Text
From the PDF’s text layer: layout, tables and figures are lost. The PDF is the document.
Query with SQL
duckdb -csv -c "SELECT p.page, p.text_source, p.text, f.rights_holder, f.license FROM 'https://openairdocs.org/data/latest/service_document_file_page.parquet' p JOIN 'https://openairdocs.org/data/latest/service_document_file.parquet' f USING (file_sha256) WHERE p.file_sha256 = '2bbf98ff1ba71b346fb43b953444548ee3967d4ce77c3e5f4cdaa049a7ee913a' ORDER BY p.page"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT p.page, p.text_source, p.text, f.rights_holder, f.license FROM 'https://openairdocs.org/data/latest/service_document_file_page.parquet' p JOIN 'https://openairdocs.org/data/latest/service_document_file.parquet' f USING (file_sha256) WHERE p.file_sha256 = '2bbf98ff1ba71b346fb43b953444548ee3967d4ce77c3e5f4cdaa049a7ee913a' ORDER BY p.page
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
Commercial Airplane Group 767 Service Bulletin Number: 767-31-0100 Revision Transmittal SheetDate: August 20, 1998 Revision 2: July 29, 1999 ATA System: 3141 SUBJECT: INDICATING/RECORDING SYSTEMS - Central Computers - Engine Indication And Crew Alerting System - EICAS Computer Replacement And Wire Change - Pratt and Whitney 4000 Engines This revision includes all pages of the service bulletin.
COMPLIANCE INFORMATION RELATED TO THIS REVISION Federal Aviation Administration (FAA) Airworthiness Directive (AD) 96-07-09, paragraph (d)(2) is related to this service bulletin.
No more work is necessary on airplanes changed as shown in the initial release or in Revision 1 of this service bulletin. Changes were made to the OPC software part numbers and Diskette Set part numbers in Appendix A. In addition, wire removal instructions were clarified and a maintenance manual reference was added on page 16.
REASON FOR REVISION This revision is sent to make changes to the EICAS functional test and to Appendix A.
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 Original Release: August 20, 1998 Revision 1: February 4, 1999 Revision 2: July 29, 1999 767-31-0100 Revision Transmittal Page 1 of 1
No text on this page: it may be a figure. Open the PDF to see it.
Commercial Airplane Group 767 Service Bulletin Number: 767-31-0100 SummaryDate: August 20, 1998 Revision 2: July 29, 1999 ATA System: 3141 SUBJECT: INDICATING/RECORDING SYSTEMS - Central Computers - Engine Indication And Crew Alerting System - EICAS Computer Replacement And Wire Change - Pratt and Whitney 4000 Engines
CONCURRENT REQUIREMENTS None
BACKGROUND This service bulletin gives instructions to replace the two Engine Indication and Crew Alerting System (EICAS) computers. The new computers allow loadable Operational Program Software (OPS) and Operational Program Configuration (OPC) software installation via a portable data loader (PDL) or an airborne data loader (ADL).
The new EICAS computers allow the use of OPC software to change the configuration of options selected by the customer. Loadable OPC software eliminates the requirement to change program pin wiring to make customer options.
The new EICAS computers have increased capacity, support optional Future Air Navigation System (FANS) features, comply with Amendment No. 121-266 [Docket No. 28109], "Revisions to Digital Flight Data Recorder Rules", and in combination with the appropriate Airplane Flight Manual (AFM) revision to Section 3.2, in accordance with Airworthiness Directive (AD) 96-07-09 paragraph (d)(2), will provide terminating action for the fuel filter bypass AD 96-07-09.
The related Rockwell/Collins Service Bulletins are EAP-701D-31-AR or EAP-701G-31-AV.
Boeing Service Letter 767-SL-31-036 is related to this service bulletin.
ACTION (PRR B12710) In the E8 rack, replace the left and right EICAS computers. Make wire changes in the E8 shelf.
Change left and right EICAS computer connector keying on the E-8 shelf. Load OPC software into both left and right EICAS computers. Do an operational test of the EICAS computers.
