BOMBARD I ER B OMBARD IE R 

### GLOBAL5000 CUSTOMER SERVICES BUSINESS A I RCRA F T 

# SERVICE BULLETIN SUMMARY This Service Bulletin is available at: www.cic. bombardier.com 

### BD-700-1A11 (BD-700) ATA 35-21 OXYGEN MODIFICATION - PASSENGER OXYGEN SYSTEM - CHANGE LANYARD ON MASK FOR CORRECT LENGTH The information below is provided for your reference. Forfull details, please see corresponding paragraph contained within this bulletin. 

## COMPLIANCE TIME 

# RECOMMENDED Within 750 Flight hours or at the next "C" SPECIFIED TIME COMPLIANCE check, whichever comes first EFFECTIVITY: Refer to Paragraph 1.A. MANPOWER: Refer to Paragraph 1 .F. CONTINUED AIRWORTHINESS (CAW) YES 

# D NO



### ~ FLEET CAMPAIGN KITS and/or PARTS YES



### ~ NO 

# D TOOLING/GSE YES 

# D NO



### ~ PLANNING INFORMATION: See important YES 

# D NO



### ~ information at the start of Paragraph 1. DEDICATED SCHEDULE YES 

## D NO 

# lZl PREREQUISITE SERVICE BULLETINS: N/A NOTE: This Service Bulletin is subject to an Airworthiness Directive (AD) , CF-2012-31 , issued by Transport Canada. To place an orderfor parts or kits, please call Bombardier Aerospace Parts Services at: 514-855-2999 or 1-866-538-1247 Basic Issue: Oct 22/2012 Revision 02: May 28/2013 

# 700-1A11-35-009 Page 1 of 1'

### , BOM B AR D IER BO M BARDIER 

### GLOBALSOOO CUSTOMER SERVICES BUSINESS AIRCRAF"T 

# SERVICE BULLETIN This Service Bulletin is available at: www.cic.bombardier. com 

### BD-700-1A11 (BD-700) ATA 35-21

OXYGEN MODIFICATION - PASSENGER OXYGEN SYSTEM - CHANGE LANYARD ON MASK FOR CORRECT LENGTH RETROACTIVE ACTION THE ACTION THAT FOLLOWS IS RECOMMENDED FOR AIRCRAFT ON WHICH THE BASIC ISSUE OR REVISION 01 OF THIS SERVICE BULLETIN WAS DONE : Ifthe all the ODU lanyards in the aircraft (entrance area,forward lavatory, cabin area and aft lavatory) have been inspected and replaced as applicable, no further action is required . Otherwise do this Service Bulletin , only to the areas that were not previously inspected . 

### 1. PLANNING INFORMATION A. Effectivity BD-700-1A11 aircraft. For the aircraft Serial No. and STC No., refer to the table that follows: Aircraft TCCASTC FAA STC EASA STC Serial No. 9130 C-LSA05-030/D 

### - 9140 SA05-60 Issue 1 ST02 140NY Dated 2005-1 0-1 4 9149 SA05-60 Issue 1 ST02 140NY Dated 2005-10-14

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. e> 2012 • 2013 Bombardier Inc. All rights reserved

**Lea~et**

**.** Challenger, Global, are registered trademarks of Bombardier Inc. or its subsidiaries.

- - 

### -

-

-

Basic Issue: Oct 22/2012 Revision 02: May 28/2013 

# 700-1A11-35-009 Page 1 of 13Aircraft Serial No. 

### 9152 9154 9156 9157 9161 9166 9168 9170 9172 9174 9176 9178 9180 9182 9186 9188 9190 9192 9198 9204 9206 9207 9209 9212 BOMBARDIER 

# GLOBAL 5000 MODEL BD-700-1A11 (BD-700) TCCASTC FAA STC SA05-60 Issue 1 ST02140NY SA05-60 Issue 1 ST02140NY SA05-60 Issue 1 ST02140NY SA05-60 Issue 1 ST02140NY SA05-60 Issue 1 ST02140NY SA05-60 Issue 1 ST02140NY Dated 14 Oct 2005 C-LSA06-014/D 

### - C-LSA05-382/D 

### - SA05-60 Issue 1 ST02140NY C-LSA06-032/D 

### - SA05-60 Issue 1 ST02140NY Dated 2005-10-14 C-LSA06-0198/D 

### - SA05-60 Issue 1 ST02140NY Dated 2005-10-14 SA05-60 Issue 1 ST02140NY Dated 2005-10-14 C-LSA06-281/D 

## - C-LSA06-256/D 

## - C-LSA06-182/D 

## - SA05-60 Issue 1 ST02140NY Dated 2005-10-14 C-LSA06-335/D 

### - C-LSA06-336/D 

## - SA05-60 Issue 1 ST02140NY Dated 2005-10-14 SA05-60 Issue 1 ST02140NY Dated 2005-10-14 SA05-60 Issue 1 ST02140NY Dated 2005-10-14 SA05-60 Issue 1 ST02140NY Dated 2005-10-14 EASA STC



