Honeywell International Inc.
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Redmond, Washington 98052-5317
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Web site: www.myaerospace.com
SERVICE BULLETIN
NAVIGATION - MK V ENHANCED GROUND PROXIMITY WARNING SYSTEM (MK V EGPWS) - Conversion
of MK V EGPWS, PN 965-0976-003-Various, PN 965-0976-020-Various, PN 965-0976-040-Various, PN
965-0976-060-Various, and PN 965-1690-05X to PN 965-0976-003-232-232, PN 965-0976-020-232-232,
PN 965-0976-040-232-232, PN 965-0976-060-232-232, and PN 965-1690-055; Update Application and
Configuration Software Versions to -232.01-232.01 and Configuration Software Version to -055.01
Legal Notice
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This document contains technical data and is subject to U.S. export regulations. These commodities,
technology, or software were exported from the United States in accordance with the export administration
regulations. Diversion contrary to U.S. law is prohibited.
ECCN: 7E994, NLR Eligible.
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terms and conditions and those of a purchase order or acknowledgement.
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Publication Number D201002000016
© Honeywell International Inc. Do not copy without express permission of Honeywell.
SERVICE BULLETIN
965-0976/1690
1. License Grant - If you are a party to an applicable product support agreement, a Honeywell Service Center
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SERVICE BULLETIN
965-0976/1690
between you and Honeywell and may only be modified by a writing duly executed by the duly authorized
representatives of the parties.
Safety Advisory
WARNING: BEFORE THE MATERIALS CALLED OUT IN THIS PUBLICATION ARE USED, KNOW THE
HANDLING, STORAGE AND DISPOSAL PRECAUTIONS RECOMMENDED BY THE MANUFACTURER OR
SUPPLIER. FAILURE TO OBEY THE MANUFACTURERS’ OR SUPPLIERS’ RECOMMENDATIONS CAN
RESULT IN PERSONAL INJURY OR DISEASE.
This publication describes physical and chemical processes which can make it necessary to use chemicals,
solvents, paints, and other commercially available materials. The user of this publication must get the Material
Safety Data Sheets (OSHA Form 174 or equivalent) from the manufacturers or suppliers of the materials to
be used. The user must know the manufacturer/ supplier data and obey the procedures, recommendations,
warnings and cautions set forth for the safe use, handling, storage, and disposal of the materials.
Warranty/Liability Advisory
WARNING: HONEYWELL ASSUMES NO RESPONSIBILITY FOR ANY HONEYWELL EQUIPMENT
WHICH IS NOT MAINTAINED AND/OR REPAIRED IN ACCORDANCE WITH HONEYWELL’S PUBLISHED
INSTRUCTIONS AND/OR HONEYWELL’S FAA/SFAR 36 REPAIR AUTHORIZATION. NEITHER DOES
HONEYWELL ASSUME RESPONSIBILITY FOR SPECIAL TOOLS AND TEST EQUIPMENT FABRICATED
BY COMPANIES OTHER THAN HONEYWELL.
WARNING: INCORRECTLY REPAIRED COMPONENTS CAN AFFECT AIRWORTHINESS OR DECREASE
THE LIFE OF THE COMPONENTS. INCORRECTLY FABRICATED SPECIAL TOOLING OR TEST
EQUIPMENT CAN RESULT IN DAMAGE TO THE PRODUCT COMPONENTS OR GIVE UNSATISFACTORY
RESULTS.
Copyright - Notice
Copyright 2010, 2011 Honeywell International Inc. All rights reserved.
Honeywell, SmartLanding, and SmartRunway are registered trademarks of Honeywell International Inc.
All other marks are owned by their respective companies.
THIS IS THE SB FOSI - DATE: 20101101
15 Jun 2010
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© Honeywell International Inc. Do not copy without express permission of Honeywell.
SERVICE BULLETIN
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Transmittal Information
ATA Number 965-0976/1690-34-130 (Publication Number D201002000016)
Summary
This revision is a FULL replacement. This revision includes the changes that follow:
•
Two text corrections in the reason statement
•
Changed the content and format to agree with Honeywell processes in effect at the time of the release
of this revision.
The information that is identified with revision bars is listed in the Revision History section. Revision bars are
not used before Paragraph 1.A. The editorial changes and information that was moved or reformatted is
not identified with revision bars.
Revision History
This service bulletin has had two revision(s) as shown in Table 1.
Table 1. Revision History
Revision Number
Revision Date
0
15 Jun 2010
1
21 Sep 2010
2
3 Feb 2011
Highlights
This section issues Revision 2 to Service Bulletin, ATA Number 965-0976/1690-34-130 (Publication Number
D201002000016), and contains these changes:
The list of highlights tells the users about the changes that the revision makes. The list has three columns. The
"Page" column shows the block of data that the revision changes and the page on which the block begins.
The block can be a section, subsection, graphic, table, etc. Revision marks give the location of the change in
the block. The "Description" column tells the user about the change or changes in each block. A paragraph,
table, or figure reference often comes before the description. The "Effectivity" column tells the user about
the part number(s) to which the block of information applies. The default value for this column is "All." "All"
means that the block applies to all parts.
Page
Description
Effectivity
8
Paragraph 1.C.(1).(b).3. Changed 70 percent to 30 percent
All
9
Paragraph 1.C.(1).(b).4. Changed greater than 20 feet to greater than 5 feet
All
10
Paragraph 1.K.(1). Changed the website address
All
15 Jun 2010
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SERVICE BULLETIN
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1.
Planning Information
A.
Effectivity
(1)
This service bulletin is applicable to the MK V EGPWS with part numbers identified
in Table 2.
Table 2. Applicable MK V EGPWS Part Numbers
Software Version,
PN 965-0976-003
Software Version,
PN 965-0976-020
Software Version,
PN 965-0976-040
Software Version,
PN 965-0976-060
System PN
965-1690
-101-101
-208-208
-102-102
-214-214
-050
-102-102
-210-210
-103-103
-216-216
-051
-104-104
-212-212
-104-104
-217-217
-052
-105-105
-213-213
-105-105
-218-218
-054
-202-202
-214-214
-202-202
-219-219
-203-203
-216-216
-204-204
-220-220
-204-204
-217-217
-206-206
-222-222
-206-206
-218-218
-208-208
-224-224
-207-207
-219-219
-210-210
-226-226
-208-208
-220-220
-212-212
-228-228
-210-210
-222-222
-213-213
-230-230
-211-211
-224-224
-214-214
-212-212
-226-226
-216-216
-213-213
-228-228
-217-217
-214-214
-230-230
-218-218
-216-216
-219-219
-217-217
-220-220
-218-218
-222-222
-219-219
-224-224
-220-220
-226-226
-222-222
-228-228
-224-224
-230-230
-226-226
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SERVICE BULLETIN
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Table 2. Applicable MK V EGPWS Part Numbers (Cont)
Software Version,
PN 965-0976-003
Software Version,
PN 965-0976-020
Software Version,
PN 965-0976-040
Software Version,
PN 965-0976-060
System PN
965-1690
-228-228
-230-230
NOTES:
1.
If a unit identified in Table 2 has SmartRunway and SmartLanding functions activated before the software
update to -232-232 or -055, it is the customer’s responsibility to reactivate the SmartRunway and
SmartLanding functions on completion of the update. For details on activation of SmartRunway and
SmartLanding functions, refer to Service Bulletin, ATA 965-0976/1690-34-119 (Publication Number
D201005000024).
If a unit identified in Table 2 has runway awareness and advisory system (RAAS) functions activated before
the software update to -232-232 or -055, it is the customer’s responsibility to reactivate the RAAS functions
on completion of the update. For details on activation of RAAS functions , refer to Service Bulletin, ATA
965-0976/1690-34-72 (Publication Number 012-0687-177).
2.
B.
Concurrent Requirements
(1)
Terrain Database Version 435 is the minimum requirement for MK V EGPWS,
PN 965-0976-0XX-232-232 or PN 965-1690-055. Refer to Service Bulletin, ATA
965-0976-XXX-34-74 (Publication Number 012-0608-174), Update EGPWS With
Terrain Database Version 435 and Envelope Modulation Database Version B05.
