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Discard the Revision 01 of this Service Bulletin dated Sep 05/2018 and replace in its entirety with this Revision 02.
Service Bulletin No. 700−35−6003 Date of Basic Issue Jul 03/2018 Revision No. 01 Dated Sep 05/2018 Revision No. 02 Dated Nov 23/2018 This revision has no effect for aircraft on which the Basic Issue or Revision 01 of this Service Bulletin was done thus no other action is necessary. Do not sign the log book if you have not done this revision. Keep the previous log book entry. You may make an entry as “Not Applicable” for this revision.
This revision is issued to:
1. Revise in Paragraph 1.A., to add aircraft 9817 to the effectivity.
2. Make miscellaneous minor changes, as necessary, with no change in context.
SERVICE BULLETIN MODEL BD−700−1A10 (BD−700) 700−35−6003 Page 1 of 1
REVISION TRANSMITTAL SHEET
MODIFICATION - PORTABLE OXYGEN PROVISION -
REPLACEMENT OF THE BRACKET OF THE OXYGEN BOTTLE BRACKET The information below is provided for your reference. For full details, including labor and part coverage, please see corresponding paragraph contained within this bulletin.
RECOMMENDED
SPECIFIED TIME COMPLIANCE
COMPLIANCE TIME At the next 60−months inspection that follows this Service Bulletin Release Date (Basic Issue)) EFFECTIVITY: Refer to Paragraph 1.A.
MANPOWER: Refer to Paragraph 1.F.
CONTINUED AIRWORTHINESS (CAW)
FLEET CAMPAIGN NOYES TLMC, CH 5 AFFECTED NOYES KITS and/or PARTS YES NO
TOOLING/GSE YES NO PLANNING INFORMATION: See important information at the start of Paragraph 1. YES NO
DEDICATED SCHEDULE NOYES PREREQUISITE SERVICE BULLETINS: N/A NOTE: This Service Bulletin may be subject to an Airworthiness Directive, which will make it necessary to implement this Service Bulletin.
To place an order for parts or kits, please call Bombardier Aerospace Parts Services at:
514−855−2999 or 1−866−538−1247
SERVICE BULLETIN SUMMARY my.businessaircraft.bombardier.com MODEL BD−700−1A10 (BD−700) ATA 35−30 OXYGEN Basic Issue: Jul 03/2018 Revision 02: Nov 23/2018 700−35−6003 Page 1 of 1 This Service Bulletin is available at:
MODIFICATION - PORTABLE OXYGEN PROVISION - REPLACEMENT OF THE BRACKET OF THE OXYGEN BOTTLE BRACKET1.
PLANNING INFORMATION NOTES: 1. Before you do this Service Bulletin, examine all STC, STA or equivalent action changes to make sure that this Service Bulletin can be completed.
2. For any technical issues, contact CSE, Technical Support, Global Express by e−mail at SRPSA@aero.bombardier.com.
A. Effectivity BD−700−1A10 aircraft, Serial No. 9381, 9438, 9460, 9470, 9475, 9478, 9479, 9481, 9484, 9485, 9499, 9524, 9529, 9530, 9533, 9538, 9551, 9553, 9568, 9598, 9615, 9624, 9632, 9638, 9640, 9641, 9648, 9657, 9670, 9680, 9682, 9689, 9700, 9706, 9723, 9726, 9730, 9731, 9745, 9752, 9753, 9757, 9759, 9773, 9775, 9804, 9814, 9816 and 9817.
NOTE: The instructions given in this Service Bulletin are only applicable to the systems and parts installed at the time of delivery of the aircraft or as changed by Bombardier Aerospace Service Bulletin(s).
B. Reason
1. Condition:
On some aircraft, fast and easy access to the portable oxygen bottle was prevented due to the bracket latch of the portable oxygen bottle upper bracket assembly catching the rigid tube or the gauge on the bottle during portable oxygen bottle retrieval.
SERVICE BULLETIN my.businessaircraft.bombardier.com MODEL BD−700−1A10 (BD−700) ATA 35−30 OXYGEN Refer to applicable governmental agency regulations and requirements and make sure that the work described in this Service Bulletin is performed in compliance with manufacturer’s recommendations and/or acceptable industry standards.
This document is proprietary to Bombardier Inc. and/or its affiliates and may not be reproduced or copied in any form or by any means without the prior written consent of Bombardier Inc. and/or its affiliates.
2018 Bombardier Inc. All rights reserved Learjet, Challenger, Global, are registered trademarks of Bombardier Inc. or its subsidiaries.
Basic Issue: Jul 03/2018 Revision 02: Nov 23/2018 700−35−6003 Page 1 of 14 This Service Bulletin is available at:
2. Evidence:
The current installation might not meet the requirement of Canadian Aviation Regulations (CAR) 704, and Airworthiness Manual 525.1411, which require easy access to the portable oxygen bottle for commercial operations when a flight attendant is needed.
