIGNAL
PIN
SUB-CABLE
WIRE
COLOR
Cessna ARC 200-9BC
Cessna ARC 40840-0204
Cessna Slaved DG
AIM Type 289-1-2
AIM Type 2892D
AIM Type 2892ED
Collins Type 331P-1V
Collins Type 331P-1
Century NSD360/A DG &
722/755, Connector CD129
Century Slaved DG
King KCS-55 w/KI-525A-01
King KCS-55A w/KI-525A-01
Sperry C6E, C6J
Sperry C6, C6A, C6C
Sperry C-14d
HDG
FLAG +
J2-24
ORANGE
WHITE
HDG
FLAG J2-25
ORANGE
BLUE
SYNC
X
J2-10
WHITE
WHITE
SYNC
Y
J2-23
WHITE
ORANGE
SYNC
Z
J2-11
WHITE
BLUE
SYNC
REF HI
J2-13
BLUE
WHITE
SYNC
REF LO
J2-12
BLUE
BLUE
N/A
N/A
N/A
N/A
N/A
N/A
N/A
N/A
N/A
N/A
N/A
N/A
N/A
N/A
N/A
N/A
A
N
E
E
M
M
N
N
E
M
D
D
N
N
M
M
D
L
A
A
K
K
D
D
C
B
C
H
L
L
B
B
B
L
B
C
K
K
L
L
N/A
N/A
1
2
3
7
5
N/A
N/A
P1-v
N/A
N/A
e
N/A
N/A
P2-P
N/A
N/A
GND
N
P2-s
P2-s
39
18
a
M
P2-v
P2-v
38
19
b
L
P2-t
P2-t
40
20
Z
B
P2-r
P2-r
37
21
X
L
P2-u
P2-u
36
41
Y
2-17
Rev. E
WX-500
Installation Manual
2.10.4 Inhibit Line
NOTE
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2.10.5 Remote Clear Line
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2.10.7 SYSTEM_ON Output
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2.11 MOUNTING TRAY INSTALLATION
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2-18
Rev. E
WX-500
Installation Manual
DRILLING DETAIL
DRILLING DETAIL
NOT TO SCALE
NOT TO SCALE
DRILLING DETAIL
NOT TO SCALE
7.25
(184.2)
1.13 (28.7) 0.70 (17.8)
8.00
(203.2)
2.80
(71.1)
3.55
(90.2)
0.19 (4.8) DIA
(4 PLACES)
8.00
(203.2)
0.19 (4.8) DIA
(3 PLACES)
0.19 (4.8) DIA
(4 PLACES)
10-32 X 1-1/2
P/N 26-1004-9152-6
(4 PLACES)
10-32 X 3/8
MS51958-61
(3 PLACES)
10-32 X 3/8
MS51958-61
(3 PLACES)
3/8 X 3/8 SPACER
P/N 101-10131-001
(4 PLACES)
AIRCRAFT
PANEL
10-32 ELASTIC STOP NUT
P/N 101-10098-001
(4 PLACES)
VERTICAL
AIRCRAFT PANEL
AIRCRAFT PANEL
10-32 ELASTIC STOP NUT
P/N 101-10098-001
(3 PLACES)
10-32 ELASTIC STOP NUT
P/N 101-10098-001
(3 PLACES)
LEFT SIDE
RIGHT SIDE
NOTE
DIMENSIONS ARE IN INCHES (MILLIMETERS)
Figure 2-12. Mounting Tray Installation
2-19 (page 2-20 blank)
Rev. E
WX-500
Installation Manual
2.12 PROCESSOR INSTALLATION
CAUTION
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NOTE
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Figure 2-13. Processor Installation
2.13 PERFORMANCE TEST
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2-21
Rev. E
WX-500
Installation Manual
7KLVSDJHLQWHQWLRQDOO\OHIWEODQN
2-22
Rev. E
WX-500
Installation Manual
CHAPTER 3
INSTALLATION CHECKOUT
3.1 INTRODUCTION
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NOTICE
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3.2 CONTROLS
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NOTE
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31
3.3 POST INSTALLATION CHECKOUT
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3-1
Rev. E
WX-500
Installation Manual
NOTE
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Figure 3-1. System Data Screens
NOTE
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Installation Manual
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3-3
Rev. E
WX-500
Installation Manual
Figure 3-3. WX-PA Antenna Alignment
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WX-500
Installation Manual
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3-5
Rev. E
WX-500
Installation Manual
Figure 3-4. Electrical Noise Test
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3-6
Rev. E
WX-500
Installation Manual
CHAPTER 4
MAINTENANCE
4.1 INTRODUCTION
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4.3 PERIODIC MAINTENANCE
NOTE
Upon delivery to a customer, the dealer should recommend an annual checkout of the sensor,
especially prior to the thunderstorm season.