(2)
For SmartRunway and SmartLanding functions to operate in the MK V EGPWS,
Terrain Database Version 456 or later is required. Refer to Service Information Letter,
Publication Number D200911000016, Terrain Database 456 and Envelope Modulation
Database B07 for MK V EGPWS, PN 965-0976-XXX-XXX-XXX and PN 965-1690-05X.
(3)
The service bulletins identified below must be done before or at the same time as the
conversion given in this service bulletin.
(a)
For MK V EGPWS, PN 965-0976-003-101-101, -102-102, -104-104, -105-105,
-202-202, -203-203, -204-204, -206-206, -207-207, -208-208, -210-210,
-211-211, -212-212, -213-213, -214-214, -216-216, -217-217, -218-218,
-219-219, -220-220, -222-222, -224-224, -226-226, -228-228, -230-230:
•
Service Bulletin, ATA Number 965-0976-00X-34-03 (Publication Number
012-0687-103), which installs MOD 1
NOTE:
•
Service Bulletin, ATA Number 965-0976-003-34-10 (Publication Number
012-0687-110), which installs MOD 2
NOTE:
•
Power supply modification to increase surge protection, PN
965-0976-003, MOD 2.
Service Bulletin, ATA Number 965-0976-0XX-34-11 (Publication Number
012-0687-111), which installs MOD 3
NOTE:
15 Jun 2010
Revision 2, 3 Feb 2011
Minor repairs and new boot loader software, PN 965-0976-003,
MOD 1.
Install updated boot loader software, PN 965-0976-003, MOD
3; PN 965-0976-040, MOD 1
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SERVICE BULLETIN
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•
Service Bulletin, ATA Number 965-0976-0XX-34-19 (Publication Number
012-0687-119), which installs MOD 4
Add program pins and Increase flash memory capacity,
965-0976-003 MOD 4, PN 965-0976-040, MOD 2
Service Bulletin, ATA Number 965-0976-0XX-34-20 (Publication Number
012-0687-120), which installs MOD 5
NOTE:
•
Correct flight history faults due to lack of update, PN
965-0976-003, MOD 5, PN 965-0976-040, MOD 3.
Service Bulletin, ATA Number 965-0976-0XX-34-22 (Publication Number
012-0687-122), which installs MOD 6
NOTE:
•
NOTE:
•
Service Bulletin, ATA Number 965-0976-0XX-34-25 (Publication Number
012-0687-125), which installs MOD 7.
NOTE:
(b)
Correct flight history faults due to the lack of update, PN
965-0976-003, MOD 6, PN 965-0976-040, MOD 4.
Improve clarity of all voices including the 100 feet altitude
callout, PN 965-0976-003, MOD 7, 965-0976-040, MOD 5
For MK V EGPWS, PN 965-0976-040-102-102, -103-103, -104-104, -105-105,
-202-202, -204-204, -206-206, -208-208, -210-210 -212-212, -213-213,
-214-214, -216-216, -217-217, -218-218, -219-219, -220-220, -222-222,
-224-224, -226-226, -228-228, -230-230:
• Service Bulletin, ATA Number 965-0976-0XX-34-11 (Publication Number
012-0687-111), which installs MOD 1
Install updated boot loader software, PN 965-0976-003, MOD
3, PN 965-0976-040, MOD 1.
Service Bulletin, ATA Number 965-0976-0XX-34-19 (Publication Number
012-0687-119), which installs MOD 2
NOTE:
•
Add program pins and Increase flash memory capacity, PN
965-0976-003, MOD 4, PN 965-0976-040, MOD 2.
Service Bulletin, ATA Number 965-0976-0XX-34-20 (Publication Number
012-0687-120), which installs MOD 3
NOTE:
•
Correct flight history faults due to lack of update, PN
965-0976-003, MOD 5, PN 965-0976-040, MOD 3.
Service Bulletin, ATA Number 965-0976-0XX-34-22 (Publication Number
012-0687-122), which installs MOD 4
NOTE:
•
NOTE:
•
Service Bulletin, ATA Number 965-0976-0XX-34-25 (Publication Number
012-0687-125), which installs MOD 5.
NOTE:
C.
Correct flight history faults due to the lack of update, PN
965-0976-003, MOD 6, PN 965-0976-040, MOD 4.
Improve clarity of all voices including the 100 feet altitude
callout, PN 965-0976-003, MOD 7, 965-0976-040, MOD 5.
Reason
(1)
This conversion updates the MK V EGPWS, PN 965-0976-0XX-XXX-XXX, to new
PN 965-0976-0XX-232-232 and PN 965-1690-05X, to new PN 965-1690-055. The
15 Jun 2010
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SERVICE BULLETIN
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update is the result of changes to the MK V EGPWS application software and the
configuration database. The changes to the application software and configuration
database are identified below.
(a)
Revised the application software to use the new runway database format to
support SmartRunway and SmartLanding functions.
• Honeywell introduced the SmartRunway and SmartLanding features in the
-230-230/-054 software release. During field usage, Honeywell discovered
an issue with Terrain Database Version 454 (and subsequently 455) that
resulted in some specific existing EGPWS part numbers occasionally
resetting and going inoperative (INOP) for 20 seconds. In order to resolve
this issue, Honeywell released Terrain Database Version 456, which
corrected the reset issue associated with Terrain Database Versions 454
and 455 and the specific EGPWS part numbers.
•
(b)
If SmartRunway and/or SmartLanding functions are activated, then
Terrain Database Version 456 or subsequent must be used. This release
incorporates a change to the application software to be compatible with
Terrain Database Version 456 and subsequent.
Boeing aircraft changes:
1
Added new aircraft type 232, P-8A MMA.
• This aircraft type includes system functions that are unique to this
aircraft configuration. A non-TSO low level operations mode is
provided.
•
2
Added heads-up-display (HUD) labels to the ARINC 429 output label
set for the aircraft types listed below. This allows the Rockwell Collins
HUD to provide aircraft braking display to the pilot.
• Aircraft type 199 – B757-200 Integrated
• Aircraft type 201 – B767-200 Integrated
• Aircraft type 205 – B777-200 Integrated
•
3
15 Jun 2010
Revision 2, 3 Feb 2011
When low level operations mode is active, Modes 1, 2, 4, and 6
are tailored to meet the operational requirements of this aircraft.
Changes are also made to the operational floors for the terrain
clearance floor and the terrain awareness functions.
Aircraft type 208 – B777-200LR/300ER with Windshear Update.
Added low airspeed monitor function to 737-NG aircraft types. There
have been a number of incidences where a slow loss of airspeed
has not been noticed by the pilots. On some aircraft equipped with
an electronic flight information system (EFIS) display, Boeing added
a yellow flashing box around the digital airspeed number when the
airspeed dips into more than 30 percent of the amber airspeed band.
The low airspeed monitor function is designed to issue an “Airspeed
Low – Airspeed Low” aural alert coincident with the flashing yellow
box. This function has been added to the following aircraft types:
• Aircraft type 195 – B737-600
• Aircraft type 196 – B737-700
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SERVICE BULLETIN
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4
(c)
•
Aircraft type 197 – B737-800
•
Aircraft type 207 – B737-700IGW
•
Aircraft type 212 – B737-NG Windshear Update.
Added a stuck radio altimeter check.
•
For aircraft configurations that use dual radio altimeters and an
air/ground switch, logic is added to switch to the alternate source
of radio altitude data when it has been determined that there is a
“stuck” radio altitude value.
•
A value is considered to be “stuck” when the aircraft is in air,
one radio altimeter is reading less than or equal to 0 feet, and
the other radio altimeter is reading greater than 5 feet. The
EGPWS will use the altitude value from the radio altimeter that is
outputting the higher value.
Embraer aircraft changes:
•
(d)
Aircraft type 33, EMB-145 - Added reference speed to support
SmartRunway and SmartLanding functionality.
Fokker aircraft changes:
•
Removed aircraft type 131, Fokker 100.
NOTE:
D.
This software release cannot be used by Fokker 100 operators.
