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Commercial Airplanes 767 Service Bulletin ALERT Number: 767-25A0505 Original Issue: January 14, 2011 ATA System: 2550 SUBJECT: EQUIPMENT / FURNISHINGS - Cargo Compartment - Forward Lower Lobe Water Incursion Change 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BOEING PROPRIETARY, CONFIDENTIAL, AND/OR TRADE SECRET Copyright © 2011 The Boeing Company Unpublished Work - All Rights Reserved Boeing claims copyright in each page of this document only to the extent that the page contains copyrightable subject matter.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.
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: January 14, 2011 767-25A0505 1 of 60
4.0
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Original Issue: January 14, 2011 767-25A0505 2 of 60 BOEING SERVICE BULLETIN 767-25A0505
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BLANK PAGE
Table of Contents
Summary5
1. PLANNING INFORMATION7
A. Effectivity7
1. Airplanes7
2. Spares Affected7
B. Concurrent Requirements7
C. Reason8
D. Description8
E. Compliance8
F. Approval8
G. Manpower9
H. Weight and Balance Changes .................................... 1 0 I. Electrical Load Data ......................................... 1 0 J. References .............................................. 1 0
1. Existing Data .......................................... 1 0
2. Data supplied with this Service Bulletin ............................ 1 0
3. Installation Drawings Used in the Preparation of this Service Bulletin ............ 1 0 K. Publications Affected ........................................ 1 1 L. Interchangeability and Intermixability of Parts ........................... 1 1
2. MATERIAL INFORMATION ........................................ 1 3 A. Material - Price and Availability ................................... 1 3 B. Industry Support Information .................................... 1 3 C. Parts Necessary For Each Airplane ................................. 1 4
1. Kits/Parts ............................................ 1 4
2. Parts and Materials Supplied by the Operator ........................ 1 8
3. Parts Modified and Reidentified ................................ 1 8
4. Parts Removed and Not Replaced .............................. 1 8 D. Parts Necessary to Change Spares ................................. 1 9 E. Special Tooling - Price and Availability ............................... 1 9 F. Special Tooling Necessary to do this Service Bulletin ....................... 1 9
3. ACCOMPLISHMENT INSTRUCTIONS .................................. 2 1 A. GENERAL INFORMATION ..................................... 2 1 B. WORK INSTRUCTIONS ....................................... 2 2 FIGURE 1: CARGO COMPARTMENT - FORWARD LOWER LOBE - REMOVE CEILING LINERS AND STRUCTURE [Group 1] .................................... 2 4 FIGURE 2: CARGO COMPARTMENT - FORWARD LOWER LOBE - INSTALL CARGO BULKHEAD SUPPORT ASSEMBLIES ................................... 2 8 FIGURE 3: CARGO COMPARTMENT - FORWARD LOWER LOBE - INSTALL RIGHT SIDE CEILING SUPPORTS ........................................... 3 1 FIGURE 4: CARGO COMPARTMENT - FORWARD LOWER LOBE - INSTALL LEFT SIDE CEILING SUPPORTS AND INSTALL SUPPORT AT STATION 368 .................. 3 9 FIGURE 5: CARGO COMPARTMENT - FORWARD LOWER LOBE - INSTALL DRAIN TUBING . . . 47 FIGURE 6: CARGO COMPARTMENT - FORWARD LOWER LOBE - INSTALL CEILING PANELS [Group 1 ] ................................................ 5 1 FIGURE 7: CARGO COMPARTMENT - FORWARD LOWER LOBE - REMOVE CEILING LINERS AND STRUCTURE [Group 2] .................................... 5 4
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Original Issue: January 14, 2011 767-25A0505 3 of 60 BOEING SERVICE BULLETIN 767-25A0505
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FIGURE 8: CARGO COMPARTMENT - FORWARD LOWER LOBE - INSTALL CEILING PANELS AND RUB STRIP [Group 2] ..................................... 5 8
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Original Issue: January 14, 2011 767-25A0505 4 of 60 BOEING SERVICE BULLETIN 767-25A0505
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Commercial Airplanes 767 Service Bulletin ALERT SummaryNumber: 767-25A0505Original Issue: January 14, 2011 ATA System: 2550 SUBJECT: EQUIPMENT / FURNISHINGS - Cargo Compartment - Forward Lower Lobe Water Incursion Change
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 and a kit of parts provides retrofit instructions to improve water drainage in the lower lobe.
Water coming through the floor panels can accumulate up to 12 gallons in this location and typical aircraft movement may not remove all the water. There is a potential for water to enter the electronic equipment bay.
Installation of parts assist in water drainage and will prevent water from getting into the electronic equipment bay. If parts are not installed possible water damage could occur to electronic equipment which could result in an electrical short and potential loss of several functions essential for safe flight.
Boeing Service Related Problem (SRP) 767-SRP-25-0290 is related to this service bulletin.
ACTION (PRR F06004-1RS) Install 2 drains, dam and new support structure.
EFFECTIVITY 767-300 and 767-200 Airplanes. Refer to Paragraph 1.A.1., Airplanes, for the list of affected airplanes.
COMPLIANCE Boeing recommends that operator accomplish the instructions provided in this bulletin within 24 months after the Original Issue date on this service bulletin.
The Federal Aviation Administration (FAA) will possibly release an Airworthiness Directive related to this service bulletin. The Airworthiness Directive will make the compliance tasks and times given in this service bulletin mandatory.