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4.3.2 Antenna
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4-1
Rev. E
WX-500
Installation Manual
4.4 TEST MODES
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4-2
Rev. E
WX-500
Installation Manual
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4-3
Rev. E
WX-500
Installation Manual
4.4.2 Fault Log
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4-4
Rev. E
WX-500
Installation Manual
4.4.3 Noise Monitor
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4-5
Rev. E
WX-500
Installation Manual
4.4.4 Test Strikes
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4-6
Rev. E
WX-500
Installation Manual
4.5 FAULT ISOLATION
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Table 4-1. Errors
ERROR
PROBABLE CAUSE
CORRECTIVE ACTION
ERROR 01. Processor Fault.
Main processor
Continued operation is not possible.
Contact Field Service.
ERROR 05. Processor Fault.
Main processor memory
Continued operation is not possible.
Contact Field Service.
ERROR 06. Processor Fault.
Main processor memory
Continued operation is not possible.
Contact Field Service.
ERROR 07. Processor Fault.
Main processor memory
Continued operation is not possible.
Contact Field Service.
ERROR 08. Processor Fault.
Main processor memory
Continued operation is not possible.
Contact Field Service.
ERROR 09. Processor Fault.
DSP processor memory
Continued operation is not possible.
Contact Field Service.
ERROR 10. Processor Fault.
DSP processor memory
Continued operation is not possible.
Contact Field Service.
ERROR 11. Processor Fault.
DSP processor memory
Continued operation is not possible.
Contact Field Service.
4-7
Rev. E
WX-500
Installation Manual
Table 4-1. Errors (Continued)
ERROR
PROBABLE CAUSE
CORRECTIVE ACTION
ERROR 12. Processor Fault.
DSP processor memory
Continued operation is not possible.
Contact Field Service.
ERROR 14. Processor Fault.
DSP processor
Continued operation is not possible.
Contact Field Service.
ERROR 15. Processor Fault.
DSP processor
Continued operation is not possible.
Contact Field Service.
ERROR 16. Antenna Fault.
Antenna or Antenna wiring
Weather mapping is inhibited.
a. Check antenna wiring for opens and shorts.
b. Use test cable to isolate between antenna
and aircraft wiring.
c. Contact Field Service.
ERROR 17. Processor Fault.
No test strikes, antenna in noisy
location, or faulty antenna.
Weather mapping is inhibited.
a. Check antenna wiring for opens and shorts.
b. Check for presence of noise using built-in
NOISE MONITOR or a WX-SM skinmapper.
c. If airborne near Annapolis, may be ground
transmitter.
d. Fault will clear automatically if interference
subsides.
e. Contact Field Service.
ERROR 18. Processor Fault.
Invalid test strikes, antenna in noisy
location or faulty antenna.
Weather mapping is inhibited.
a. Check antenna wiring for opens and shorts.
b. Check for presence of noise using built-in
NOISE MONITOR or a WX-SM skinmapper.
c. Fault will clear automatically if interference
subsides.
d. Contact Field Service.
ERROR 19. Processor Fault.
Main Processor or Antenna in noisy
location.
Weather mapping is inhibited.
a. Check for presence of noise using built-in
NOISE MONITOR or a WX-SM skinmapper.
b. If airborne near Annapolis, may be ground
transmitter.
c. Fault will clear automatically if interference
subsides.
d. Contact Field Service.
ERROR 20. Configuration Changed.
Antenna location (top/bottom,
determined by processor wiring)
changed since system was last
powered up.