3. Objective/Benefit:
This Service Bulletin introduces a modified top bracket and new middle bracket which will improve the access to the portable oxygen bottle.
C. Description NOTE: Existing installation, location and quantity within the aircraft cabin may vary. This Service Bulletin is to be performed on each applicable installation. Refer to the applicable aircraft specific IPC or SIPC for more details.
This Service Bulletin gives instructions to:
− Get access to the portable oxygen bottle, − Install the new adaptor, − Install the new upper bracket assembly, − Install the new middle bracket assembly, and − Install the portable oxygen bottle.
D. Compliance Recommended at the next 60−months inspection that follows this Service Bulletin Release Date (Basic Issue).
NOTE: If it is not possible to complete all the instructions in this Service Bulletin because of the aircraft configuration, submit an SRPSA for analysis and to get an approved disposition to complete this Service Bulletin.
E. Approval The technical content of this Service Bulletin has been approved under the authority of TC STC number SA12–16, FAA STC number ST03088NY, EASA STC number 10042314.
MODEL BD−700−1A10 (BD−700) Basic Issue: Jul 03/2018 Revision 02: Nov 23/2018 700−35−6003 Page 2 of 14
F. Manpower NOTES: 1. The man−hours given are to help you schedule the tasks given in this Service Bulletin. The man−hours are for direct labor performed by an experienced crew and do not include the time for familiarization, planning, aircraft preparation in hangar such as towing and positioning of scaffolds, removal of interior furnishings, repainting, supervision and inspection.
For more information related to the manpower, refer to SB 700−00−6002.
2. This Service Bulletin may require consumable materials that have specific curing times (refer to Paragraph 3). The accumulated curing time is not included in the man−hours and should be considered for planning purposes before you schedule this Service Bulletin.
3. Labor hours are based on the fact that the modification will be done at the next scheduled maintenance task or inspection Therefore no man−hours are allotted to prepare the aircraft for maintenance or to prepare for this Service Bulletin.
2 man−hours is necessary to do this modification for each portable oxygen cylinder.
The labor required to do this Service Bulletin is at no cost if:
− the work is done at Bombardier Business Aviation Services (BBAS) or Authorized Service Facilities (ASF), and − this Service Bulletin is scheduled at the next 60−months inspection that follows its release date (Basic Issue).
G. Material − Cost and Availability Kit 700K35−014 is necessary to do this modification.
KIT NO. PRICE 700K35−014 Please contact Bombardier Aerospace Parts Services, in Montreal, for delivery lead times and confirmation of prices.
NOTE: A kit is necessary for each portable oxygen cylinder installation.
This kit is available at no cost if:
− a no−charge purchase order is sent to Bombardier Aerospace before the next 60−months inspection that follows this Service Bulletin release date (Basic Issue).
MODEL BD−700−1A10 (BD−700) Basic Issue: Jul 03/2018 Revision 02: Nov 23/2018 700−35−6003 Page 3 of 14
For all parts transactions, Bombardier Aerospace’s current Spare Parts and Component Repair Price Catalogue General Terms and Conditions apply. These terms and conditions are found on the Bombardier Customer Portal at:
my.businessaircraft.bombardier.com During or after the above free period, Smart Parts Plus does not pay for the kit.
H. Tooling The equipment and tools listed below are necessary to do this modification:
GSE REFERENCE NO. PART NO. DESCRIPTION Commercially Available − Torque Wrench NOTES: 1. Refer to the Global 6000 Illustrated Tool and Equipment Manual (ITEM) to make sure that you use the correct equipment configuration.
2. Refer to the Liability Statement in the ITEM for the G6000 for acceptable GSE equivalents.
I. Weight and Balance It is the responsibility of the maintenance facility incorporating this change to calculate the weight and balance impact for this installation and to update the aircraft weight and balance report accordingly.
ITEM WEIGHT Middle Bracket Assembly (Part No.
H3−2178−1)
0.21 pounds (0.10 kg) Adaptor Plate (Part No.
BAS67039859−22)
0.34 pounds (0.15 kg) J. Electrical Load Data No change.
K. References − Bombardier Aerospace, Drawing BAS67039859, Rev. A.
− Bombardier Aerospace, Standard Practices Manual (SPM), Chapter 20.
− Global 6000 BD−700 Aircraft Maintenance Manual (AMM), Chapter 6.
− Global 6000 BD−700 Structural Repair Manual (SRM), Chapter 51.
− Bombardier Aerospace, Instructions for Continued Airworthiness, BAS67058060 (attached).