Description
(1)
A summary of the work necessary to do this conversion is given below:
•
Preparation:
–
If a Personal Computer Memory Card Interface Association (PCMCIA) card
with the production software is used, no preparation is necessary.
–
If a PCMCIA card without the production software is used, one of the
procedures given below must be used:
–
The production software from a PCMCIA card is put into a different
PCMCIA card.
–
The production software from a compact disk-read only memory (CD
ROM) is put into a PCMCIA card.
•
The production software is put into the MK V EGPWS.
•
A check is done to make sure the production software is correct.
•
The production software versions and modification statuses are identified on the
EGPWS identification label.
•
If this conversion is done at a shop location with a MK V EGPWS ground support
equipment (EGPWS GSE), a test is done on the MK V EGPWS.
15 Jun 2010
Revision 2, 3 Feb 2011
NOTE:
This conversion can be done at a customer location (in the aircraft) or
at a shop location.
NOTE:
This is a software change only. The MK V EGPWS will not be
disassembled and the inspection seals will not be broken.
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SERVICE BULLETIN
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E.
Compliance
(1)
F.
Approval
(1)
G.
This conversion is optional. The operator can make the decision if this conversion is
necessary.
The upgrade outlined in this service bulletin includes approved conversion instructions
from the manufacturer. The configuration created by this conversion is approved
by the applicable regulatory agency and meets the requirements of TSO-C92c,
TSO-C151b, TSO-C117a, and TSO-C129a. This service bulletin approval applies
only to the MK V EGPWS. The MK V EGPWS aircraft installation approval must be
separately addressed.
Manpower
(1)
If this conversion is done at a customer location (in the aircraft):
•
0.5 hour(s) for the labor to do the conversion of the MK V EGPWS.
The time given does not include the time to get access to the MK V
EGPWS on the aircraft, to do the return-to-service tests.
NOTE:
(2)
H.
•
If the shop location uses MK V EGPWS GSE, 1.0 more hour(s) for the labor to do
a test of the MK V EGPWS.
Not applicable.
Not changed.
Software Accomplishment Summary
(1)
K.
0.5 hour(s) for the labor to do the conversion of the MK V EGPWS
Electrical Load Data
(1)
J.
•
Weight and Balance
(1)
I.
If this conversion is done at a shop location:
A Software Accomplishment Summary has been completed to agree with the
necessary conditions of RTCA document DO-178B, Software Considerations in
Airborne Systems and Equipment Certification.
References
(1)
To find, see, and download Honeywell Technical Publications, go to
www.myaerospace.com.
(2)
The document(s) that follow(s) is/are necessary to complete this conversion. Unless
specified differently, you can use subsequent revisions.
•
(3)
CMM, ATA Number 34-45-36 (Publication Number 012-0687-001), MK V Enhanced
Ground Proximity Warning System, Revision 36 with Temporary Revision 34-19.
The document(s) that follow(s) can possibly be necessary to complete this conversion.
Refer to Paragraph 1.B. Unless specified differently, you can use subsequent revisions.
15 Jun 2010
Revision 2, 3 Feb 2011
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•
Service Bulletin, ATA Number 965-0976-00X-34-03 (Publication Number
012-0687-103), Enhanced Ground Proximity Warning Computer, Incorporate
Modification Status (MOD) 1, Revision 0
NOTE:
For enhanced ground proximity warning computer (EGPWC), PN
965-0976-003.
•
Service Bulletin, ATA Number 965-0976-003-34-10 (Publication Number
012-0687-110), Enhanced Ground Proximity Warning Computer Change
Modification Status of 965-0976-003 to MOD 2, Revision 1
•
Service Bulletin, ATA Number 965-0976-0XX-34-11 (Publication Number
012-0687-111), Enhanced Ground Proximity Warning Computer Install Updated
Boot Loader Software, Revision 0
NOTE:
MOD 3 for EGPWC, PN 965-0976-003 and MOD 1 for PN
965-0976-040.
•
Service Bulletin, ATA Number 965-0976-0XX-34-19 (Publication Number
012-0687-119), MK V Enhanced Ground Proximity Warning System (EGPWS),
MOD 2 to Part Number 965-0976-040, MOD 4 to Part Number 965-0976-003,
Revision 3
•
Service Bulletin, ATA Number 965-0976-0XX-34-20 (Publication Number
012-0687-120), Enhanced Ground Proximity Warning Computer Correct Flight
History Faults Due to Lack of Update PN 965-0976-003, MOD 5 and PN
965-0976-040, MOD 3, Revision 1
•
Service Bulletin, ATA Number 965-0976-0XX-34-22 (Publication Number
012-0687-122), Enhanced Ground Proximity Computer Increase Output Amplitude
of 453 Transmitter PN 965-0976-003, MOD 6 and PN 965-0976-040, MOD 4,
Revision 0
•
Service Bulletin, ATA Number 965-0976-0XX-34-25 (Publication Number
012-0687-125), Enhanced Ground Proximity Computer Improve Clarity of All
Voices Including the 100ft Altitude Callout PN 965-0976-003, MOD 7 and PN
965-0976-040, MOD 5, Revision 0
•
Service Bulletin, ATA Number 965-0976-XXX-34-74 (Publication Number
012-0687-174), Update EGPWS with Terrain Database Version 435 and Envelope
Modulation Database Version B05, Revision 1
•
Service Bulletin, ATA Number 965-0976/1690-34-77 (Publication Number
012-0687-177), Enhanced Ground Proximity Warning System (EGPWS) - Part
No. 965-0976-0XX-218-218 or Higher and 965-1690-051 or Higher - Runway
Awareness and Advisory System (RAAS) Activation; Add RAAS Capability,
Revision 2
•
Service Information Letter, Publication Number D200911000016, Terrain Database
456 and Envelope Modulation Database B07 for MK V Enhanced Ground Proximity
Warning System (EGPWS), PN 965-0779-00X, PN 965-0976-0XX-XXX-XXX, PN
965-1676-00X, and PN 965-1690-05X, Revision 0.
15 Jun 2010
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SERVICE BULLETIN
965-0976/1690
(4)
The document(s) that follow(s) is/are recommended but not necessary to do this
conversion. Unless specified differently, you can use subsequent revisions.
•
Service Bulletin, ATA Number 965-0976/1690-34-125 (Publication Number
012-0687-225), MK V Enhanced Ground Proximity Warning System (EGPWS),
Part Number 965-0976-0XX-XXX-XXX and 965-1690-05X; Install a Terrain
Database and an Envelope Modulation Database, Revision 1
NOTE:
L.
M.
Generic installation of terrain database and envelope modulation
database.
Other Publications Affected
(1)
CMM, ATA Number 34-45-36 (Publication Number 012-0687-001), MK V Enhanced
Ground Proximity Warning System, will be revised because of this service bulletin.
(2)
This service bulletin has no effect on the test procedure.
Interchangeability or Intermixability of Parts
(1)
The operator must speak to the original equipment manufacturere (OEM) about the
interchangeability and intermixability of the MK V EGPWS part numbers identified
in this service bulletin.
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SERVICE BULLETIN
965-0976/1690
2.
Material Information
A.
Material - Price and Availability
(1)
Speak to Honeywell personnel at the location identified below for the necessary
documentation, applicable material and labor prices, available parts, and supply times.
Honeywell
Global Customer Care Center
Telephone: (800) 601-3099 (U.S.A.)
Telephone: (602) 365-3099 (International)
NOTE:
B.
(2)
This conversion can be done at a Honeywell service center or Honeywell-authorized
repair location for the price given at the time of the order.
(3)
Honeywell can supply the parts necessary to do this conversion. There will be no
cost to approved customers for 60 months after the initial release date of this service
bulletin. If you make an order for parts, send a no-charge purchase order that refers
to this Service Bulletin, ATA Number 965-0976/1690-34-130 (Publication Number
D201002000016) - free of charge (FOC). The purchase order must include only the
applicable parts specified in Table 3 of this service bulletin.
(4)
To activate SmartRunway and SmartLanding features, a separate reloadable customer
definitions (RCD) is required, which is chargeable and sold separately. Contact your
Honeywell customer care representative.