EFFECTIVITY All 767 airplanes line positions 1 - 695 with PW4000 Full Authority Digital Electronic Engine Control (FADEC) engines.
The effectivity is broken up into four major groups for convenience of wire changes.
COMPLIANCE Federal Aviation Administration (FAA) Airworthiness Directive 96-07-09, Amendment 39-9558, is related to this service bulletin.
INDUSTRY SUPPORT INFORMATION Boeing warranty remedies are not available for the configuration changes given in this service bulletin.
MANPOWER Total Man-hours Elapsed Time
14.0 7.0 The change to the EICAS computers as given in the Rockwell/Collins service bulletins are not included.
MATERIAL INFORMATION Operator Supplied Parts 767-31-0100 Summary Page 1 of 2
BOEING SERVICE BULLETIN 767-31-0100
REPLACE LEFT AND RIGHT EICAS COMPUTERS IN E8 RACK FWD
MAIN EQUIPMENT CENTER
EICAS SHELF WIRES
MAKE CHANGES TO S51692 August 20, 1998 767-31-0100 Revision 2: July 29, 1999 Summary Page 2 of 2
Commercial Airplane Group 767 Service Bulletin Number: 767-31-0100 Date: August 20, 1998 Revision 2: July 29, 1999 ATA System: 3141 SUBJECT: INDICATING/RECORDING SYSTEMS - Central Computers - Engine Indication And Crew Alerting System - EICAS Computer Replacement And Wire Change - Pratt and Whitney 4000 Engines
1. PLANNING INFORMATION A. Effectivity
1. Airplanes Refer to Service Bulletin Index Document D624T001, Part 3 for Airplane Variable Number, Line Number, and Serial Number data.
This service bulletin is for the airplanes shown below. An equivalent change is on subsequent production airplanes. Refer to PRR B12710 for data about this change.
IDENTIFICATION BY CUSTOMER, CUSTOMER CODE, GROUP AND VARIABLE NUMBER
AEROFLOT (ARO) 3 VN561-VN562
AEROMEXICO (AMX) 3 VF091 VF093 VN556
AIR CANADA (ACN) 3 VN931-VN936
AIR CHINA (BEJ) 1 VE085 2 VE086 3 VK161-VK164
AIR EUROPE ITALY (EIY) 3 VL931-VL932 VN682 4 VN972
AIR FRANCE (AFA) 3 VN631-VN633
AIR MADAGASCAR (MAD) 3 VN376
AIR NAMIBIA (NAM) 3 VN385
AIR ZIMBABWE (ZMB) 3 VF061-VF062 August 20, 1998 767-31-0100 Revision 2: July 29, 1999 Page 1 of 33
BOEING SERVICE BULLETIN 767-31-0100
AVIANCA (AVI) 3 VE171-VE172 VF092 VN152
CONDOR (CDF) 3 VN683-VN691
DELTA AIR LINES (DAL) 3 VK055-VK056 VN251-VN276 VS066-VS068
EGYPTAIR (EGP) 3 VN211-VN212
EL AL ISRAEL AIRLINES (ELA) 3 VF101-VF102
ETHIOPIAN AIRLINES (ETH) 3 VN371
LAM (LAM) 3 VF162
LANCHILE AIRLINES (LAN) 3 VN531 VN557 4 VN966-VN967 VN971
LAUDA AIR (LAL) 3 VN242-VN243 VN388 LAUDA AIR S.P.A. (LDI) 1 VL011 3 VN671
LTU (LTU) 4 VN171-VN174 VN381
MARTINAIR HOLLAND (MTH) 3 VN221-VN225 VN672
ROYAL BRUNEI AIRLINES (RBA) 3 VN372 VN382-VN384 VN386-VN387
SAS (SAS) 3 VF071 VN151 VN153-VN158 VN163-VN168 VN536 VN551
SHANGHAI AIRLINES (SHA) 3 VK171 VR421
SPANAIR (SPP) 3 VN541-VN542
TRANSBRASIL (TBL) 3 VF072 VF161 VN532
TWA (TWA) 3 VN537 VN681 VS206-VS207
UNITED AIRLINES (UAL) 3 VN491-VN513 August 20, 1998 767-31-0100 Revision 2: July 29, 1999 2
BOEING SERVICE BULLETIN 767-31-0100
UZBEKISTAN AIRWAYS (UZB) 4 VL806-VL807
IDENTIFICATION BY VARIABLE NUMBER GROUP 1 VE085 VL011 GROUP 2 VE086 GROUP 3 VE171-VE172 VF061-VF062 VF071-VF072 VF091-VF093 VF101-VF102 VF161-VF162 VK055-VK056 VK161-VK164 VK171 VL931-VL932 VN151-VN158 VN163-VN168 VN211-VN212 VN221-VN225 VN242-VN243 VN251-VN276 VN371-VN372 VN376 VN382-VN388 VN491-VN513 VN531-VN532 VN536-VN537 VN541-VN542 VN551 VN556-VN557 VN561-VN562 VN631-VN633 VN671-VN672 VN681-VN691 VN931-VN936 VR421 VS066-VS068 VS206-VS207 GROUP 4 VL806-VL807 VN171-VN174 VN381 VN966-VN967 VN971-VN972
