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2. Parts and Materials Supplied by the Operator:
NotesNameQTYPart Number / Specification
(a)Primer1ozBMS 10-11 Type 1
(a) See the Qualified Products List at the end of the Boeing Material Specification (BMS) for supplier data.
3. Parts Modified and Reidentified:
The parts shown below are changed as shown in this service bulletin. The quantity (QTY) is the number of parts changed on each airplane.
Group 1-2:
NotesNew Part NumberNameQTYExisting Part Number
(a) (b)416T2184-4 (c) (d)DEPLOYMENT BAR
ASSEMBLY -416T2184-2 (416T2184-3 optional)
(a) Make the change given in this service bulletin.
(b) There is no equivalent Boeing part number for the changed part. Identify on the part that the change given in this service bulletin was made.
(c) This part is used in production.
(d) This is the part number of the optional part after the change given in this service bulletin.
Group 3-4:
NotesNew Part NumberNameQTYExisting Part Number
(a) (d)416T2184-4 (b) (c)DEPLOYMENT BAR
ASSEMBLY -416T2184-3 (416T2184-2 optional)
(a) Make the change given in this service bulletin.
(b) This is the part number after the change given in this service bulletin.
(c) This part is used in production
(d) There is no equivalent Boeing part number for the optional part. Identify on the optional part that the change given in this service bulletin was made.
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.
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: August 23, 2007 767-25-0428Revision 3: October 21, 2010 25 of 66 BOEING SERVICE BULLETIN 767-25-0428
The parts shown below are for each deployment bar location.
QTYNamePart Number 1SPARES KIT015T1811-3 (a) 1SEPARATION LINK ASSY 416T2232-5 (b) 1SEPARATION LINK ASSY 416T2232-6 (b) 2NUTBACN10YR4CM
(b) 2WASHERNAS1149C0432R
(b)
(a) This kit contains all parts necessary to complete the change for deployment bar location.
(b) These parts are contained in the 015T1811-3
SPARES KIT 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.
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: August 23, 2007 767-25-0428Revision 3: October 21, 2010 26 of 66 BOEING SERVICE BULLETIN 767-25-0428
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. For approved fastener and process material substitutions, refer to 767 SRM, Chapter 51, Alternate fasteners are given in 767 SRM Chapter 51 and Boeing Drawing 012W6100.
4. If the length of any fastener specified in this service bulletin does not meet the installation standards given in SRM Chapter 51, then a fastener of the same specification, or an approved substitute, with a length which meets the installation standards given in SRM Chapter 51 may be used.
5. A General Visual Inspection is defined as: A visual examination of an interior or exterior area, installation or assembly to detect obvious damage, failure or irregularity.
This level of inspection is made from within touching distance unless otherwise specified. A mirror may be necessary to ensure visual access to all surfaces in the inspection area. This level of inspection is made under normal available lighting conditions such as daylight, hangar lighting, flashlight or drop-light and may require removal or opening of access panels or doors. Stands, ladders or platforms may be required to gain proximity to the area being checked.
6. 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. Group 1, 3:
Remove the bustle on the entry/service doors in accordance with FIGURE 1.
2. Group 2, 4:
Remove the bustle on the entry/service doors in accordance with FIGURE 2.
3. Group 1, 3:
Remove existing separation link assembly on the deployment bar in accordance with FIGURE 3.
4. Group 2, 4:
Remove existing separation link assembly on the deployment bar in accordance with FIGURE 4.
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: August 23, 2007 767-25-0428Revision 3: October 21, 2010 27 of 66 BOEING SERVICE BULLETIN 767-25-0428
5. Group 1, 3:
Install new separation link assembly in accordance with FIGURE 5.
6. Group 2, 4:
Install new separation link assembly in accordance with FIGURE 6.
7. Group 1:
Part mark deployment bar assembly in accordance with FIGURE 7.
8. Group 2:
Part mark deployment bar assembly in accordance with FIGURE 8.
9. Group 3:
Part mark deployment bar assembly in accordance with FIGURE 9.
10. Group 4:
Part mark deployment bar assembly in accordance with FIGURE 10.
11. Group 1, 3:
Install the bustle on the entry/service doors in accordance with FIGURE 11.
12. Group 2, 4:
Install the bustle on the entry/service doors in accordance with FIGURE 12.
