TextPartly OCR
Some pages are OCR from a scan. OCR can misread letters and numbers.
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 = '03aa4e4eefb97582192d64aac429f756e14460d4bf8d55ffdabc15f8123f6306' 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 = '03aa4e4eefb97582192d64aac429f756e14460d4bf8d55ffdabc15f8123f6306' 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.
GroupVariable Number 2VN191 - VN193 3VN194 - VN198 2VN211 - VN212 2VN221 - VN224 3VN225 2VN231 - VN234 2VN241 3VN242 - VN243 2VN251 - VN259 3VN260 - VN276 2VN291 3VN292 - VN293 2VN301 - VN306 3VN307 - VN314 2VN371 - VN372 2VN376 2VN381 3VN382 - VN388 3VN421 - VN427 3VN436 2VN471 - VN472 2VN491 - VN496 3VN497 - VN513 2VN531 - VN532 2VN536 - VN537 2VN541 - VN542 3VN546 - VN547 2VN551 3VN556 - VN557 3VN561 - VN562 2VN631 - VN633 3VN634 - VN638 2VN651 - VN652 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: April 20, 2015 767-53A0266 13 of 41 BOEING SERVICE BULLETIN 767-53A0266
ALERTALERT
GroupVariable Number 3VN653 - VN658 2VN671 - VN672 3VN676 2VN681 - VN683 3VN684 - VN691 2VN731 3VN732 2VN751 - VN753 3VN791 - VN792 3VN811 - VN813 3VN921 - VN922 3VN931 - VN936 3VN951 - VN953 3VN966 - VN972 3VQ001 - VQ021 3VQ071 - VQ086 4VQ111 3VR051 - VR060 3VR081 3VR084 3VR086 4VR087 - VR089 4VR106 - VR109 3VR201 - VR211 3VR251 3VR256 - VR260 4VR266 - VR292 3VR401 3VR421 - VR423 3VR426 3VR441 3VR461 3VR471 - VR472 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: April 20, 2015 767-53A0266 14 of 41 BOEING SERVICE BULLETIN 767-53A0266
ALERTALERT
GroupVariable Number 3VS051 - VS056 3VS061 3VS066 - VS070 3VS073 - VS078 3VS091 - VS104 3VS111 - VS113 3VS131 - VS133 3VS136 - VS137 3VS176 - VS177 3VS186 - VS187 3VS196 - VS203 3VS206 - VS208 3VS211 3VS216 - VS217 3VS231 3VS246 - VS248 3VS261 - VS263 3VS266 - VS274 3VS291 - VS293 3VS301 - VS303 3VS306 - VS311 3VS316 3VS321 - VS324 3VS331 - VS333 3VS336 - VS337 3VS366 - VS367 3VS381 - VS382 3VS391 - VS392 3VS401 3VS426 - VS428 3VS466 - VS472 3VS486 3VS496 - VS497 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: April 20, 2015 767-53A0266 15 of 41 BOEING SERVICE BULLETIN 767-53A0266
ALERTALERT
GroupVariable Number 3VS506 - VS507 3VS526 3VS546 - VS549 3VS701 - VS710 4VS711 - VS720 3VS721 - VS731 4VS732 - VS736 3VS751 - VS759 3VS821 - VS825 3VS841 - VS844 3VS861 3VS881 - VS882 4VS883 3VS891 4VS896 4VS901 - VS912 4VS916 4VS921 - VS928 4VS931 - VS933 4VS941 4VS951 - VS954 4VS961 - VS969 4VS971 - VS977 4VS981 - VS984 4VT001 - VT013 4VT021 4VT031 - VT033 3VT501 4VT511 - VT513 4VT521 - VT523 4VT531 - VT533 4VT541 - VT546 4VT551 - VT552 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: April 20, 2015 767-53A0266 16 of 41 BOEING SERVICE BULLETIN 767-53A0266
ALERTALERT
GroupVariable Number 4VT556 - VT585 3VV001 3VW701 - VW721 3VW851
2. Spares Affected None.
B. Concurrent Requirements None.
C. Reason Accomplishment of the inspection described in this service bulletin will enable detection and repair of cracks if they should occur, in the areas under splice plates at the STA 1582 aft pressure bulkhead web to pressure chord joint. If a crack is present in the aft pressure bulkhead web and not found and repaired, crack growth can result in possible rapid decompression and loss of structural integrity.