Industry Support Information
(1)
C.
Identified Global Material System (GMS) users can make an order for
the material at http://www.avionicservices.com/gms/login. Customers
who are not yet identified GMS users can use the same address to
apply for identification.
Honeywell will give no reimbursement to do this conversion. The customer will receive
an applicable invoice for the conversion of each MK V EGPWS done at a Honeywell
service center or Honeywell-authorized repair location.
Material Necessary for Each Component
(1)
If the conversion given in this service bulletin is done at a location other than a
Honeywell service center, complete the Customer Support Service Report (CSSR).
The CSSR is found in Paragraph 4.A. of this service bulletin.
(2)
The parts identified in Table 3 are necessary to do this service bulletin.
15 Jun 2010
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SERVICE BULLETIN
965-0976/1690
Table 3. Operator-Purchased Material
New PN
Keyword/ Nomenclature
Old PN
Qty
718-1461-069
Production software
PCMCIA card
(Version -232.01-232.01)
718-1461-060
As
required
(AR)
718-1471-074
Production software CD
ROM
(Version -232.01-232.01)
718-1471-065
AR
011-4070-001
MOD kit (for PN
965-0976-0XX)
None
1
718-1461-070
Production software
PCMCIA card
(Version -055.01)
718-1461-061
AR
718-1471-075
Production software CD
ROM (Version -055.01)
718-1471-066
AR
011-4070-002
MOD kit (for PN
965-1690-05X)
None
1
998-1955-655
MK V EGPWS
configuration matrix
diskette
Many
AR
NOTES:
1.
2.
List
Price
Instructions/
Disposition
Codes
1
2 3 4
1
2 3 4
1
2 3 6 8
1
2 3 4
1
2 3 4
1
2 3 7 8
1
2 3 5
There is no charge for this part.
Refer to the Honeywell Global Customer Care Center (Paragraph 2.A.) when you need data about available
parts, supply times, or minimum order quantities.
The customer or local regulatory authority can make decisions about what to do with the used parts.
Honeywell recommends that old part number software be discarded or erased.
The requirement for this item is determined by the procedure used to get the production software. Refer to
Paragraph 3.B. If the part is necessary, the quantity is one for each location that does this conversion.
This part is necessary if this conversion is done at a shop location with an EGPWS GSE. Refer to Paragraph
3.J. If the part is necessary, the quantity is one for each location that does this conversion. Dash numbers
higher than -655 are permitted alternatives. Refer to Paragraph 3.J.
This MOD kit is applicable to MK V EGPWS, PNs 965-0976-0XX. Refer to Paragraph 3.B.(1) for details.
This MOD kit is applicable to MK V EGPWS, PNs 965-1690-05X. Refer to Paragraph 3.B.(2) for details.
PN 965-0976-XXX denotes PN 965-0976-003, -020, -040 or -060. PN 965-1690-05X denotes PN
965-1690-050, -051, -052, -054.
3.
4.
5.
6.
7.
8.
(3)
D.
Material Necessary for Each Spare
(1)
E.
No operator-supplied material is necessary to do this service bulletin.
Same as Paragraph 2.C.
Reidentified Parts
(1)
Not applicable.
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SERVICE BULLETIN
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F.
Tooling - Price and Availability
(1)
The equipment specified in the locations identified below can possibly be necessary to
do this conversion. Equivalent alternatives are permitted for the equipment specified in
this paragraph. Use the applicable procedures to get and install the software to make
a decision about the necessary equipment. Unless specified differently or a Honeywell
part number is given, the equipment is available from commercial sources. Do not
send an order to Honeywell for the equipment as part of this service bulletin.
•
•
•
•
•
•
(2)
Paragraph
Paragraph
Paragraph
Paragraph
Paragraph
Paragraph
3.C.(1)
3.D.(1)
3.E.(1)
3.F.(1)
3.G.(1)
3.H.(1).
If this conversion is done at a shop location, the equipment specified in the documents
given in Paragraph 1.K. can also be necessary.
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SERVICE BULLETIN
965-0976/1690
3.
Accomplishment Instructions
A.
General Information
WARNING:
CAUTION:
(1)
TO AVOID INJURY TO PERSONNEL, BE AWARE THAT VOLTAGES ARE
PRESENT IN THE UNIT AND IN THE TEST EQUIPMENT. VOLTAGES
AS LOW AS 28 VOLTS CAN CAUSE SERIOUS INJURY UNDER SOME
CONDITIONS. DO NOT BE MISLED BY THE TERM “LOW VOLTAGE.”
THE MK V EGPWS CONTAINS ELECTROSTATIC DISCHARGE SENSITIVE
ITEMS. USE INDUSTRY APPROVED PRECAUTIONS.
Unless indicated otherwise, for the purpose of Paragraph 3 of this service bulletin:
(a)
(b)
MK V EGPWS, PN 965-0976-0XX is used to abbreviate:
1
MK V EGPWS, PN 965-0976-003-101-101, -102-102, -104-104,
-105-105, -202-202, -203-203, -204-204, -206-206, -207-207,
-208-208, -210-210, -211-211, -212-212, -213-213, -214-214,
-216-216, -217-217, -218-218, -219-219, -220-220, -222-222,
-224-224, -226-226, -228-228, -230-230.
2
MK V EGPWS, PN 965-0976-020-208-208, -210-210, -212-212,
-213-213, -214-214, -216-216, -217-217, -218-218, -219-219,
-220-220, -222-222, -224-224, -226-226, -228-228, -230-230.
3
MK V EGPWS, PN 965-0976-040-102-102, -103-103, -104-104,
-105-105, -202-202, -204-204, -206-206, -208-208, -210-210
-212-212, -213-213, -214-214, -216-216, -217-217, -218-218,
-219-219, -220-220, -222-222, -224-224, -226-226, -228-228,
-230-230.
4
MK V EGPWS, PN 965-0976-060-214-214, -216-216, -217-217,
-218-218, -219-219, -220-220, -222-222, -224-224, -226-226,
-228-228, -230-230.
MK V EGPWS, PN 965-1690-05X is used to abbreviate:
1
(2)
A PCMCIA card with the software identified below is necessary to do this conversion.
(a)
For MK V EGPWS, PN 965-0976-0XX:
1
(b)
Production PCMCIA card, PN 718-1461-069, for Software Version
-232.01-232.01 is used. Refer to Table 3.
For MK V EGPWS, PN 965-1690-05X:
1
(3)
MK V EGPWS, PN 965-1690-050, -051, -052, -054.
Production PCMCIA card, PN 718-1461-070, for Software Version
-055.01 is used. Refer to Table 3.
One of the three procedures identified below is permitted to get the PCMCIA card.
Only one PCMCIA card is necessary for each location that does this conversion.
(a)
A new production software PCMCIA card. The applicable PCMCIA card is
identified below. Do the instructions in Paragraph 3.C.
1
15 Jun 2010
Revision 2, 3 Feb 2011
PCMCIA card, PN 718-1461-069, for MK V EGPWS, PN
965-0976-0XX.
965-0976/1690-34-130
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SERVICE BULLETIN
965-0976/1690
PCMCIA card, PN 718-1461-070, for MK V EGPWS, PN
965-1690-05X.
2
B.
(b)
The data from a production software PCMCIA card, PN 718-1461-069 or PN
718-1461-070 is put into a PCMCIA card. Do the instructions in Paragraph 3.D.
(c)
The data from a production software CD ROM is copied into a PCMCIA
card. The applicable CD ROM card is identified below. Do the instructions
in Paragraph 3.E.
1
CD ROM, PN 718-1471-074, for MK V EGPWS, PN 965-0976-0XX
2
CD ROM, PN 718-1471-075, for MK V EGPWS, PN 965-1690-05X.
(4)
Obey the precautions.
(5)
If this conversion is done at a shop location, refer to the MK V Enhanced Ground
Proximity Warning System CMM, ATA Number 34-45-36 (Publication Number
012-0687-001), for procedures and precautions. Use all CAUTIONS and WARNINGS.