Select Antenna Location
a. That corresponds to Stormscope system
antenna location.
b. If jumper does not agree with user selection,
the error message remains displayed and
status will change to “fatal error”.
c. Check jumper selection in mating connector
assembly (refer to paragraph 2.9, table 2-2).
d. At MFD, select antenna location.
e. Contact Field Service
This may occur the first time the
system is powered on in a new
installation or after the configuration
wiring is changed.
ERROR 21. Processor Fault.
4-8
Rev. E
Main processor
Continued operation is not possible.
Contact Field Service.
WX-500
Installation Manual
Table 4-1. Errors (Continued)
ERROR
PROBABLE CAUSE
CORRECTIVE ACTION
ERROR 22. Invalid XYZ Input.*
The system is configured for
synchro heading but the XYZ
synchro signals are not present or
are out of specification.
Heading stabilization is not available.
a. Check wiring between heading system and
WX-500 processor.
b. Check configuration wiring to make sure
system is set up for proper heading type
(stepper, synchro or serial).
c. If heading signals become valid, the system
will recover automatically.
d. Contact Field Service.
ERROR 23. Invalid Heading Ref.*
The system is configured for
synchro heading but the heading
reference (400 Hz) is not present or
out of specification.
Heading stabilization is not available.
a. Check wiring between heading system and
WX-500 processor.
b. Check configuration wiring to make sure
system is set up for proper heading type
(stepper, synchro or serial).
c. If the reference signal become valid, the
system will recover automatically.
d. Contact Field Service.
ERROR 24. MIC KEY STUCK.
Mic key (inhibit line) has been
asserted for at least 60 seconds.
Weather mapping is inhibited.
a. Check inhibit line wiring.
b. If inhibit line not used, leave it unconnected.
c. Check power to comms radio; if off, the radio
may be asserting the inhibit line.
d. Contact Field Service.
ERROR 25 - 34. Processor Fault.
Main processor
Continued operation is not possible.
Contact Field Service.
ERROR 35. Processor Fault.
Main or DSP processor
Continued operation is not possible.
Contact Field Service.
ERROR 36. Processor Fault.
Main or DSP processor
Continued operation is not possible.
Contact Field Service.
ERROR 40. Processor Fault.
Main processor
Continue without weather mapping functions.
Contact Field Service.
ERROR 41. Processor Fault.
Main or DSP processor
Continued operation is not possible.
Contact Field Service.
ERROR 42. Processor Fault.
Main processor
Continued operation is not possible.
Contact Field Service.
ERROR 43. Invalid request.
MFD
Message error will clear once processed
a. Excessive noise on communication lines,
check wiring.
b. If error occurs frequently, contact Field
Service.
ERROR 44 - 49.
MFD
Message error will clear once processed
Serial Communication.
a. Improper baud rate from MFD.
b. Excessive noise on communication lines,
check wiring.
c. If error occurs frequently, contact Field
Service.
* ERROR 22 and 23 (i.e., heading errors) are not written to the Fault Log (see paragraph 4.4.2).
4-9
Rev. E
WX-500
Installation Manual
Table 4-1. Errors (Continued)
ERROR
PROBABLE CAUSE
CORRECTIVE ACTION
ERROR 50. Illegal Serial Heading
Value.
MFD
ERROR 51. Invalid Message.
MFD
ERROR 52. Invalid Antenna
Change Request.
MFD
ERROR 53 - 54. Communications
Buffer Overload.
MFD
Message error will clear once processed
a. Excessive noise on communication lines,
check wiring.
b. If error occurs frequently, contact Field
Service.
Message error will clear once processed
a. Excessive noise on communication lines,
check wiring.
b. If error occurs frequently, contact Field
Service.
Message error will clear once processed
a. A request was received to change the
antenna mount to a location that does not
match the configuration jumpers. Request
is ignored.
b. If error occurs frequently, contact Field
Service.
Message error will clear once processed
a. Excessive noise on communication lines,
check wiring.
b. If error occurs frequently, contact Field
Service.
Heading flag indicator (FLG) appears
in weather screens.
Heading Flag
a. It is normal for the heading flag indicator to
be present if the heading flag line is asserted
b. The heading flag indicator will also be
present if a heading related fault is present
(Error 22,23).
c.