2. Spares Examine your spares supply for the parts identified in Paragraph 2.E., Existing Parts Accountability. If any parts are found, refer to Paragraph 2.E., Existing Parts Accountability, for the recommended use.
August 20, 1998 767-31-0100 Revision 2: July 29, 1999 3
BOEING SERVICE BULLETIN 767-31-0100 B. Concurrent Requirements None C. Reason This service bulletin gives instructions to replace the two Engine Indication and Crew Alerting System (EICAS) computers. The new computers allow loadable Operational Program Software (OPS) and Operational Program Configuration (OPC) software installation via a portable data loader (PDL) or an airborne data loader (ADL).
The new EICAS computers allow the use of OPC software to change the configuration of options selected by the customer. Loadable OPC software eliminates the requirement to change program pin wiring to make customer options.
The new EICAS computers have increased capacity, support optional Future Air Navigation System (FANS) features, comply with Amendment No. 121-266 [Docket No. 28109], "Revisions to Digital Flight Data Recorder Rules", and in combination with the appropriate Airplane Flight Manual (AFM) revision to Section 3.2, in accordance with Airworthiness Directive (AD) 96-07-09 paragraph (d)(2), will provide terminating action for the fuel filter bypass AD 96-07-09.
The related Rockwell/Collins Service Bulletins are EAP-701D-31-AR or EAP-701G-31-AV.
Boeing Service Letter 767-SL-31-036 is related to this service bulletin.
Revision 1 is sent to make changes to the EICAS functional test, the Parts Necessary for Each Airplane section 2.C. and in Appendix A.
Revision 2 is sent to make changes to the EICAS functional test and to Appendix A.
D. Description In the E8 rack, replace the left and right EICAS computers. Make wire changes in the E8 shelf.
Change left and right EICAS computer connector keying on the E-8 shelf. Load OPC software into both left and right EICAS computers. Do an operational test of the EICAS computers.
NOTE: Some service bulletins with EICAS program pin changes are not usable after this change is done. Operators must contact Boeing for the OPC diskette that accomplishes the equivalent of those program pin changes.
The changes in this service bulletin will change the Engine Indication and Crew Alerting System (EICAS).
Revision 1 - No more work is necessary on airplanes changed as shown in the initial release of this service bulletin. Changes were made to the Parts Necessary for Each Airplane section 2.C., OPC and software part numbers in Appendix A and the EICAS functional test were changed with the addition of two new steps on page 14 and to show the correct circuit breaker name, location and numbers on pages 12, 13 and 14.
Revision 2 - No more work is necessary on airplanes changed as shown in the initial release or in Revision 1 of this service bulletin. Changes were made to the OPC software part numbers and Diskette Set part numbers in Appendix A. In addition, wire removal instructions were clarified and a maintenance manual reference was added on page 16.
An evaluation form is attached to this service bulletin. Please use this form to tell us what you think of the quality of this service bulletin.