Refer to the IPL in the CMM for the location of the parts, unless specified differently.
(6)
If this service bulletin is done at a customer location (in the aircraft), the instructions in
Paragraph 3.F. will be used. If this service bulletin is done at a shop location without
an EGPWS GSE, the instructions in Paragraph 3.G. will be used. If this service
bulletin is to be done at a shop location with an EGPWS GSE, the instructions in
Paragraph 3.H. will be used.
(7)
This is a software change only. The MK V EGPWS is not disassembled and the
inspection seals are not broken.
Preparation
(1)
To perform the conversion of MK V EGPWS, PN 965-0976-0XX, get the MOD kit, PN
011-4070-001. Make sure the parts identified in Table 4 are in the kit.
Table 4. MOD Kit, PN 011-4070-001, Components For Use With MK V EGPWS, PN 965-0976-0XX
Find Number
Part Number
Description
Qty
1
402-6068-103
Cover up label
1
2
402-6068-107
Instruction label
1
3
620-2050-002
Software/configuration (SW/CFG) version
label
1
4
402-6105-001
Terrain database label
1
5
620-1907-193
PN label
(MK V EGPWS, PN 965-0976-003-232-232)
1
6
620-1907-194
PN label
(MK V EGPWS, PN 965-0976-020-232-232)
1
7
620-1907-195
PN label
(MK V EGPWS, PN 965-0976-040-232-232)
1
8
620-1907-196
PN label
(MK V EGPWS, PN 965-0976-060-232-232)
1
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SERVICE BULLETIN
965-0976/1690
(2)
To perform the conversion of MK V EGPWS, PN 965-1690-05X, get the MOD kit, PN
011-4070-002. Make sure the parts identified in Table 5 are in the kit.
Table 5. MOD Kit, PN 011-4070-002, Components For Use With MK V EGPWS PN 965-1690-05X
Find Number
Part Number
Description
Qty
1
402-6068-103
Cover up label
1
2
402-6068-107
Instruction label
1
3
402-6091-001
Software MOD status label
1
4
402-6105-001
Terrain database label
1
5
620-1907-202
PN label
(MK V EGPWS, PN 965-1690-055)
1
C.
New Production Software PCMCIA Card
This paragraph gives the procedure to use a new production software PCMCIA card.
NOTE:
(1)
No special equipment is necessary to do this procedure.
(2)
Get the applicable new production software PCMCIA card.
(a)
For MK V EGPWS, PN 965-0976-0XX, units:
1
(b)
For MK V EGPWS, PN 965-1690-05X, units:
1
(3)
D.
Production software PCMCIA card, PN 718-1461-069.
Production software PCMCIA card, PN 718-1461-070.
Make a decision about how to do the conversion of the MK V EGPWS.
(a)
If the conversion is to be done at a customer location (in the aircraft), go
to Paragraph 3.F.
(b)
If the conversion is to be done at a shop location without the EGPWS GSE, go
to Paragraph 3.G.
(c)
If the conversion is to be done at a shop location with the EGPWS GSE, go
to Paragraph 3.H.
PCMCIA Data
This paragraph gives the procedure to put the production software from one
PCMCIA card into a different PCMCIA card.
NOTE:
(1)
The equipment identified below is necessary to do this procedure:
(a)
For MK V EGPWS, PN 965-0976-0XX units:
1
(b)
For MK V EGPWS, PN 965-1690-05X units:
1
(c)
15 Jun 2010
Revision 2, 3 Feb 2011
Production software PCMCIA card, PN 718-1461-069.
Production software PCMCIA card, PN 718-1461-070.
A PCMCIA card identified in Table 6 or an equivalent.
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SERVICE BULLETIN
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Table 6. PCMCIA Source Data
Part Number
Company Data
CU10481
CU10481 Smart Modular Technologies
7 Lopez Road
Wilmington, MA 01887
U.S.A.
Telephone: (978) 988-8848
Web site: http://www.smartmodulartech.com
(d)
An IBM personal computer (PC) or an equivalent with a Pentium processor,
133 megahertz (MHz) or higher, and the items identified below:
•
Windows 95/98/ME or Windows 2000/XP
•
One of the items identified below:
–
PCMCIA drive with FlashTools software for WINDOWS 95/98/ME,
PN 331-0054-001
–
PCMCIA drive with FlashTools software for WINDOWS 2000/XP,
PN 331-0054-002
–
CSM OMNIDrive universal serial bus (USB) linear flash (LF) PC
card read-writer, OMNIDrive USB professional interface cable, and
OMNIDrive USB professional (PC card manager) software. These
OMNIDrive items are supplied together if an order is made for the
OMNIDrive part number given in Table 7.
Table 7. OMNIDrive Data
Part Number
Company Data
PCM-CR-U2EX-LF
Synchrotech
3333 Wilshire Boulevard, Suite 806
Los Angeles, CA 90010
U.S.A.
Telephone: (800) 793-9207 (U.S.A.)
Telephone, alternate: (213) 368-3765
Web site: http://www.synchrotech.com
(2)
(3)
Make a decision about the equipment used to do this procedure.
(a)
If the FlashTools equipment is to be used, go to Paragraph 3.D.(3).
(b)
If the OMNIDrive equipment is to be used, go to Paragraph 3.D.(4).
Do the instructions given below if the FlashTools equipment is used:
(a)
Put the PCMCIA card to be copied into the PCMCIA card drive.
(b)
Click on the FlashTools icon to start the FlashTools software.
NOTE:
(c)
15 Jun 2010
Revision 2, 3 Feb 2011
If more data is necessary on the operation of the FlashTools
software, use the HELP function on the FlashTools toolbar.
As necessary, use the HELP function on the FlashTools toolbar to install the
applicable drivers for the PCMCIA cards.
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SERVICE BULLETIN
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(d)
Make a file on the PC. Use the instructions given below:
1
Make a folder on the PC.
2
On the menu bar, make the selections as follows: FILE, NEW CARD,
AUTO DETECT.
3
Push the OK button.
4
Use the READ function on the toolbar.
5
Go to the folder that was made in Paragraph 3.D.(3)(d)1.
6
Put in the applicable file name identified in Table 8 and push the
SAVE button.
Table 8. PCMCIA File Name Data
Production Software
File Name
-232.01-232.01
232-232.BIN
-055.01
055.BIN
(e)
After the data has been put into the file, remove the PCMCIA card from the
PCMCIA card drive.
(f)
Put the other PCMCIA card into the PCMCIA card drive.
NOTE:
Make sure the write-protect tab on the PCMCIA card is in the
write-protect OFF position.
(g)
On the menu bar, make the selections as follows: FILE, NEW CARD, AUTO
DETECT.
(h)
Push the OK button.
(i)
On the menu bar, make the selection as follows: BLANK CHECK. If the
RESULTS window shows CARD IS BLANK, go to Paragraph 3.D.(3)(k). If not,
go to Paragraph 3.D.(3)(j) and erase the PCMCIA card.
(j)
Use the ERASE function on the toolbar. Push the YES button to erase all
of the data on the PCMCIA card.
(k)
Use the PROGRAM function on the toolbar.
(l)
Go to the file where the production software was put in Paragraph 3.D.(3)(d)6.
Use the OPEN function on the toolbar.
(m)
After the data has been put into the PCMCIA card, do the instructions
given below:
1
Use the VERIFY function on the toolbar.
2
Go to the file where the production software was put in Paragraph
3.D.(3)(d)6. Use the OPEN function on the toolbar.
3
Make sure the message CARD MATCHES FILE can be seen in the
RESULTS box.
(n)
Remove the PCMCIA card from the PCMCIA card drive.
(o)
Set the write-protect tab on the PCMCIA card to the write-protect ON position.
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SERVICE BULLETIN
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(p)
Identify the PCMCIA card with the applicable data given in Table 9.
Table 9. PCMCIA Card Identification
Production Software
(4)
PCMCIA Card
Identification
-232.01-232.01
EGPWS production
PCMCIA 232.01-232.01
-055.01
EGPWS production
PCMCIA 055.01
(q)
Stop the FlashTools software.