The aft pressure bulkhead web is attached to the pressure chords with a double row of fasteners and the pressure chord segments are spliced using pressure chord splice plates. At these splice plate locations, the aft pressure bulkhead web is hidden and cannot be inspected in accordance with existing 767 MPD Section 9 or SB 767-53A0087 and do not provide sufficient crack detection probability of the aft pressure bulkhead web under splice plates.
Boeing Service Related Problem 767-SRP-53-0470 is related to this service bulletin.
Boeing Service Bulletins 767-53A0087 and 767-53A0139 are related to this service bulletin.
Boeing 767 MPD SSI 53-80-I01A is related to this service bulletin.
D. Description Get access to the forward and aft sides of the aft pressure bulkhead at STA 1582. Locate the splice plates that splice pressure chords on the circumference of the forward side of the aft pressure bulkhead.
Remove the aft row of fasteners from each splice plate and do an open hole HFEC inspection for any crack in the aft pressure bulkhead web. If any crack is found, contact The Boeing Company for repair instructions and do the repair. If no crack is found, install new fasteners, close access to the area and repeat the inspection at the time specified in Paragraph 1.E., Compliance.
The work in this service bulletin is done in the maintenance zone(s) given below.
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: April 20, 2015 767-53A0266 17 of 41 BOEING SERVICE BULLETIN 767-53A0266
ALERTALERT
Group 1-2:
Affected Maintenance Zones ZoneModel 165, 166, 251, 252, 253, 254, 311, 312767-200, 767-300 Group 3-4:
Affected Maintenance Zones ZoneModel 165, 166, 251, 252, 253, 254, 311, 312767-200, 767-300, 767-300F, 767-400ER E. Compliance The Federal Aviation Administration (FAA) will possibly release an additional Airworthiness Directive related to this service bulletin. The Airworthiness Directive will make the compliance tasks and times given in this service bulletin mandatory.
Federal Aviation Administration (FAA) Airworthiness Directive AD 2004-05-16 is related to this service bulletin. The effective date of AD 2004-05-16 is April 13, 2004.
Federal Aviation Administration (FAA) Airworthiness Directive AD 2012-09-08 is related to this service bulletin. The effective date of AD 2012-09-08 is June 18, 2012.
Federal Aviation Administration (FAA) Airworthiness Directive AD 2014-14-04 is related to this service bulletin. The effective date of AD 2014-14-04 is September 5, 2014.
This service bulletin is related to 767 MPD SSI 53-80-I01A of 767 MPD 622T001-9, which is mandated by AD 2014-14-04. All other MPD inspections outside of the affected area are not affected and must continue.
Logic diagrams showing compliance tasks and compliance times are included as an aid in APPENDIX A and APPENDIX B.
Do the required actions in accordance with Paragraph 3. Accomplishment Instructions.
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: April 20, 2015 767-53A0266 18 of 41 BOEING SERVICE BULLETIN 767-53A0266
ALERTALERT
Group 2, Configuration 1; Group 3-4:
Table 1: Open Hole High Frequency Eddy Current (HFEC) Inspection at STA 1582 Aft Pressure Bulkhead Web Under the Pressure Splice Plates Repeat Interval (Not to Exceed) Compliance Time (Whichever Occurs Later) ActionCondition -Within 3,000 flight cycles after the original issue date of this service bulletin.
Before 50,000 total flight cycles.
Do PART 2: FASTENER
REMOVAL AND OPEN
HOLE HFEC INSPEC- TION of the aft pressure bulkhead web for any crack.
All airplanes.
(a) -Before further flight.Contact The Boeing Company for repair instructions and do the repair.
CONDITION 1: ANY
CRACK FOUND IN THE
AFT PRESSURE BULK- HEAD WEB.
12,000 flight cycles.
--Repeat PART 2: FASTEN-
ER REMOVAL AND
OPEN HOLE HFEC IN- SPECTION of the aft pressure bulkhead web for any crack.
CONDITION 2: NO
CRACK FOUND IN THE
AFT PRESSURE BULK- HEAD WEB.
