# Boeing Alert Service Bulletin 777-34A0191: Revision 1

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- Document: [Boeing Alert Service Bulletin 777-34A0191](https://openairdocs.org/service-documents/boeing/777-34a0191.md)
- Title as filed: U.S. DOT/FAA - SB-777-34A0191-01
- Pages: 21
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## Text

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### Page 1

Commercial 
Airplanes
777
Service Bulletin
ALERT
Number: 777-34A0191
Original Issue: September 20, 2011
Revision 1: March 23, 2012
ATA System: 3433
SUBJECT: NAVIGATION - Radio Altimeter System - Radio Altimeter Transceiver Replacement
Export of this technology is controlled under the United States Export Administration Regulations (EAR) (15
CFR 730-774). An export license may be required before it is used for development, production or use by foreign
persons from specific countries. The controller of this data has the individual responsibility to abide by all export
laws.
9E991ECCN:
BOEING PROPRIETARY, CONFIDENTIAL, AND/OR TRADE SECRET
Copyright © 2011 The Boeing Company
Unpublished Work - All Rights Reserved
Boeing claims copyright in each page of this document only to the extent that the page contains copyrightable
subject matter. Boeing also claims copyright in this document as a compilation and/or collective work.
This document includes proprietary information owned by The Boeing Company and/or one or more third parties.
Treatment of the document and the information it contains is governed by contract with Boeing. For more
information, contact The Boeing Company, P.O. Box 3707, Seattle, Washington 98124.
Boeing, the Boeing signature, the Boeing symbol, 707, 717, 727, 737, 747, 757, 767, 777, 787, Dreamliner,
BBJ, DC-8, DC-9, DC-10, KC-10, KDC-10, MD-10, MD-11, MD-80, MD-88, MD-90, P-8A, Poseidon and the
Boeing livery are all trademarks owned by The Boeing Company; and no trademark license is granted in
connection with this document unless provided in writing by Boeing.
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Table of Contents
Revision Transmittal Sheet ............................................ 5
Summary ...................................................... 7
1. PLANNING INFORMATION ........................................ 1 1
A. Effectivity ............................................... 1 1
1. Airplanes ............................................ 1 1
2. Spares Affected ........................................ 1 2
B. Concurrent Requirements ...................................... 1 2
C. Reason ................................................ 1 2
D. Description .............................................. 1 3
E. Compliance .............................................. 1 3
F. Approval ............................................... 1 3
G. Manpower .............................................. 1 3
H. Weight and Balance Changes .................................... 1 4
I. Electrical Load Data ......................................... 1 4
J. References .............................................. 1 4
1. Existing Data .......................................... 1 4
2. Data supplied with this Service Bulletin ............................ 1 4
3. Installation Drawings Used in the Preparation of this Service Bulletin ............ 1 4
K. Publications Affected ........................................ 1 5
L. Interchangeability and Intermixability of Parts ........................... 1 5
2. MATERIAL INFORMATION ........................................ 1 7
A. Material - Price and Availability ................................... 1 7
B. Industry Support Information .................................... 1 7
C. Parts Necessary For Each Airplane ................................. 1 7
1. Kits/Parts ............................................ 1 7
2. Parts and Materials Supplied by the Operator ........................ 1 7
3. Parts Modified and Reidentified ................................ 1 7
4. Parts Removed and Not Replaced .............................. 1 7
D. Parts Necessary to Change Spares ................................. 1 7
E. Special Tooling - Price and Availability ............................... 1 8
F. Special Tooling Necessary to do this Service Bulletin ....................... 1 8
3. ACCOMPLISHMENT INSTRUCTIONS .................................. 1 9
A. GENERAL INFORMATION ..................................... 1 9
B. WORK INSTRUCTIONS ....................................... 1 9
FIGURE 1: RADIO ALTIMETER TRANSCEIVER REPLACEMENT ................... 2 0
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777-34A0191Revision 1: March 23, 2012
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Commercial 
Airplanes
777
Service Bulletin
ALERT
Revision Transmittal SheetNumber: 777-34A0191Original Issue: September 20, 2011
Revision 1: March 23, 2012
ATA System: 3433
SUBJECT: NAVIGATION - Radio Altimeter System - Radio Altimeter Transceiver Replacement
This revision includes all pages of the service bulletin.