4-10
Rev. E
Serial heading is selected by configuration
jumpers, but not being received by WX-500.
WX-500
Installation Manual
Table 4-2. LED Status
COMMUNICATION
LED
NORMAL OPERATION
FAILED OPERATION
DSP
LED 1
ON
OFF
LED 6
TOGGLES ON/OFF (WHEN STRIKE IS DETECTED)*
DOES NOT TOGGLE ON/OFF WHEN
STRIKE IS PRESENT
LED 7
OFF
ON
LED 8
ON/OFF - ONCE PER SECOND
ON or OFF
(DOES NOT PULSE ONCE PER SECOND)
TX
RESERVED FOR FUTURE USE
RESERVED FOR FUTURE USE
RX
RESERVED FOR FUTURE USE
RESERVED FOR FUTURE USE
TX
ON
(PULSES WHEN TX OCCURS)**
OFF or ON
(DOES NOT PULSE EVERY 2 SECONDS)
RX
ON
(PULSES WHEN RX OCCURS)**
OFF or ON
(DOES NOT PULSE EVERY 2 SECONDS)
MAIN
SERIAL
*
Should pulse once every 10 seconds due to the internal self test strike.
** Serial communication occurs every 2 seconds, causing LEDs to rapidly pulse. Due to transmission speed, LEDs may
appear not to change conditions during TX/RX operation.
•
For installation troubleshooting ignore the conditions of all LEDs not listed in table 4-2.
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WX-500
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Installation Manual
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Installation Manual
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APPENDIX A
WX-500 INTERFACE
SIGNAL & CABLE CHARACTERISTICS
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WX-500
Installation Manual
APPENDIX B
ENVIRONMENTAL QUALIFICATION FORMS
This appendix includes the environmental qualification forms required for the WX-500 system. Forms
included are for the WX-500 and NY163 antenna.
B.1 WX-500 ENVIRONMENTAL QUALIFICATION FORM
(Reference Document 016-11521-001, Rev. B)
MODEL:
PART NO:
WX-500
805-11500-001
TSO NO: TSO-C110a
APPLICABLE SPEC. NO: RTCA/DO-191
MANUFACTURER: BFGoodrich Avionics Systems, Inc.
ADDRESS:
1105 Schrock Road, Suite 800, Columbus, Ohio 43229
CONDITION
SECTION/
PARAGRAPH
(614)825-2001
TEST DESCRIPTION
Temperature and Altitude
Operating Low Temperature
Operating High Temperature
Short-Time Operating High Temperature
Loss of Cooling
Ground Survival Low Temperature
Ground Survival High Temperature
Altitude
4.0
4.5.1
4.5.3
4.5.2
4.5.4
4.5.1
4.5.2
4.6
Tested to Category F2-55 Degrees Celsius
+70 Degrees Celsius
+70 Degrees Celsius
- Not Applicable -55 Degrees Celsius
+85 Degrees Celsius
55,000 Feet MSL
Temperature Variation
5.0
Tested to Category B
Humidity
6.0
Tested to Category A
Operational Shock and Crash Safety
Operational Shock
Crash Safety
7.0
7.2
7.3
6 g’s Peak
15 g’s all axes
Vibration
8.0
Tested to Categories [NBM]
Instrument Panel Mount
Without Vibration Isolators
Explosion Proofness
9.0
Category X - No Test Required
Waterproofness
10.0
Category X - No Test Required
Fluids Susceptibility
11.0
Category X - No Test Required
Sand and Dust
12.0
Category X - No Test Required
Fungus Resistance
13.0
Category X - No Test Required
B-1
Rev. E
WX-500
Installation Manual
WX-500 ENVIRONMENTAL QUALIFICATION FORM (Continued)
CONDITION
SECTION/
PARAGRAPH
TEST DESCRIPTION
Salt Spray
14.0
Category X - No Test Required
Magnetic Effect
15.0
Tested to Class Z
Power Input
16.0
Tested to Category AB
Voltage Spike
17.0
Tested to Category A
Audio Frequency Susceptibility
18.0
Tested to Category B
Induced Signal Susceptibility
19.0
Tested to Category Z
Radio Frequency Susceptibility
20.0
Tested to Category T
Radio Frequency Emission
21.0
Tested to Category Z
Lightning Induced Transient Susceptibility
22.0
Tested to Category AZEZ
Lightning Direct Effects
23.0
Category X - No Test Required
Icing
24.0
Category X - No Test Required
Other Tests
B-2
Rev. E
No Test Required
WX-500
Installation Manual
B.2 NY163 ANTENNA ENVIRONMENTAL QUALIFICATION FORM
(Reference Document 016-10930-001, Rev. 01)
MODEL:
PART NO:
NY163
805-10930-001
TSO NO: TSO-C110a
APPLICABLE SPEC. NO: RTCA/DO-197
MANUFACTURER: BFGoodrich FlightSystems, Inc.