August 20, 1998 767-31-0100 Revision 2: July 29, 1999 4
BOEING SERVICE BULLETIN 767-31-0100 E. Compliance Federal Aviation Administration (FAA) Airworthiness Directive 96-07-09, Amendment 39-9558, is related to 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 Federal Aviation Regulations (FAR) and are FAA approved. This service bulletin and the FAA approval were based on the airplane in its original Boeing delivery configuration or as modified by other FAA 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.
The FAA has examined the configuration changes specified in this service bulletin. The FAA has approved the configuration change as a method of compliance to those specified in paragraph (d), (1) of AD 96-07-09, Amendment 39-9558.
G. Manpower The table below shows an estimate of the man-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 man-hour data if necessary. The estimate does not include lost time. These are some examples of lost time:
- Time to adjust to the workplace
- Time to schedule the work
- Time to examine the work
- Time to cure the materials
- Time to make the parts
- Time to find the tools.
Task Number of Persons Man-Hours Elapsed Time (Hours) Open Access 2 1.5 0.75 Change 1-2 8.0 4.00 Close Access 2 1.5 0.75 Test 2 3.0 1.50 TOTAL FOR EACH AIRPLANE 14.0 7.00 The change to the EICAS computers as given in Collins Service Bulletins EAP-701D-31-AR and EAP-701G-31-AV are not included.
August 20, 1998 767-31-0100 Revision 2: July 29, 1999 5
BOEING SERVICE BULLETIN 767-31-0100 H. Weight and Balance Changes Airplane Group and Model Change in Weight (Pounds) Change in Moment (Pound-Inches) Group 1 -200 airplanes -6.4 -1,638.4 -300 airplanes -6.4 -864.0 Group 2 -200 airplanes -6.4 -1,638.4 Group 3 -200 airplanes -6.4 -1,638.4 -300 airplanes -6.4 -864.0 Group 4 -200 airplanes -6.4 -864.0 I. Electrical Load Data Not changed J. References
1. Existing Data:
a. Engineering Change Memo PRR B12710
b. 767 Maintenance Manual (AMM) Subjects 20-41-01, 24-22-00, 31-41-02, 31-41-02/201
c. 767 Wiring Diagrams 31-41-15, 31-41-18, 31-51-33
d. Boeing Standard Wiring Practices Manual (BSWPM) 20-10-11, 20-10-12, 20-10-14, 20-10-19, 20-30-11, 20-71-14, 20-90-11
e. Collins Service Bulletins EAP-701D-31-AR, EAP-701G-31-AV*
f. Boeing Service Letter 767-SL-31-036 Rev A, dated August 21, 1998.
g. FAA Airworthiness Directive 96-07-09, Amendment 39-9558
h. Amendment No. 121-266 [Docket No. 28109], Revisions to Digital Flight Data Recorder Rules * The supplier was told to send copies of the service bulletin to each operator.
2. Data supplied with this service bulletin:
None
3. Installation Drawings:
None August 20, 1998 767-31-0100 Revision 2: July 29, 1999 6
BOEING SERVICE BULLETIN 767-31-0100 K. Publications Changed Publication Chapter-Section 767 FAA Approved Airplane Flight Manual * 767 Operations Manual Chapter 21 767 Maintenance Manual 23-21, 23-42, 23-43, 23-46, 31-41, 32-61 767 Fault Isolation Manual 31-41, 71-20 767 Ramp Maintenance Manual 31-03, 31-04, 31-05 Overhaul Manual 3, 4, 9, 21, 22 (Old Format) QRH, 5, 7, 15 (New Format) 767 Illustrated Parts Catalog 31-41 * This change affects Sections 1 and 3.2 of the FAA Approved Airplane Flight Manual. Operators will receive applicable data.
L. Interchangeability and Intermixability of Parts Refer to Paragraph 2.E., Existing Parts Accountability, for interchangeability and intermixability information.
August 20, 1998 767-31-0100 Revision 2: July 29, 1999 7
BOEING SERVICE BULLETIN 767-31-0100
BLANK PAGE August 20, 1998 767-31-0100 Revision 2: July 29, 1999 8