COMPLIANCE INFORMATION RELATED TO THIS REVISION
No more work is necessary on the airplanes changed in accordance with the original issue of this service bulletin.
REASON FOR REVISION
This revision is sent to add one airplane to the effectivity list of the original issue of this service bulletin.
These sections were changed:
1. In PLANNING INFORMATION, Paragraph 1.A.1., airplane WE091 was added to the effectivities.
Vertical lines are put on the left edge of each page, except in Paragraph 1.A., Effectivity, to show the location
of important changes.
Pages with no vertical lines have no important changes.
REVISION HISTORY
September 20, 2011Original Issue:
March 23, 2012Revision 1:
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Commercial 
Airplanes
777
Service Bulletin
ALERT
SummaryNumber: 777-34A0191Original Issue: September 20, 2011
Revision 1: March 23, 2012
ATA System: 3433
SUBJECT: NAVIGATION - Radio Altimeter System - Radio Altimeter Transceiver Replacement
THIS BULLETIN IS SENT TO THE OPERATORS OF RECORD OF THE AIRPLANES SHOWN IN PARAGRAPH
1.A., EFFECTIVITY. IF AN AIRPLANE HAS BEEN LEASED OR SOLD, SEND THIS SERVICE BULLETIN TO
THE NEW OPERATOR. IF APPLICABLE SPARES HAVE BEEN SOLD, SEND THIS SERVICE BULLETIN TO
THE NEW OWNER.
CONCURRENT REQUIREMENTS
None.
BACKGROUND
This service bulletin gives instructions to replace the existing Radio Altimeter (RA) Transceivers with the upgraded
units. The upgraded Radio Altimeter Transceivers have improved antenna monitoring capabilities for detecting
antenna deterioration caused by the environmental conditions or damage to the antenna during antenna alteration
which can result in breaks in the coaxial cables or damage to the coax connector. If the changes in this service
bulletin are not done, incorrect Radio Altimeter output may be observed on the Primary Flight Displays (PFD).
Some operators have reported inconsistent Radio Altimeter Transceiver outputs during the flight and on the
ground. The antenna alteration at the antenna level can create micro cracks on the electrical grounding connection,
damage the coax cables or the coax connector center pin contact. Any one of these damages to the antenna
assembly can affect the Radio Altimeter system functionality.
Boeing Service Related Problem 777-SRP-34-0120 is related to this service bulletin.
Boeing Fleet Team Digest 777 FTD 34-10013 is related to this service bulletin.
This table is provided to operators for planning purposes only. Refer to the applicable sections for more
information.
ReferenceAffectedPlanning Data
Paragraph 1.A.2., Spares AffectedYesSpares Affected
Paragraph 1.E., ComplianceNoAD Related
Paragraph 1.H., Weight and Balance ChangesNoWeight and Balance Change
Paragraph 1.I., Electrical Load DataNoElectrical Load Changed
Paragraph 1.K., Publications AffectedYesPublications Affected
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ReferenceAffectedPlanning Data
Paragraph 1.K., Publications AffectedNoAirplane Flight Operations Affected (Flight Crew
Operations Manual and/or FAA Approved Air-
plane Flight Manual)
Paragraph 2.C.1., Kits/PartsNoKits/Parts Required
Paragraph 2.C.2., Parts and Materials Supplied
by the Operator
YesOperator Supplied Material
Paragraph 2.F., Special Tooling Necessary to
do this Service Bulletin
NoSpecial Tooling Required
ACTION (PRR 62777-85S)
1. Gain access to the E5 rack in the forward cargo compartment.
2. Replace the Radio Altimeter (RA) Transceivers.
3. Do Installation Test.
EFFECTIVITY
777-200, 777-200LR, 777-300, 777-300ER, and 777F Airplane(s). Refer to Paragraph 1.A.1., Airplanes, for the
list of affected airplane(s).
COMPLIANCE
Boeing recommends that the changes given in this service bulletin be done within 24 months after the original
issue date of this service bulletin.