ADDRESS:
2001 Polaris Parkway, Columbus, Ohio 43240-2001, (614)825-2001
˝
˝
CONDITION
SECTION/
PARAGRAPH
TEST DESCRIPTION
Temperature and Altitude
Operating Low Temperature
Operating High Temperature
Loss of Cooling
Ground Survival Low Temperature
Ground Survival High Temperature
4.0
4.5.1
4.5.2 & 4.5.3
4.5.4
4.5.1
4.5.2
Tested to Category F2-55 Degrees Celsius
+70 Degrees Celsius
- Not Applicable -55 Degrees Celsius
+85 Degrees Celsius
Altitude
4.6
55,000 Feet MSL
Temperature Variation
5.0
Tested to Category A
Humidity
6.0
Tested to Category C
Operational Shock and Crash Safety
Operational Shock
Crash Safety
7.0
7.2
7.3
6 g’s Peak
15 g’s all axes
Vibration
8.0
YLMC
Explosion Proofness
9.0
Category X - No Test Required
Waterproofness
10.0
Category S - Hermetically Sealed
Fluids Susceptibility
11.0
Category F - Ethylene Glycol
Sand and Dust
12.0
Category X - No Test Required
Fungus Resistance
13.0
Category X - No Test Required
Salt Spray
14.0
Category X - No Test Required
Magnetic Effect
15.0
Category X - No Test Required
Power Input
16.0
Category X - No Test Required
Voltage Spike
17.0
Category X - No Test Required
Audio Frequency Susceptibility
18.0
Category X - No Test Required
B-3
Rev. E
WX-500
Installation Manual
NY163 ANTENNA ENVIRONMENTAL QUALIFICATION FORM (Continued)
˝
CONDITION
SECTION/
PARAGRAPH
TEST DESCRIPTION
Induced Signal Susceptibility
19.0
Tested to Category Z
Radio Frequency Susceptibility
20.0
Category X - No Test Required
Radio Frequency Emission
21.0
Tested to Category Z
Lightning Induced Transient Susceptibility
22.0
Tested to Category XXE3
Lightning Direct Effects
23.0
Category X - No Test Required
Icing
24.0
Category X - No Test Required
Other Tests
L-Band Interference
B-4
Rev. E
BFGoodrich FlightSystems Defined Test
WX-500
Installation Manual
APPENDIX C
DISPLAY INTERFACE
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DQGLQWHUFRQQHFWLQIRUPDWLRQVHHWDEOH%56LQWHUIDFHRU%56LQWHUIDFH)RULQWHUFRQQHFW
ZLULQJGLDJUDPUHIHUHQFHILJXUH,QWHUIDFHWRWKH0)'LVYLDDVWDQGDUG56RU56VHULDOSRUW
CAUTION
(YHU\HIIRUWKDVEHHQPDGHWRFRUUHFWO\LGHQWLI\WKHSDUWQXPEHUVDQGSLQ
QXPEHUVOLVWHGLQWDEOHV%DQG%+RZHYHU*RRGULFK$YLRQLFV6\VWHPV
FDQQRWEHUHVSRQVLEOHIRUFKDQJHVPDGHE\RWKHUPDQXIDFWXUHUV,WLVWKH
UHVSRQVLELOLW\RIWKHLQVWDOOHUWRFRQILUPFRPSDWLELOLW\&RQWDFWWKHGLVSOD\
PDQXIDFWXUHUIRUWKHODWHVWLQIRUPDWLRQUHODWLQJWRWKHLUSURGXFW
Table C-1. WX-500 Compatible Displays – RS-232 Interface
WX-500
INTERCONNECT WIRING
MANUFACTURER/MODEL
REMARKS
J3-20
J3-8
J2-5
CASE
RS232TX
RS232RX
RS232GND
GND
GREEN
WHITE
BLACK
N/C
RPU-17
RPU-16
RPU-13
RPU-18
P529-12
P529-11
P529-8
P2-2
P2-20
P2-34
J1-3
J1-4
J1-5
Requires software version 1.1 or
later.