13. Put the airplane back to a serviceable condition.
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: August 23, 2007 767-25-0428Revision 3: October 21, 2010 28 of 66 BOEING SERVICE BULLETIN 767-25-0428
BOEING SERVICE BULLETIN 767-25-0428 This Figure applies only to: Group 1, 3.
AFT
SERVICE DOOR
FORWARD SERVICE > AFT
DOOR ENTRY DOOR
FORWARD
ENTRY DOOR SEE (A (4 LOCATIONS)
ESCAPE SLIDE PACK
INFLATION
CYLINDER
REGULATOR
STOWAGE POUCH SEE B SEE INBD
YELLOW INDICATOR
FLAG WINDOW FIGURE 1: ENTRY/SERVICE DOOR BUSTLE REMOVAL (SHEET 1 OF 3) Original Issue: August 23, 2007 Revision 3 October 21, 2010 BOEING PROPRIETARY - 767-25-0428 Copyright © Unpublished Work - See page 1 for details. 29 of 66
BOEING SERVICE BULLETIN 767-25-0428
- INFLATION
CYLINDER
REGULATOR SAFETY PIN
PRESSURE SLIDE INSTALLATION IN A/C REMOVE PIN AT TIME OF GAGE
- FIRING
LANYARD
• ESCAPE SLIDE PACK
• DEPLOYMENT BAR — DEPLOYMENT CABLE
GIRT BAR
CARRIER
- FLOOR LEVEL UP
GIRT BAR (IN GIRT BAR CARRIER) FIGURE 1: ENTRY/SERVICE DOOR BUSTLE REMOVAL (SHEET 2 OF 3) Original Issue: August 23, 2007 Revision 3 October 21, 2010 BOEING PROPRIETARY - 767-25-0428 Copyright © Unpublished Work - See page 1 for details. 30 of 66
MORE DATAQTYIDENTIFICATIONNAMETASKSTEP Close and latch the entry/service door.
--DOORClose1 WARNING: BE SURE TO INSTALL THE GROUND LOCK FOR THE ENTRY/SERVICE DOOR. WITHOUT
THE GROUND LOCK INSTALLED, THE DOOR CAN LIFT ACCIDENTALLY, CAUSING INJURY OR DAMAGE.
Install the ground lock for the entry/service door. Refer to 767 AMM 52-11-13 as an accepted procedure.
--DOORLock2 Move the arm/disarm handle to the DISARMED position. Make sure the yellow flag indicators are not shown in the windows at the bottom of the entry/service door.
--ARM/DISARM HANDLE Move3 ---BUSTLERemove / Keep 4 Remove the safety pin from the pouch on the escape slide pack.
--SAFETY PINRemove / Keep 5 WARNING: BE SURE TO INSTALL THE SAFETY PIN IN THE INFLATION CYLINDER REGULATOR. THE ACCIDENTAL INFLATION OF THE ESCAPE SYSTEM CAN CAUSE INJURY OR DAMAGE.
Install safety pin in the inflation cylinder regulator.
--SAFETY PINInstall (Kept)6 CAUTION: DO NOT PULL ON THE RELEASE CABLES WHEN THE GIRT BAR IS MOVED. A FORCE ON
THE CABLES CAN CAUSE THE ESCAPE SLIDE PACK TO RELEASE FROM THE ENTRY/SERVICE DOOR Remove deployment bar cables from the separation links and carefully allow them to retract into the cables retractors --DEPLOYMENT
BAR CABLES Remove / Keep 7 FIGURE 1: ENTRY/SERVICE DOOR BUSTLE REMOVAL (SHEET 3 OF 3)
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: August 23, 2007 767-25-0428Revision 3 October 21, 2010 31 of 66 BOEING SERVICE BULLETIN 767-25-0428
BOEING SERVICE BULLETIN 767-25-0428 This Figure applies only to: Group 2, 4.