(a)
(a) It is not necessary to do inspections in accordance with this service bulletin in areas where existing repairs approved by Boeing ODA via FAA 8100-9 form cover the affected inspection areas. Damage tolerance inspection instructions specified in approval for existing repairs must continue. Inspection outside of the repaired area must continue in accordance with this service bulletin.
Group 1; Group 2, Configuration 2:
Table 2: Open Hole High Frequency Eddy Current (HFEC) Inspection at STA 1582 Aft Pressure Bulkhead Web Under the Pressure Splice Plates Repeat Interval (Not to Exceed) Compliance Time (Whichever Occurs Later) ActionCondition -Within 3,000 flight cycles after the original issue date of this service bulletin.
Within 37,500 flight cycles after replacement of the aft pressure bulkhead.
Do PART 2: FASTENER
REMOVAL AND OPEN
HOLE HFEC INSPEC- TION of the aft pressure bulkhead web for any crack.
All airplanes.
(a) -Before further flight.Contact The Boeing Company for repair instructions and do the repair.
CONDITION 1: ANY
CRACK FOUND IN THE
AFT PRESSURE BULK- HEAD WEB.
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: April 20, 2015 767-53A0266 19 of 41 BOEING SERVICE BULLETIN 767-53A0266
ALERTALERT
Group 1; Group 2, Configuration 2:
Table 2: Open Hole High Frequency Eddy Current (HFEC) Inspection at STA 1582 Aft Pressure Bulkhead Web Under the Pressure Splice Plates Repeat Interval (Not to Exceed) Compliance Time (Whichever Occurs Later) ActionCondition 12,000 flight cycles.
--Repeat PART 2: FASTEN-
ER REMOVAL AND
OPEN HOLE HFEC IN- SPECTION of the aft pressure bulkhead web for any crack.
CONDITION 2: NO
CRACK FOUND IN THE
AFT PRESSURE BULK- HEAD WEB.
(a)
(a) It is not necessary to do inspections in accordance with this service bulletin in areas where existing repairs approved by Boeing ODA via FAA 8100-9 form cover the affected inspection areas. Damage tolerance inspection instructions specified in approval for existing repairs must continue. Inspection outside of the repaired area must continue in accordance with 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.
The Manager of the FAA Seattle Aircraft Certification Office (SACO) approves the accomplishment of inspections defined in this Service Bulletin (SB) along with the corresponding compliance times specified in Paragraph 1.E., Compliance of this SB, Original Issue, as an Alternative Method Of Compliance (AMOC) to the inspections defined in D622T001-DTR Structural Significant Item (SSI) 53-80-I01A and Section 9 of the Maintenance Planning Document (MPD) D622T001-9, required by paragraphs (i) and
(k) of Airworthiness Directive (AD) 2014-14-04. This AMOC only applies to the areas inspected in accordance with this SB. All other inspections outside of this SB inspection region are not affected and must continue. All provisions of AD 2014-14-04 that are not specifically referenced in this paragraph remain fully applicable and must be complied with accordingly.
In Addition, the Manager of the FAA SACO approves the accomplishment of inspections defined in this SB along with the corresponding compliance times specified in Paragraph 1.E., Compliance of this SB, Original Issue, as an AMOC to the inspections defined in SB 767-53A0087 required by paragraphs
(a) and (b) of AD 2004-05-16. This AMOC only applies to the areas inspected in accordance with this SB. All other inspections outside of this SB inspection region are not affected and must continue. All provisions of AD 2004-05-16 that are not specifically referenced in this paragraph remain fully applicable and must be complied with accordingly.
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: April 20, 2015 767-53A0266 20 of 41 BOEING SERVICE BULLETIN 767-53A0266
ALERTALERT
In addition, the Manager of the FAA SACO approves the accomplishment of inspections, after Replacement of an Aft Pressure Bulkhead, defined in this SB along with the corresponding compliance times specified in Paragraph 1.E., Compliance of this SB, Original Issue, as an AMOC to the inspections defined in SB 767-53A0139 required by paragraph (h) of AD 2012-09-08. This AMOC only applies to the areas inspected in accordance with this service bulletin. All other inspections outside of this service bulletin inspection region are not affected and must continue. All provisions of AD 2012-09-08 that are not specifically referenced in this paragraph remain fully applicable and must be complied with accordingly.