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Original Issue: January 14, 2011 767-25A0505 5 of 60
INDUSTRY SUPPORT INFORMATION Group 1:
Boeing warranty remedies are available for airplanes in warranty as of November 5, 2009. Please refer to Paragraph 2.B., Industry Support Information.
Group 2:
Boeing warranty remedies are not available for the configuration changes given in this service bulletin.
MANPOWER Group 1:
Elapsed HoursTotal Task HoursAirplanes
8.5016.00767-300BCF Group 2:
Elapsed HoursTotal Task HoursAirplanes
8.5016.00767-200SF
MATERIAL INFORMATION Boeing Supplied Kits/Parts.
Refer to Paragraph 2.A., Material - Price and Availability.
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: January 14, 2011 767-25A0505 6 of 60 BOEING SERVICE BULLETIN 767-25A0505
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Commercial Airplanes 767 Service Bulletin ALERT Number: 767-25A0505 Original Issue: January 14, 2011 ATA System: 2550 SUBJECT: EQUIPMENT / FURNISHINGS - Cargo Compartment - Forward Lower Lobe Water Incursion Change
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 airplanes shown below. An equivalent change is on subsequent production airplanes. Refer to PRR F06004-1RS for data about this change.
DESCRIPTIONCONFIGURATIONGROUP 767-300BCF for VN191-VN195-1 767-200SF for VA511-2 Airplane Models:
767-200, 767-300 GroupVariable Number 2VA511 1VN191 - VN195
2. Spares Affected None.
B. Concurrent Requirements None.
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C. Reason This service bulletin and a kit of parts provides retrofit instructions to improve water drainage in the lower lobe. Water coming through the floor panels can accumulate up to 12 gallons in this location and typical aircraft movement may not remove all the water. There is a potential for water to enter the electronic equipment bay. Installation of parts assist in water drainage and will prevent water from getting into the electronic equipment bay. If parts are not installed possible water damage could occur to electronic equipment which could result in an electrical short and potential loss of several functions essential for safe flight.
Boeing Service Related Problem (SRP) 767-SRP-25-0290 is related to this service bulletin.
D. Description Installs 2 drains, dam and new support structure.
The work in this service bulletin is done in the maintenance zone(s) given below.
Group 1:
Affected Maintenance Zones ZoneModel 119, 121, 122767-300 Group 2:
Affected Maintenance Zones ZoneModel 119, 121, 122767-200 E. Compliance Boeing recommends that operator accomplish the instructions provided in this bulletin within 24 months after the Original Issue date on this service bulletin.
The Federal Aviation Administration (FAA) will possibly release an Airworthiness Directive related to this service bulletin. The Airworthiness Directive will make the compliance tasks and times given in this service bulletin mandatory.
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 for all 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.
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Original Issue: January 14, 2011 767-25A0505 8 of 60 BOEING SERVICE BULLETIN 767-25A0505
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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 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 1:
Elapsed HoursTask HoursNumber of PersonsTask
0.500.501Open Access
1.503.002Figure 1
0.501.002Figure 2
1.503.002Figure 3
1.252.502Figure 4
1.252.502Figure 5
1.503.002Figure 6
0.500.501Close Access
8.5016.00TOTAL FOR EACH AIRPLANE Group 2:
Elapsed HoursTask HoursNumber of PersonsTask
0.500.501Open Access
1.503.002Figure 7
0.501.002Figure 2
1.503.002Figure 3
1.252.502Figure 4
1.252.502Figure 5
1.503.002Figure 8
0.500.501Close Access
8.5016.00TOTAL FOR EACH AIRPLANE
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Original Issue: January 14, 2011 767-25A0505 9 of 60 BOEING SERVICE BULLETIN 767-25A0505
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H. Weight and Balance Changes Group 1:
Change in Moment (Pound-Inches) Change in Weight (Pounds)Airplane +408.0+2.6767-300BCF Group 2:
Change in Moment (Pound-Inches) Change in Weight (Pounds)Airplane +902.0+3.5767-200SF I. Electrical Load Data Not changed.
J. References
1. Existing Data
a. Engineering Change Memo PRR F06004-1RS
b. Boeing Service Related Problem (SRP) 767-SRP-25-0290
c. Standard Overhaul Practices Manual (SOPM) 20-41-02, 20-50-01, 20-50-19
d. 767 Aircraft Maintenance Manual (AMM) 25-52-02
e. 767-200SF Structural Repair Manual (SRM) 51-40-02
f. 767-300BCF Structural Repair Manual (SRM) 51, 51, 51-40-02, 51-40-08
2. Data supplied with this Service Bulletin None.
3. Installation Drawings Used in the Preparation of this Service Bulletin TitleDrawing Number SUPP0RT INSTALLATION - END LINING, STA 355,453T1104 LINING INSTL - CEILING, FWD LWR CARGO COMPT, MOD657T4640 SUPPORT INSTL - CEILING, FWD LWR CARGO COMPT, MOD657T4641 LINING INSTL - CEILING, LWR CARGO COMPT, MOD845T3108 SUPPORT INSTL - CEILING, LWR CARGO COMPT (MOD)845T3109 STA 355 ENDWALL ASSY - REWORK INSTL845T3154
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Original Issue: January 14, 2011 767-25A0505 10 of 60 BOEING SERVICE BULLETIN 767-25A0505
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These drawings were used to prepare this service bulletin. These drawings are not necessary to make the specified changes, and are not supplied with this service bulletin. These 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 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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Original Issue: January 14, 2011 767-25A0505 11 of 60 BOEING SERVICE BULLETIN 767-25A0505
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