INDUSTRY SUPPORT INFORMATION
Boeing warranty remedies are not available for the configuration changes given in this service bulletin.
MANPOWER
Elapsed HoursTotal Task HoursAirplanes
1.651.65All
MATERIAL INFORMATION
Operator Supplied Parts/Materials.
Refer to Paragraph 2.A., Material - Price and Availability.
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BOEING SERVICE BULLETIN 777-34A0191
ALERT  ALERT
E5 RACK (FORWARD
CARGO COMPARTMENT)
REPLACE RADIO ALTIMETER (RA)
E  TRANSCEIVERS (XCVR)
RIGHT RA XCVR (E5-2)
CENTER RA XCVR (E5-3)
LEFT RA XCVR (E5-4) ^
FWD
ELECTRONIC EQUIPMENT RACK, E5-  2095348
FORWARD CARGO COMPARTMENT
Original Issue: September 20, 2011
Revision 1: March 23, 2012  777-34A0191
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Commercial 
Airplanes
777
Service Bulletin
ALERT
Number: 777-34A0191
Original Issue: September 20, 2011
Revision 1: March 23, 2012
ATA System: 3433
SUBJECT: NAVIGATION - Radio Altimeter System - Radio Altimeter Transceiver Replacement
THIS BULLETIN IS SENT TO THE OPERATORS OF RECORD OF THE AIRPLANES SHOWN IN PARAGRAPH
1.A., EFFECTIVITY. IF AN AIRPLANE HAS BEEN LEASED OR SOLD, SEND THIS SERVICE BULLETIN TO
THE NEW OPERATOR. IF APPLICABLE SPARES HAVE BEEN SOLD, SEND THIS SERVICE BULLETIN TO
THE NEW OWNER.
1.    PLANNING INFORMATION
A. Effectivity
1. Airplanes
This service bulletin is for the airplane(s) shown below. Refer to PRR 62777-85S for data about
this change.
Refer to Service Bulletin Index D624W001 Part 3 for Airplane Variable Number, Line Number, and
Serial Number data.
DESCRIPTIONCONFIGURATIONGROUP
Replace existing Radio Altimeter Transceivers with 9599-607-19996
part number
-1
Airplane Models:
777-200, 777-200LR, 777-300, 777-300ER, 777F
GroupVariable Number
1WA196 - WA198
1WB101 - WB106
1WB161 - WB177
1WB306 - WB307
1WB631 - WB638
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GroupVariable Number
1WB646 - WB649
1WC111 - WC120
1WC581
1WD046 - WD055
1WD581 - WD599
1WD606 - WD609
1WD621 - WD632
1WD671 - WD677
1WD846 - WD862
1WD921 - WD922
1WE091
1WF031 - WF032
1WF131
2. Spares Affected
Examine your spares supply for the parts or components identified in Paragraph 2.C., Parts
Necessary for Each Airplane. If any parts or components are found, refer to Paragraph 2.C. for
the recommended use.
B. Concurrent Requirements
None.
C. Reason
This service bulletin gives instructions to replace the existing Radio Altimeter (RA) Transceivers with
the upgraded units. The upgraded Radio Altimeter Transceivers have improved antenna monitoring
capabilities for detecting antenna deterioration caused by the environmental conditions or damage to
the antenna during antenna alteration which can result in breaks in the coaxial cables or damage to
the coax connector. If the changes in this service bulletin are not done, incorrect Radio Altimeter output
may be observed on the Primary Flight Displays (PFD).
Some operators have reported inconsistent Radio Altimeter Transceiver outputs during the flight and
on the ground. The antenna alteration at the antenna level can create micro cracks on the electrical
grounding connection, damage the coax cables or the coax connector center pin contact. Any one of
these damages to the antenna assembly can affect the Radio Altimeter system functionality.
Boeing Service Related Problem 777-SRP-34-0120 is related to this service bulletin.
Boeing Fleet Team Digest 777 FTD 34-10013 is relate to this service bulletin.
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Original Issue: September 20, 2011
777-34A0191Revision 1: March 23, 2012
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Revision 1 is sent to add WE091 to the effectivity list of the airplanes in the original issue of this service
bulletin.