G. Manpower The tables below show estimates of the task hours necessary to do the inspection 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 estimates do not include lost time. These are some examples of lost time:
• Time to adjust to the workplace
• 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.
Group 2, Configuration 1; Group 3:
Passenger Airplanes Only Elapsed HoursTask HoursNumber of PersonsTask
5.0020.004Open Access
2.354.702FIGURE 1
0.250.502FIGURE 3
5.0020.004Close Access
12.6045.20TOTAL FOR EACH AIRPLANE Group 2, Configuration 1; Group 3:
Freighters and Converted Freighters Only Elapsed HoursTask HoursNumber of PersonsTask
3.006.002Open Access
2.354.702FIGURE 1
0.250.502FIGURE 3
3.006.002Close Access
8.6017.20TOTAL FOR EACH AIRPLANE Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: April 20, 2015 767-53A0266 21 of 41 BOEING SERVICE BULLETIN 767-53A0266
ALERTALERT
Group 1; Group 2, Configuration 2; Group 4:
Passenger Airplanes Only Elapsed HoursTask HoursNumber of PersonsTask
5.0020.004Open Access
3.006.002FIGURE 2
0.350.702FIGURE 4
5.0020.004Close Access
13.3546.70TOTAL FOR EACH AIRPLANE Group 1; Group 2, Configuration 2; Group 4:
Freighters and Converted Freighters Only Elapsed HoursTask HoursNumber of PersonsTask
3.006.002Open Access
3.006.002FIGURE 2
0.350.702FIGURE 4
3.006.002Close Access
9.3518.70TOTAL FOR EACH AIRPLANE H. Weight and Balance Changes None.
I. Electrical Load Data Not changed.
J. References
1. Existing Data:
a. Boeing Service Bulletin 767-53A0087, 767-53A0139
b. Boeing Service Letter 767-SL-51-036
c. Boeing Service Related Problem (SRP) 767-SRP-53-0470
d. Federal Aviation Administration (FAA) Airworthiness Directive (AD) 2004-05-16, 2012-09-08, 2014-14-04
e. Service Bulletin Index D624T001
f. Standard Overhaul Practices Manual (SOPM) 20-50-01 Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: April 20, 2015 767-53A0266 22 of 41 BOEING SERVICE BULLETIN 767-53A0266
ALERTALERT
g. 767 Aircraft Maintenance Manual (AMM) 25-31-04, 25-52-01, 25-52-03, 25-55-01, 25-59-01, 25-59-05, 27-41-00, 38-11-01, 38-32-11
h. 767 Maintenance Planning Data (MPD) 622T001-9, Section 9, SSI 53-80-I01A
i. 767 Non-Destructive Testing (NDT) Manual Part 6, 51-00-04, Part 6, 51-00-11
j. 767-200 Structural Repair Manual (SRM) 51-40-02, 51-40-03, 51-40-05
k. 767-200SF Structural Repair Manual (SRM) 51-40-02, 51-40-03, 51-40-05
l. 767-300 Structural Repair Manual (SRM) 51-40-02, 51-40-03, 51-40-05
m. 767-300BCF Structural Repair Manual (SRM) 51-40-02, 51-40-03, 51-40-05
n. 767-300F Structural Repair Manual (SRM) 51-40-02, 51-40-03, 51-40-05
o. 767-400 Structural Repair Manual (SRM) 51-40-02, 51-40-03, 51-40-05
2. Data Supplied with this Service Bulletin:
None.
3. Installation Drawings Used in the Preparation of this Service Bulletin:
TitleDrawing Number Splice Plate - Press Bulkhead STA 1582148T2620 Bulkhead End Item Pressure Dome, Station 1582.0148T2610 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:
None.
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 affects FCS but no new DTIs are necessary.
L. Interchangeability and Intermixability of Parts Accomplishment of this service bulletin does not affect interchangeability or intermixability of parts.
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: April 20, 2015 767-53A0266 23 of 41 BOEING SERVICE BULLETIN 767-53A0266
ALERTALERT
M. Software Accomplishment Summary Not affected.
Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: April 20, 2015 767-53A0266 24 of 41 BOEING SERVICE BULLETIN 767-53A0266