AFT
SERVICE DOOR MID
SERVICE
DOOR - AFT ENTRY DOOR
FORWARD
SERVICE DOOR MID
ENTRY DOOR
FORWARD
ENTRY DOOR SEE A (6 LOCATIONS)
ESCAPE SLIDE PACK
INFLATION
CYLINDER
REGULATOR
STOWAGE POUCH SEE
UP SEE C INBD '
YELLOW INDICATOR FLAG WINDOW 1362345 FIGURE 2: ENTRY/SERVICE DOOR BUSTLE REMOVAL (SHEET 1 OF 3) Original Issue: August 23, 2007 Revision 3 October 21, 2010 BOEING PROPRIETARY - 767-25-0428 Copyright © Unpublished Work - See page 1 for details. 32 of 66
BOEING SERVICE BULLETIN 767-25-0428
INFLATION
CYLINDER
REGULATOR SAFETY PIN
PRESSURE SLIDE INSTALLATION IN A/C REMOVE PIN AT TIME OF GAGE
- FIRING
LANYARD
ESCAPE SLIDE PACK
DEPLOYMENT BAR
- DEPLOYMENT CABLE
GIRT BAR
CARRIER
• FLOOR LEVEL UP 'GIRT BAR (IN GIRT BAR CARRIER) 1362372 FIGURE 2: ENTRY/SERVICE DOOR BUSTLE REMOVAL (SHEET 2 OF 3) Original Issue: August 23, 2007 Revision 3 October 21, 2010 BOEING PROPRIETARY - 767-25-0428 Copyright © Unpublished Work - See page 1 for details. 33 of 66
MORE DATAQTYIDENTIFICATIONNAMETASKSTEP Close and latch the entry/service door.
--DOORClose1 WARNING: BE SURE TO INSTALL THE GROUND LOCK FOR THE ENTRY/SERVICE DOOR. WITHOUT
THE GROUND LOCK INSTALLED, THE DOOR CAN LIFT ACCIDENTALLY, CAUSING INJURY OR DAMAGE.
Install the ground lock for the entry/service door. Refer to 767 AMM 52-11-13 as an accepted procedure.
--DOORLock2 Move the arm/disarm handle to the DISARMED position. Make sure the yellow flag indicators are not shown in the windows at the bottom of the entry/service door.
--ARM/DISARM HANDLE Move3 ---BUSTLERemove/Keep4 Remove the safety pin from the pouch on the escape slide pack.
--SAFETY PINRemove/Keep5 WARNING: BE SURE TO INSTALL THE SAFETY PIN IN THE INFLATION CYLINDER REGULATOR. THE ACCIDENTAL INFLATION OF THE ESCAPE SYSTEM CAN CAUSE INJURY OR DAMAGE.
Install safety pin in the inflation cylinder regulator.
--SAFETY PINInstall (Kept)6 CAUTION: DO NOT PULL ON THE RELEASE CABLES WHEN THE GIRT BAR IS MOVED. A FORCE ON
THE CABLES CAN CAUSE THE ESCAPE SLIDE PACK TO RELEASE FROM THE ENTRY/SERVICE DOOR Remove deployment bar cables from the separation links and carefully allow them to retract into the cables retractors --DEPLOYMENT
BAR CABLES Remove/Keep7 FIGURE 2: ENTRY/SERVICE DOOR BUSTLE REMOVAL (SHEET 3 OF 3)
BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details.
Original Issue: August 23, 2007 767-25-0428Revision 3 October 21, 2010 34 of 66 BOEING SERVICE BULLETIN 767-25-0428
BOEING SERVICE BULLETIN 767-25-0428 This Figure applies only to: Group 1, 3.
AFT
SERVICE DOOR
FORWARD
SERVICE AFT
DOOR ENTRY DOOR
• FORWARD
ENTRY DOOR SEE 1 (4 LOCATIONS)
DEPLOYMENT BAR SEE INBD 1362407 FIGURE 3: SEPARATION LINK ASSEMBLY REMOVAL (SHEET 1 OF 3) Original Issue: August 23, 2007 Revision 3 October 21, 2010 Copyright © Unpublished Work - See page 1 for details. BOEING PROPRIETARY - 767-25-0428 35 of 66
BOEING SERVICE BULLETIN 767-25-0428 SEE (D SEE C- INBD 1362413 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 each airplane.
FIGURE 3: SEPARATION LINK ASSEMBLY REMOVAL (SHEET 2 OF 3) Original Issue: August 23, 2007 Revision 3 October 21, 2010 BOEING PROPRIETARY - 767-25-0428 Copyright © Unpublished Work - See page 1 for details. 36 of 66