(r)
Go to Paragraph 3.D.(5).
Do the instructions given below if the OMNIDrive equipment is used.
(a)
Put the PCMCIA card to be copied into the OMNIDrive USB PC card
read-writer.
(b)
Start the PCM software.
(c)
Make a file on the PC. Use the instructions given below:
(d)
15 Jun 2010
Revision 2, 3 Feb 2011
1
On the menu bar, make the selections as follows: ACTIONS, COPY,
CARD TO FILE(S).
2
Push the NEW button in the COPY: CARD TO FILE(S) dialog box. In
the DEFINE COPY JOB dialog box, push the Browse button identified
by the symbol … for the target file location.
3
In the SAVE AS window, put in the applicable file name identified
in Table 8.
4
Push the SAVE button.
5
In the DEFINE COPY JOB dialog box, push the OK button.
6
Push the COPY button.
7
On the menu bar, make the selections as follows: ACTIONS,
COMPARE, to make sure the data is correct.
8
After the check of the data is done, remove the PCMCIA card from the
OMNIDrive USB PC card read-writer.
Put the other PCMCIA card into the OMNIDrive USB PC card read-writer.
Use the instructions given below:
1
Make sure the write-protect tab on the card is in the write-protect
OFF position.
2
Hold the card so the write-protect tab is on the right side of the
card as it is installed.
3
Put the card into the slot of the OMNIDrive USB PC card read-writer.
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(e)
Read the file that was made in Paragraph 3.D.(4)(c) and put the data into the
PCMCIA card. Use the instructions given below:
1
On the menu bar, make the selections as follows: ACTIONS, COPY,
FILE(S) TO CARD.
2
Push the NEW button in the COPY: FILE(S) TO CARD dialog box.
3
In the DEFINE COPY JOB dialog box, push the Browse button
identified by the symbol … for the source file location.
4
In the OPEN dialog box, go to the file that was made in Paragraph
3.D.(4)(c) and push the OPEN button.
NOTE:
5
In the DEFINE COPY JOB dialog box, push the OK button.
6
Make a selection of the two options identified below in the COPY:
FILE(S) TO CARD dialog box. Then push the COPY button.
• ERASE (LINEAR) FLASH BEFORE WRITE
•
7
(5)
E.
Make a selection of ALL FILES in the FILES OF TYPE
box to see the .BIN file.
WRITE WITH VERIFY.
Make sure there is a box with a checkmark before the source file
identified in the COPY JOBS window.
(f)
Remove the PCMCIA card from the OMNIDrive USB PC Card Read-Writer.
(g)
Set the write-protect tab on the PCMCIA card to the write-protect ON position.
(h)
Identify the PCMCIA card with the applicable data given in Table 9.
(i)
Stop the PCM software.
Make a decision about how to do the conversion of the MK V EGPWS.
(a)
If the conversion is to be done at a customer location (in the aircraft), go
to Paragraph 3.F.
(b)
If the conversion is to be done at a shop location without the EGPWS GSE, go
to Paragraph 3.G.
(c)
If the conversion is to be done at a shop location with the EGPWS GSE, go
to Paragraph 3.H.
CD-ROM Data
This paragraph gives the procedure to read the production software from a CD
ROM and write the data into a PCMCIA card.
NOTE:
(1)
The equipment identified below is necessary to do this procedure:
(a)
For MK V EGPWS, PN 965-0976-0XX, units:
1
(b)
For MK V EGPWS, PN 965-1690-05X units:
1
(c)
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Production software CD ROM, PN 718-1471-074 (-232.01-232.01).
Production software CD ROM, PN 718-1471-075 (-055.01).
A PCMCIA card identified in Table 6 or an equivalent.
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(d)
(2)
(3)
An IBM PC or an equivalent with a Pentium processor, 133 megahertz (MHz)
or higher, and the items identified below:
•
CD ROM drive
•
Windows 95/98/ME or Windows 2000/XP
•
One of the items identified below:
–
PCMCIA drive with FlashTools software for WINDOWS 95/98/ME,
PN 331-0054-001
–
PCMCIA drive with FlashTools software for WINDOWS 2000/XP,
PN 331-0054-002
–
CSM OMNIDrive USB LF PC card read-writer, OMNIDrive USB
professional interface cable, and OMNIDrive USB professional (PC
card manager) software. These OMNIDrive items are supplied
together if an order is made for the OMNIDrive part number given
in Table 7.
Make a decision about the equipment used to do this procedure.
(a)
If the FlashTools equipment is to be used, go to Paragraph 3.E.(3).
(b)
If the OMNIDrive equipment is to be used, go to Paragraph 3.E.(4).
Do the instructions given below if the FlashTools equipment is used:
(a)
Click on the FlashTools icon to start the FlashTools software.
NOTE:
If more data is necessary on the operation of the FlashTools
software, use the HELP function on the FlashTools toolbar.
(b)
As necessary, use the HELP function on the FlashTools toolbar to install the
applicable drivers for the PCMCIA cards.
(c)
Put the CD ROM into the PC CD ROM drive.
(d)
Put the other PCMCIA card into the PCMCIA card drive.
NOTE:
Make sure the write-protect tab on the PCMCIA card is in the
write-protect OFF position.
(e)
On the menu bar, make the selections as follows: FILE, NEW CARD, AUTO
DETECT.
(f)
Push the OK button.
(g)
On the menu bar, make the selection as follows: BLANK CHECK. If the
RESULTS window shows CARD IS BLANK, go to Paragraph 3.E.(3)(i). If not,
go to Paragraph 3.E.(3)(h) and erase the PCMCIA card.
(h)
Use the ERASE function on the toolbar. Push the YES button to erase all
of the data on the PCMCIA card.
(i)
Use the PROGRAM function on the toolbar.
(j)
Go to the applicable file on the CD ROM identified in Table 10 and use
the OPEN function on the toolbar.
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Table 10. CD ROM File Name Data
Production Software
File Name
-232.01-232.01
996-0125-587.BIN
-055.01
996-0125-587.BIN
(k)
(4)
After the data has been put into the PCMCIA card, do the instructions
given below:
1
Use the VERIFY function on the toolbar.
2
Go to the applicable file on the CD ROM identified in Table 10 and use
the OPEN function on the toolbar.
3
Make sure the message CARD MATCHES FILE can be seen in the
RESULTS box.
(l)
Remove the PCMCIA card from the PCMCIA card drive.
(m)
Set the write-protect tab on the PCMCIA card to the write-protect ON position.
(n)
Identify the PCMCIA card with the applicable data given in Table 9.
(o)
Remove the CD ROM from the PC CD ROM drive.
(p)
Stop the FlashTools software.
(q)
Go to Paragraph 3.E.(5).
Do the instructions given below if the OMNIDrive equipment is used:
(a)
Put the CD ROM into the PC CD ROM drive.
(b)
Start the PCM software.
(c)
Put the PCMCIA card into the OMNIDrive USB PC card read-writer. Use the
instructions given below:
(d)
1
Make sure the write-protect tab on the card is in the write-protect
OFF position.
2
Hold the card so the write-protect tab is on the right side of the
card as it is installed.
3
Put the card into the slot of the OMNIDrive USB PC card read-writer.
Read the file from the CD-ROM and put the data into the PCMCIA card.
Use the instructions given below:
1
On the menu bar, make the selections as follows: ACTIONS, COPY,
FILE(S) TO CARD.
2
Push the NEW button in the COPY: FILE(S) TO CARD dialog box.
3
In the DEFINE COPY JOB dialog box, push the Browse button
identified by the symbol … for the source file location.
4
In the OPEN dialog box, go to the file from the CD-ROM identified in
Table 10 and push the OPEN button.
NOTE:
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Revision 2, 3 Feb 2011
Make a selection of ALL FILES in the FILES OF TYPE
box to see the .BIN file.
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5
In the DEFINE COPY JOB dialog box, push the OK button.
6
Make a selection of the two options identified below in the COPY:
FILE(S) TO CARD dialog box. Then push the COPY button.
7
(5)
F.