D. Description
1. Gain access to the E5 rack in the forward cargo compartment.
2. Replace the Radio Altimeter (RA) Transceivers.
3. Do Installation Test.
Revision 1 - No more work is necessary on airplanes changed in accordance with the original issue of
this service bulletin.
The work in this service bulletin is done in the maintenance zone(s) given below.
Affected Maintenance Zones
ZoneModel
122, 211, 212777-200, 777-200LR, 777-300,
777-300ER, 777F
E. Compliance
Boeing recommends that the changes given in this service bulletin be done within 24 months after the
original issue date of this service bulletin.
F. Approval
This service bulletin was examined by the Federal Aviation Administration (FAA). The changes specified
in this service bulletin comply with the applicable regulations and are FAA approved, as well as European
Aviation Safety Agency (EASA)/Joint Aviation Authorities (JAA) approved for all EASA/JAA approved
airplanes listed in the service bulletin effectivity. This service bulletin and its approval were based on
the airplane in its original Boeing delivery configuration or as modified by other approved Boeing
changes.
If an airplane has a non-Boeing modification or repair that affects a component or system also affected
by this service bulletin, the operator is responsible for obtaining appropriate regulatory agency approval
before incorporating this service bulletin.
G. Manpower
The table below shows an estimate of the task hours necessary to do this change for each airplane.
This estimate is for direct labor only, done by an experienced crew. Adjust the estimate with operator
task hour data if necessary. The estimate does not include lost time. These are some examples of lost
time:
 Time to adjust to the workplace
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 Time to schedule the work
 Time to inspect the work
 Time to cure the materials
 Time to make the parts
 Time to find the tools.
Elapsed HoursTask HoursNumber of PersonsTask
0.250.251Open Access
0.900.901Figure 1
0.250.251RA Installation tests
0.250.251Close Access
1.651.65TOTAL FOR EACH AIRPLANE
H. Weight and Balance Changes
None.
I. Electrical Load Data
Not changed.
J. References
1. Existing Data
a. Engineering Change Memo PRR 62777-85S
b. Service Related Problem (SRP) 777-SRP-34-0120
c. Fleet Team Digest (FTD) 777 FTD 34-10013
d. 777 Maintenance Manual (AMM) Subject 777 AMM 34-33-01
e. THALES SB ERT-550-34-04
2. Data supplied with this Service Bulletin
None.
3. Installation Drawings Used in the Preparation of this Service Bulletin
TitleDrawing Number
EQUIPMENT INSTL - E5 RACK284W1205
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The table above lists applicable drawings used to prepare this service bulletin. The drawings are
not necessary to make the specified changes, and are not supplied with this service bulletin. The
drawings may not be applicable to all airplane configurations or operators.
K. Publications Affected
1. Publications:
Chapter-SectionPublication
34-33777 Aircraft Maintenance Manual
EQUIPMENT LIST777 Wiring Diagram Manual
34-33, 25-17777 Illustrated Parts Catalog
34-32Component Maintenance Manual
2. Damage Tolerance Based Structural Inspections:
Boeing has evaluated the repairs and/or changes in this service bulletin for effects on Fatigue
Critical Structure (FCS) and for changes to Damage Tolerance Inspections (DTI) required in the
Maintenance Program. This service bulletin does not affect FCS, therefore DTIs are not necessary.
L. Interchangeability and Intermixability of Parts
Accomplishment of this service bulletin does not affect interchangeability or intermixability of parts.
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2.    MATERIAL INFORMATION
A. Material - Price and Availability
The operator can supply the parts and materials shown in Paragraph 2.C., Parts Necessary for Each
Airplane . Refer to THALES SB ERT-550-34-04 for price and upgrade kit availability.
B. Industry Support Information
Boeing warranty remedies are not available for the configuration changes given in this service bulletin.
C. Parts Necessary For Each Airplane
1. Kits/Parts
None.
2. Parts and Materials Supplied by the Operator
NotesExisting Part NumberNameQTYPart Number /
Specification
(a) (b) (c)9599-607-19991 or 9599-
607-19992 or 9599-607-
19993
Radio Altimeter Transceiver39599-607-19996
(a) The existing/installed Radio Altimeter Transceivers have one of the part numbers mentioned in the
"Existing Part Number" column.