ARCHANGEL AE1002 or AE1004
Use cable CDS901-3.
RPU: P/N 453-2530-08
ARNAV MFD 5000 SERIES
ARNAV ICDS 2000
Requires software V520CG or later.
Connected as an RS-232 Auxiliary
device (P2) via the 24 pin MFD RPU
connector.
Requires software V920AE or later
Tray Assembly: P/N D98-00002
CPU/Display: P/N D98-00001-XX
AVIDYNE MFD 5RR-MFC-XXX
Software: P/N: 530-0101 release 2.0
or later.
P2-36
Connected via P2 located at tray
assembly.
L-3 Avionics Systems
RGC250/RGC350
Provides interface to various weather
radar indicators
Connected via J1 at RGC mating
connector assembly.
C-1
Rev. E
WX-500
Installation Manual
Table C-1. WX-500 Compatible Displays – RS232 Interface
&RQWLQXHG
WX-500
INTERCONNECT WIRING
MANUFACTURER/MODEL
EVENTIDE
ARGUS 5000-25-xx & 5000CE
ARGUS 7000-25-xx & 7000/CE
GARMIN®
GPS 400
GNC 420
GNS 430
GARMIN® GNS 530
SANDEL SN3308
REMARKS
Requires software version 05.1x or
later.
J3-20
J3-8
J2-5
CASE
RS232TX
RS232RX
RS232GND
GND
1P1-18
1P1-19
1P1-10
1. When heading is available to the
4xx, it outputs serial heading to the
WX-500. Where possible, the
WX-500 should be connected
directly to the aircraft heading
source (synchro preferred). See
paragraph 2.7.
CHAN 4
P4001-55
CHAN 4
P4001-54
Aircraft
Ground
CHAN 3
P4001-42
CHAN 3
P4001-4
CHAN 2
P4001-59
CHAN 2
P4001-58
2. Requires software V2.20 or higher.
CHAN 1
P4001-57
CHAN 1
P4001-56
1. When heading is available to the
GNS, the GNS outputs serial
heading to the WX-500. Where
possible, the WX-500 should be
connected directly to the aircraft
heading source (synchro
preferred). See paragraph 2.7.
CHAN 4
P5001-55
CHAN 4
P5001-54
CHAN 3
P5001-42
CHAN 3
P5001-4
CHAN 2
P5001-59
CHAN 2
P5001-58
2. Requires software V2.05 or higher.
CHAN 1
P5001-57
CHAN 1
P5001-56
Requires software version 1.0 or
later.
P3-32
P3-30
P1-3
J1-4
J1-21
J1-7
J1-5
J1-22
J1-6
J1-23
J1-3
J1-25
1P1-12 &
1P1-24
Connected via connector 1P1.
L-3 Avionics Systems I-linc
UPSAT MX-20
Port 1
Port 2
Port 3
Aircraft
Ground
Table C-2. WX-500 Compatible Displays – RS422 Interface
WX-500
INTERCONNECT WIRING
MANUFACTURER/MODEL
ARCHANGEL
AE1002 or AE1004
L-3 Avionics Systems I-linc
UPSAT MX-20
C-2
Rev. E
REMARKS
Requires software version 1.1 or later.
J3-25
J3-13
J2-24
J3-12
RS422TX+
RS422TX-
RS422RX+
RS422RX-
WHITE
BLACK
RED
GREEN
J1-11
J1-26
J1-8
J1-10
Use cable CDS901-3.
Port 4

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