MODEL BD−700−1A10 (BD−700) Basic Issue: Jul 03/2018 Revision 02: Nov 23/2018 700−35−6003 Page 4 of 14
L. Other Publications Affected − Bombardier Aerospace, Supplemental Maintenance Manual (SMM), Chapter 35.
− Bombardier Aerospace, Supplemental Illustrated Parts Catalog (SIPC), Chapter 35.
M. Equivalent Service Bulletins For the Global Express and Global Express XRS BD−700−1A10 aircraft, use SB 700−35–014.
For the Global 5000 BD−700−1A11 aircraft, use SB 700−1A11−35−013.
For the Global 5000 BD−700−1A11 Featuring Global Vision Flight Deck aircraft, use SB 700−35−5003.
2. ACCOMPLISHMENT INSTRUCTIONS NOTES: 1. All TASKs given in the procedures that follow are from the Global 6000 BD−700−1A10 Aircraft Maintenance Manual (AMM) unless otherwise specified.
2. All references made to zones, access panels and/or doors, are from the Global 6000 BD−700−1A10 Aircraft Maintenance Manual (AMM), Chapter 6.
3. Existing installation, location and quantity within the aircraft cabin may vary. This Service Bulletin to be performed on each applicable installation.
Refer to the applicable aircraft specific IPC or SIPC for more details.
A. Aircraft Setup NOTE: The steps in the Aircraft Setup section of this Service Bulletin are recommended steps. The steps give a recommendation to get access to the work area. This recommendation is to give a safe work area and to minimize possible damage to surrounding aircraft parts. Alternative steps can be used at the operator’s discretion.
Get access to the portable oxygen cylinder, usually in the forward wardrobe.
B. Modification NOTE: If it is not possible to complete all the instructions in this Service Bulletin because of the configuration of the aircraft, submit an SRPSA for analysis and to get an approved disposition to complete this Service Bulletin.
(1) Remove the oxygen cylinder from the upper bracket, Part No. 36758−02 or 36758−12, and lower brackets, Part No. 36758−01 or 36758−11. Refer to Drawing BAS67039859.
(2) Remove and keep the screws and the upper and lower bracket. Refer to Drawing BAS67039859.
MODEL BD−700−1A10 (BD−700) Basic Issue: Jul 03/2018 Revision 02: Nov 23/2018 700−35−6003 Page 5 of 14
(3) Modify the upper bracket (1) as follows. Refer to Figure 1.
(a) Remove and discard the spring pins (2), spring (3), lever (4), and the clamp (5), from the upper bracket (1).
(b) Re−identify the upper bracket (1) to BAS67039859−10 with an ink stamp, per best shop practice.
(4) Install the adaptor plate, Part No. BAS67039859−22 as follows. Refer to Drawing BAS67039859.
(a) Install the middle bracket, Part No. H3−2178−1 on the adaptor plate with the screws, Part No. NAS1581F3T7 and the nuts, Part No. MS21042L3.
Torque the nuts 15 to 18 lbf in (1.70 to 2.03 Nm). Refer to Views A−A (Post−Modification) and B−B.
(b) Position the adaptor over the inserts (on which the lower and upper brackets were installed) View A−A (Post−Modification).
(c) Locate upper bracket on the adaptor plate, centering the upper bracket and drill three holes to match the mounting inserts or nutplates in the adaptor plate of a diameter of 0.165 to 0.169 in. (4.20 to 4.29 mm), as shown in View A−A (Post−Modification).
NOTE: If the inserts are #10, drill the holes to 0.189 to 0.192 in. (4.80 to
4.87 mm).
(d) Mark the position of the two lower inserts to match the mounting inserts or nutplates in the adaptor plate.
NOTE: If necessary, trim the adaptor to make sure that there is no interference with existing parts.
(e) Drill the two marked holes in the adaptor plate of a diameter of 0.165 to
0.169 in. (4.20 to 4.29 mm).
NOTE: If the inserts are #10, drill the holes to 0.189 to 0.192 in. (4.80 to
4.87 mm).
(f) Remove the burrs and sharp edges.
(g) Touch−up the holes and, if necessary, the reworked areas of the adaptor plate to finish A032. Refer to SRM 51−01−04.
NOTE: It is permitted to refinish the adaptor plate to a color to match the surrounding color.
(h) Install the adaptor plate with the lower and upper brackets one of the ways that follows:
(i) If there is mounting brackets, install the adaptor plate, the lower bracket and the upper bracket with the existing screws on the mounting brackets. If there is interference with other parts, it is allowed to use the screws, Part No. MS35207−266, and the spacers, Part No. NAS43DD3−24FC between the mounting brackets and the adaptor plate. Torque the screws 12 to 15 lbf in (1.36 to 1.69 Nm).