(b) You can use the existing Radio Altimeter Transceivers to upgrade to 9599-607-19996 part number.
Refer to THALES SB ERT-550-34-04 for the information on how to upgrade the existing Radio Altimeter
Transceivers to 9599-607-19996 part number.
(c) 9599-607-19991 and 9599-607-19992 units must first be converted to 9599-607-19993 part number
before they can be upgraded to 9599-607-19996 part number. Refer to the "Concurrent Requirements"
section of THALES SB ERT-550-34-04 for this information.
3. Parts Modified and Reidentified
None.
4. Parts Removed and Not Replaced
None
D. Parts Necessary to Change Spares
To get the parts shown below, refer to Paragraph 2.A., Material - Price and Availability.
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QTYNamePart Number
-Radio Altimeter
Transceiver
9599-607-19996
(a)
(a) Refer to THALES SB ERT-550-34-04 for the
information on how to upgrade the existing
RAs to 9599-607-19996 part number.
E. Special Tooling - Price and Availability
None.
F. Special Tooling Necessary to do this Service Bulletin
No special tools or equipment are necessary to do the change in this service bulletin. But, maintenance
and overhaul tools in the manuals given in Paragraph 1.J., References, can be necessary. Examine
operator tool supply to make sure all necessary tools are available.
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3.    ACCOMPLISHMENT INSTRUCTIONS
A. GENERAL INFORMATION
CAUTION: KEEP THE WORK AREA, WIRES AND ELECTRICAL BUNDLES CLEAN OF METAL
PARTICLES OR CONTAMINATION WHEN YOU USE TOOLS. UNWANTED MATERIAL,
METAL PARTICLES OR CONTAMINATION CAUGHT IN WIRE BUNDLES CAN CAUSE
DAMAGE TO THE BUNDLES. DAMAGED WIRE BUNDLES CAN CAUSE SPARKS OR
OTHER ELECTRICAL DAMAGE.
NOTE: 1. Manual titles are referred to by acronyms. Refer to Paragraph 1.J., References, for
definition of the acronyms.
2. Obey all of the warnings and cautions given in the specified manual sections.
3. These work instructions refer to procedures included in other Boeing documents.
When the words "refer to" are used and the operator has an accepted alternative
procedure, the accepted alternative procedure can be used. When the words "in
accordance with" are included in the instruction, the procedure in the Boeing document
must be used.
B. WORK INSTRUCTIONS
1. Get access to Electronic Equipment Rack E5 in the Forward Cargo Compartment.
2. Replace the Radio Altimeter (RA) Transceivers in accordance with FIGURE 1.
3. Do installation test. Refer to 777 AMM 34-33-01 as an accepted procedure.
4. Put the airplane back to a serviceable condition.
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BOEING SERVICE BULLETIN 777-34A0191
ALERT  ALERT
CARGO COMPARTMENT)  E5 RACK (FORWARD
RIGHT RA XCVR (E5-2)
CENTER RA XCVR (E5-3)
LEFT RA XCVR (E5-4)
FWD
ELECTRONIC EQUIPMENT RACK, E5-  2095352
FORWARD CARGO COMPARTMENT
FIGURE 1: RADIO ALTIMETER TRANSCEIVER REPLACEMENT
(SHEET 1 OF 2)
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The step numbers shown below agree with the numbers shown in the circle symbols in the figure. The QTY
numbers shown below are the number of parts necessary for this figure.
More DataQtyIdentificationNameTaskStep
(a)39599-607-19991 OR
9599-607-19992 OR
9599-607-19993
RADIO ALTIMETER
TRANSCEIVER
Remove1
(b)39599-607-19996RADIO ALTIMETER
TRANSCEIVER
Install (Changed)2
(a) Refer to 777 AMM 34-33-01 as an accepted procedure. The existing/installed Radio Altimeter Transceivers
have one of the following 9599-607-19991, 9599-607-19992 or 9599-607-19993 part numbers.
(b) Refer to 777 AMM 34-33-01 as an accepted procedure.
FIGURE 1: RADIO ALTIMETER TRANSCEIVER REPLACEMENT
(SHEET 2 OF 2)
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