•
ERASE (LINEAR) FLASH BEFORE WRITE
•
WRITE WITH VERIFY.
Make sure there is a box with a checkmark before the source file
identified in the COPY JOBS window.
(e)
Remove the PCMCIA card from the OMNIDrive USB PC card read-writer.
(f)
Set the write-protect tab on the PCMCIA card to the write-protect ON position.
(g)
Identify the PCMCIA card with the applicable data given in Table 9.
(h)
Remove the CD ROM from PC CD ROM drive.
(i)
Stop the PCM software.
Make a decision about how to do the conversion of the MK V EGPWS.
(a)
If the conversion is to be done at a customer location (in the aircraft), go
to Paragraph 3.F.
(b)
If the conversion is to be done at a shop location without the EGPWS GSE, go
to Paragraph 3.G.
(c)
If the conversion is to be done at a shop location with the EGPWS GSE, go
to Paragraph 3.H.
Modification at Customer Location (in the Aircraft)
The MK V EGPWS must identify that the aircraft is on the ground before the
production software can be installed.
NOTE:
(1)
No special equipment is necessary to do this procedure.
(2)
Make sure the power to the MK V EGPWS is on. Make sure the COMPUTER OK light
emitting diode (LED) on the MK V EGPWS front panel is on. Refer to Figure 1.
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Figure 1. (Sheet 1 of 1) Instruction Label Placement
(3)
Open the door on the MK V EGPWS front panel.
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(4)
Put the PCMCIA card into the PCMCIA card slot.
NOTE:
G.
Do not use the notes on the PCMCIA card that identify problems related
to the installation or removal while power is applied. The MK V EGPWS
automatically applies and removes power from the PCMCIA card.
(5)
While the production software is installed, make sure the IN PROG LED comes on
and the COMPUTER OK LED goes off.
(6)
After the production software is installed, make sure the XFER COMP LED comes on.
(7)
Remove the PCMCIA card from the MK V EGPWS.
(8)
After approximately 15 seconds, make sure the COMPUTER OK LED comes on. This
identifies that the production software was installed correctly.
(9)
Close the door on the MK V EGPWS front panel.
(10)
Go to Paragraph 3.I.
Modification at Shop Location Without EGPWS GSE
(1)
The equipment identified below is necessary to do this procedure:
NOTE:
•
A 600 ohms headphone with a connector that will fit the HEADPHONES connector
on the front panel of the MK V EGPWS.
•
For the MK V EGPWS, PN 965-0976-003-XXX-XXX, PN 965-0976-020-XXX-XXX,
PN 965-0976-060-XXX-XXX, and PN 965-1690-05X:
–
•
A 115 volts, alternating current (VAC), 400 hertz, single-phase power supply
with a minimum supply current of 2 amperes.
For the MK V EGPWS, PN 965-0976-040-XXX-XXX:
–
(2)
The characters XXX used in the part numbers in this paragraph are user
supplied.
A 28 VDC power supply with a minimum supply current of 2 amperes.
Make sure the power supply is off. Connect the power supply to the bottom rear
connector of the MK V EGPWS as identified in Table 11.
Table 11. Power Supply Connections
Pin
Pin 115 VAC Pin
Nomenclature
28 VDC Pin
Nomenclature
2
Power 115 VAC (H)
28 VDC (+)
3
Power 115 VAC (L)
28 VDC (-)
4
Chassis ground
(GND)
Chassis GND
(3)
Connect a wire between the top rear connector Pin 6D (Program Pin 17) and the
middle rear connector pin 3A (program pin common) of the MK V EGPWS.
(4)
Apply power to the power supply. Make sure the COMPUTER OK LED on the MK V
EGPWS front panel comes on after approximately 15 seconds. Refer to Figure 1.
(5)
Open the door on the MK V EGPWS front panel.
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(6)
Put the PCMCIA card into the PCMCIA card slot.
NOTE:
H.
Do not use the notes on the PCMCIA card that identify problems related
to the installation or removal while power is applied. The PCMCIA
automatically applies and removes power from the PCMCIA card.
(7)
While the production software is installed, make sure the IN PROG LED comes on
and the COMPUTER OK LED goes off.
(8)
After the production software is installed, make sure the XFER COMP LED comes on.
(9)
Remove the PCMCIA card from the MK V EGPWS.
(10)
After approximately 15 seconds, make sure the COMPUTER OK LED comes on. This
identifies that the production software was installed correctly.
(11)
Connect the 600 ohms headphone to the HEADPHONES connector on the front
panel of the MK V EGPWS.
(12)
Go to Paragraph 3.I.
Modification at Shop Location With EGPWS GSE
(1)
The equipment identified below is necessary to do this procedure:
•
UTS-2000 GSE, PN 951-0372-001, -010, -020, or -030.
NOTE:
This equipment is identified as the EGPWS GSE in this paragraph.
This equipment is identified in the SPECIAL TOOLS, FIXTURES, AND
EQUIPMENT section of the CMM.
(2)
Connect the MK V EGPWS to the EGPWS GSE. Refer to the instructions in the
TESTING AND TROUBLESHOOTING section of the CMM.
(3)
In the MK V EGPWS ATP program group, click two times on the EGPWS TERMINAL
icon (use COM 1).
NOTE:
(4)
This gets to the boot monitor in the MK V EGPWS. No data is seen until the
power is applied to the MK V EGPWS in Paragraph 3.H.(4). When power is
applied, data about the MK V EGPWS can be seen.
Use the discrete card control panel in the GSE CARDS program group to apply
power to the MK V EGPWS. Click two times on the PAC UNIVERSAL DISCRETE
CARD icon. Use the POWER/TTL from the small dialog box that comes into view.
When the control panel opens in the power control as TTL output section, click the
applicable button identified below:
The characters XXX used in the part numbers in this paragraph are user
supplied.
For the MK V EGPWS, PN 965-0976-003-XXX-XXX, PN 965-0976-020-XXX-XXX,
PN 965-0976-060-XXX-XXX, and PN 965-1690-05X: click the 115 VAC button.
NOTE:
•
•
For the MK V EGPWS, PN 965-0976-040-XXX-XXX: click the 28 VDC button.
(5)
Push the ALT and TAB keys at the same time as necessary to get to the MK V EGPWS
terminal. Look at the output of the MK V EGPWS on the display.
(6)
Push the CTRL and Z keys at the same time to get the prompt.
(7)
In this sequence push the P key, the S key then the ENTER key. Make sure the
message GPWS COMPUTER OK is seen on the display.
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(8)
Open the door on the MK V EGPWS front panel. Refer to Figure 1.
(9)
Put the PCMCIA card into the PCMCIA card slot.
Do not use the notes on the PCMCIA card that identify problems related
to the installation or removal while power is applied. The PCMCIA
automatically applies and removes power from the PCMCIA card.
NOTE:
I.
(10)
While the production software is installed, make sure the IN PROG LED comes on
and the COMPUTER OK LED goes off.
(11)
After the production software is installed, make sure the XFER COMP LED comes on.
(12)
Remove the PCMCIA card from the MK V EGPWS.
(13)
Make sure the COMPUTER OK LED on the MK V EGPWS front panel comes on
after approximately 15 seconds. This identifies that the production software was
installed correctly.
(14)
Push the CTRL and Z keys at the same time.
(15)
Push the P, S, and ENTER keys one after the other.
(16)
Make sure the production software data is correct.
(17)
Close the door on the MK V EGPWS front panel.
(18)
Go to Paragraph 3.J.
Production Software Check
A check of the production software is done with the ST function. The ST function
cannot be started if the MK V EGPWS does not identify that the aircraft is on
the ground.
NOTE:
(1)
The operation and characteristics of the ST function are given below.
(a)
The ST function may be started from the two possible locations.
1
The aircraft cockpit with the MK V EGPWS test switch.
NOTE:
2
(b)
Condition of the different inputs.
To help go through the different levels, there are two cancel functions:
• Short cancel (push and hold the ST button for more than 0.5 second
but less than 2 seconds).
•
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Revision 2, 3 Feb 2011
The ST button behind the front panel door of the MK V EGPWS.