Refer to Views A−A (Post−Modification) and C−C.
NOTE: It is allowed to use longer or shorter screws and spacers.
MODEL BD−700−1A10 (BD−700) Basic Issue: Jul 03/2018 Revision 02: Nov 23/2018 700−35−6003 Page 6 of 14
(ii) If there is no mounting bracket, install the adaptor plate, the lower bracket and the upper bracket with the screws, Part No.
MS35207−266, directly to the panel. If there is interference with other parts, it is allowed to use the spacers, Part No. NAS43DD3−24FC between the panel and the adapter plate. Torque the screws 12 to 15 lbf in (1.36 to 1.69 Nm). Refer to View C−C. Refer to Views A−A (Post−Modification) and C−C.
NOTE: It is allowed to use longer or shorter screws and spacers.
(5) Install the oxygen cylinder on the lower brackets and middle bracket.
C. Close−out NOTE: The steps in the Close−out section of this Service Bulletin, except for the return−to−service tests, are recommended steps. The steps give a recommendation to install components removed during the Aircraft Setup.
This recommendation is to make sure that the aircraft is safe and ready to return to service. Alternative steps can be used at the operator’s discretion.
Remove all tools, equipment and unwanted materials from the aircraft.
D. Recording When this Service Bulletin is completed, make an entry in the aircraft log and send the attached Incorporation Notice to Bombardier Business Aircraft Customer Services (BBACS).
In an effort to improve the quality of our technical communications, we are requesting your feedback. Please take a moment to fill out our easy on−line Service Bulletin survey:
http://csefeedback.aero.bombardier.com
3. MATERIAL INFORMATION A. Kit Kit 700K35−014 is necessary to do this Service Bulletin and contains the parts that follow:
NEW PART NO. QTY ITEM USED PART NO.
INSTRUCTIONS
- DISPOSITION BAS67039859−22 1 Adaptor Plate − − H3−2178−1 1 Middle bracket Assembly − − MODEL BD−700−1A10 (BD−700) Basic Issue: Jul 03/2018 Revision 02: Nov 23/2018 700−35−6003 Page 7 of 14
NEW PART NO. QTY ITEM USED PART NO.
INSTRUCTIONS
- DISPOSITION MS21042L3 3 Nut − − MS35207−266 6 Screw − − NAS1581F3T7 3 Screw, countersink, Reduced Head − − NAS43DD3−24FC 6 Spacer − − NOTES: 1. A kit is required for each portable oxygen installation.
2. In case of discrepancy between this list and the Service Bulletin Kit Parts List contained in the respective kit, then the latter list prevails.
3. The actual quantity for some of the hardware contained in the kit can be greater than the amount shown in the table as these items are supplied in prepackaged quantities.
B. Parts No parts required.
C. Material The materials that follow, or equivalent, are necessary to do this Service Bulletin.
They can be purchased from a local supplier. Bombardier Aerospace does not pay for these consumables.
DESCRIPTION PARTNO./NAME SPECIFICATION QUANTITY
SUPPLIER (SEE NOTE) Polyurethane Topcoat CT: 6 hours − BAMS 565−002 Color: Grey #16515 per FED−STD−595) Color: To match Aircraft Paint Scheme As Necessary Code: A Primer, Epoxy CT: 3.5 hours − BAMS 565−001 As Necessary Code: A MODEL BD−700−1A10 (BD−700) Basic Issue: Jul 03/2018 Revision 02: Nov 23/2018 700−35−6003 Page 8 of 14
DESCRIPTION PARTNO./NAME SPECIFICATION QUANTITY
SUPPLIER (SEE NOTE) Coating Chemical Conversion Alodine 1200S MIL−DTL−81706, Class 1A As Necessary Code: B NOTES: 1. Refer to the table that follows for each suppliers address listed by codes.
2. The Curing Time (CT), if applicable, for each consumable material is indicated with the description of each product.
3. At time of release of this Service Bulletin, the information on the supplier was valid and accurate. In the event that this information has changed, the operator is encouraged to use the World Wide Web to find a local supplier.
SUPPLIERS ADDRESSES BY CODES Code: A Tempo Aerospace 205 Fenmar Dr.
North York, ON, Canada M9L 2X4 Tel.: (416) 746−2233 Fax.: (416) 746−2235 www.tempo−aerospace.com Code: B Commercially Available D. Publications No publications required.
MODEL BD−700−1A10 (BD−700) Basic Issue: Jul 03/2018 Revision 02: Nov 23/2018 700−35−6003 Page 9 of 14
BAS67039859 − Portable Oxygen Bottle Bracket Replacement (Sheet 1 of 4, Rev. A) Basic Issue: Jul 03/2018 Revision 02: Nov 23/2018 700−35−6003 Page 10 of 14