The ST button is the means used to start the ST function from the aircraft
cockpit or the MK V EGPWS front panel. The EGPWS ST function has six
levels that identify the data given below:
• Condition and configuration of the MK V EGPWS
• Fault and warning history
•
(c)
Use of the cockpit ST function can be different from one
aircraft to another. For example, the ST function can be
started when the GPWS PULL-UP indicator is pushed or
when a separate ST switch is pushed.
Long cancel (push and hold the ST button more than 2 seconds but less
than 8 seconds).
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(2)
(d)
The short cancel and long cancel functions operate differently when the ST is
in different levels. To start the ST sequence, or to continue from one level to
another, use the short cancel. When the instruction "push the ST button" is
given in this paragraph, use the short cancel sequence.
(e)
The procedure given below moves the operator directly to the Level 3 ST
(system configuration). Most of the Level 1 and Level 2 STs are not done.
Push the ST button to start the Level 1 ST.
If a program pin parity error is identified, the ST will not work until the
aircraft configuration is correct.
NOTE:
(3)
After the Level 1 ST message starts, push the ST button. This cancels the Level 1
ST and starts the Level 2 ST.
(4)
After the Level 2 ST message starts (CURRENT FAULTS), push the ST button.
This cancels the Level 2 ST.
(5)
When the message PRESS TO CONTINUE is heard, push the ST button. This starts
the Level 3 ST (system configuration).
(6)
Make sure the applicable messages identified in Table 12 are heard.
Table 12. MK V EGPWS Messages
Serial
Number
Message
Application
Software
Version
Configuration
Software
Version
Remaining
Messages
965-0976-003-232-232 Ignore
Ignore
-232.01
-232.01
Ignore
965-0976-020-232-232 Ignore
Ignore
-232.01
-232.01
Ignore
965-0976-040-232-232 Ignore
Ignore
-232.01
-232.01
Ignore
965-0976-060-232-232 Ignore
Ignore
-232.01
-232.01
Ignore
965-1690-055
Ignore
-055.01
NA
Ignore
MK V EGPWS PN
NOTE:
1.
MOD Status
Message
1
Ignore
The message is the spoken words for the MK V EGPWS part number.
(7)
When the Level 3 ST is complete, the message PRESS TO CONTINUE comes on. If
the ST button is not pressed, the ST sequence stops.
(8)
If the conversion of the MK V EGPWS was done with the instructions in Paragraph
3.G., do the instructions given below:
(a)
Disconnect the 600 ohms headphone from the HEADPHONES connector on
the front panel of the MK V EGPWS.
(b)
Close the door on the MK V EGPWS front panel.
(c)
Remove power from the power supply.
(d)
Disconnect the power supply from the MK V EGPWS.
(e)
Disconnect the wire between the top rear connector and the middle rear
connector of the MK V EGPWS.
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J.
Modification Status Marking for MK V EGPWS PNs 965-0976-0XX
(1)
Get MOD kit, PN 011-4070-001, and complete the work below. Refer to Figure 1.
(a)
Examine the inside of the MK V EGPWS front panel assembly door. If there is
no instruction label, get a new instruction label, PN 402-6068-107, and install
it. Refer to Figure 1 for where to install the new instruction label.
(b)
(Optional) If a new instruction label is installed, use a permanent procedure to
identify the currently installed terrain database version.
NOTE:
(2)
The use of a blank label, PN 402-6105-001, is acceptable to
use if desired.
For old style front panel labels, do the work below. Refer to Figure 2.
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Figure 2. (Sheet 1 of 1) Old Style Label Application and Configuration Software Version Labels
(a)
Examine the TSO label, and if the characters CAA SPEC 14 are visible, install
a cover up label, PN 402-6068-103, over the characters CAA SPEC 14.
(b)
Get the new software label, PN 620-2050-002.
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(3)
(c)
Remove the application software label and configuration database label
from the front panel label. Refer to Table 3 for the instructions about what
to do with the used labels.
(d)
Install the new software label in approximately the same location as the labels
removed in Paragraph 3.J.(2)(c).
For new style front panel labels, do the work below. Refer to Figure 3.
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Figure 3. (Sheet 1 of 1) New Style Labels Placement for MK V EGPWS, PNs 965-0976-0XX
(a)
Remove the part number label located on the front panel. Refer to Table 3 for
the instructions about what to do with the used labels.
(b)
Install the applicable new part number label identified below.
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K.
•
For MK V EGPWS, PN 965-0976-003-232-232, use part number label,
PN 620-1907-193
•
For MK V EGPWS, PN 965-0976-020-232-232, use part number label,
PN 620-1907-194
•
For MK V EGPWS, PN 965-0976-040-232-232, use part number label,
PN 620-1907-195
•
For MK V EGPWS, PN 965-0976-060-232-232, use part number label,
PN 620-1907-196.
Modification Status Marking for MK V EGPWS PNs 965-1690-05X
(1)
Get MOD kit, PN 011-4070-002, and complete the work below.
(a)
Examine the inside of the MK V EGPWS front panel assembly door. If there is
no instruction label, get a new instruction label, PN 402-6068-107, and install
it. Refer to Figure 1 for where to install the new instruction label.
(b)
(Optional) If a new instruction label is installed, use a permanent procedure to
identify the currently installed terrain database version.
NOTE:
(2)
The use of a blank label, PN 402-6105-001, is acceptable to
use if desired.
For old style front panel labels, do the work below. Refer to Figure 4.
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Figure 4. (Sheet 1 of 1) Old Style Labels Placement for MK V EGPWS, PNs 965-1690-05X
(a)
Remove the part number label located on the front panel.
(b)
Install a new part number label, PN 620-1907-202.
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(3)
(c)
Examine the TSO label on the front panel and if the characters CAA SPEC 14
are visible, install a cover up label, PN 402-6068-103, over the characters
CAA SPEC 14.
(d)
Examine the software MOD status label. If any of the MOD status boxes are
marked, remove the label and replace it with a new label, PN 402-6091-001.
Refer to Table 3 for the instructions about what to do with the used labels.
For new style front panel labels, do the work below. Refer to Figure 5.
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Figure 5. (Sheet 1 of 1) New Style Labels Placement for MK V EGPWS, PNs 965-1690-05X
(a)
Remove the part number label located on the front panel.
(b)
Install the applicable new part number label, PN 620-1907-202.
(c)
Examine the software MOD status label. If any of the MOD status boxes are
marked, remove the label and replace it with a new label, PN 402-6091-001.
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L.
Testing
(1)
M.
If this conversion was done with the instructions in Paragraph 3.H. (at a shop location
with an EGPWS GSE), do a test of the MK V EGPWS. Refer to the instructions in the
TESTING AND TROUBLESHOOTING section of the CMM. Use the configuration
matrix diskette, PN 998-1955-655. Dash numbers higher than-655 are permitted
alternatives.
Verification
(1)
If a location other than a Honeywell service center did the conversion given in this
service bulletin:
(a)
Make sure that the data sent to Honeywell is accurate on the CSSR. Refer
to Paragraph 4.A.
(b)
Make sure that all serial numbers are accurate.
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4.
Appendix
A.
Appendix A, Customer Support Service Report
(1)
If the conversion given in this service bulletin is done at a location other than a
Honeywell service center, complete the CSSR.
LRU/SRU Model/Nomenclature:
MK V EGPWS
LRU/SRU PN
(Before conversion):
965-
LRU/SRU PN
(After conversion):
965-
LRU/SRU Serial Number:
Hardware/Software MOD Level
(Before conversion):
Hardware/Software MOD Level
(After conversion):
Aircraft Type, Serial Number, Tail Number:
End User
Company Name:
Company Address:
Service Provider
Person to Contact:
Company Name:
Company Address:
Company Phone Number:
Date of conversion:
Required Information Fields
Honeywell Internal Use Only
SAR Number:
QDS Customer Number:
Mail or Fax
Completed Form to:
Honeywell International Inc.
Aerospace Electronic Systems
Attn: Order Management
P.O. Box 21111
Phoenix, AZ 85036-1111
Fax: (602) 822-7272
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