### -

-

-



### -

-



## - EASA.IM.A.S.01605 EASA.IM.A.S.01607 Issue 1



## - EASA.IM.A.S.01828



### -

-

- EASA.IM.A.S.02515 EASA.IM.A.S.02247 EASA.IM.A.S.02098



### -

- EASA.IM .A.S.02176 EASA.IM.A.S.02101



### -

-



### -

-

Basic Issue: Oct 22/2012 Revision 02: May 28/2013 

# 700-1A11-35-009 Page 2 of 13

### Aircraft Serial No. 

### 9216 9217 9221 9224 9226 9227 9231 9233 9241 9243 9245 9249 9255 9257 9261 9263 9265 9269 9271 BOMBARDIER 

# GLOBAL 5000 MODEL BD-700-1A11 (BD-700) 

### TCCASTC FAASTC SA05-60 Issue 1 ST02140NY Dated 2005-10-14 SA05-60 Issue 1 ST02140NY Dated 2005-10-14 SA05-60 Issue 1 ST02140NY Dated 2005-10-14 SA05-60 Issue 1 ST02140NY Dated 2005-10-14 C-LSA07-161/D 

## - SA05-60 Issue 1 ST02140NY SA05-60 Issue 1 ST02140NY C-LSA07-162/D ST02140NY Dated 2005-10-14 SA05-60 Issue 1 ST02140NY Dated 2005-10-14 C-LSA07-278/D 

### - SA05-60 Issue 1 ST02140NY Dated 2005-10-14 C-LSA07-229/D 

### - SA05-60 Issue 1 ST02140NY Dated 2005-10-14 C-LSA08-019/D 

### - SA05-60 Issue 1 ST02140NY Dated 2005-10-14 SA05-60 Issue 1 ST02033NY Dated 2004-12-02 SA05-60 Issue 1 ST02140NY C-LSA08-065/D 

## - Issue 1 SA05-60 Issue 1 ST02140NY Dated 2005-10-14 

### EASASTC



### -



## -

-



## -

-

-

-

- EASA.IM.A.S.02602 EASA.IM.A.S.02603



### - EASA.IM.A.S.02641



### -

-

-

-

- EASA.IM .A.S.02779



## -

Basic Issue: Oct 22/2012 Revision 02: May 28/2013 

# 700-1A11-35-009 Page 3 of 13Aircraft Serial No. 

### 9273 9282 9285 9288 9293 9295 9298 9301 9305 9311 9315 9318 9321 9325 9328 9330 BOMBARDIER 

# GLOBAL 5000 MODEL BD-700-1A11 (BD-700) TCCASTC FAA STC SA05-60 Issue 1 ST02140NY Dated 2005-10-14 SA05-60 Issue 1 ST02140NY Dated 2005-10-14 SA05-60 Issue 1 ST02140NY Dated 2005-10-14 SA05-60 Issue 1 ST02140NY Dated 2005-10-14 SA05-60 Issue 1 ST02140NY Dated 2005-10-14 SA05-60 Issue 1 ST02140NY Dated 2005-10-14 SA05-60 Issue 1 ST02140NY Dated 2005-10-14 SA05-60 Issue 1 ST02140NY Dated 2005-10-14 SA05-60 Issue 1 ST02140NY Dated 2005-10-14 SA05-60 Issue 1 ST02140NY Dated 2005-10-14 SA05-60 Issue 1 ST02140NY Dated 2005-10-14 SA05-60 Issue 1 ST02140NY Dated 2005-10-14 SA05-60 Issue 1 ST02140NY Dated 2005-10-14 SA05-60 Issue 1 ST02140NY Dated 2005-10-14 SA05-60 Issue 1 ST02140NY Dated 2005-10-14 SA05-60 Issue 1 ST02140NY Dated 2005-10-14 EASASTC EASA.IM.A.S.02795



## -

-



## - EASA.IM.A.S.03100



### -



## - EASA.IM.A.S.03105



### - EASA.IM.A.S.03121 EASA.IM.A.S.03162 EASA.IM.A.S.03164



## -

-

-



## -

Basic Issue: Oct 22/2012 Revision 02: May 28/2013 

# 700-1A11-35-009 Page 4 of 13BOMBARDIER 

# GLOBALsooo MODEL BD-700-1A11 (BD-700) Aircraft TCCA STC FAA STC EASA STC Serial No. 

### 9334 SA05-60 Issue 1 ST02140NY Dated 10028579 2005-10-14 

### 9337 SA05-60 Issue 1 ST02140NY Dated 

### - 2005-10-14 

### 9340 SA05-60 Issue 1 ST02140NY Dated 

## - 2005-10-14 

### 9343 SA05-60 Issue 1 ST02140NY Dated 10027762 Rev. 1 2005-10-14 

### 9346 SA05-60 Issue 1 ST02140NY Dated 

### - 2005-10-14 

### 9353 SA05-60 Issue 1 ST02140NY Dated 10028361 2005-10-14 All other subsequent BD-700-1A11 aircraft are scheduled for the modification in completion prior to delivery. NOTES: 1. The instructions given in this Service Bulletin are only applicable to the systems and parts installed at the time ofdelivery ofthe aircraft or as changed by Bombardier Aerospace Service Bulletin(s). Before you do this bulletin, examine all STC, STA or equivalent action changes to make sure that this bulletin can be completed . B. Reason During an interior evaluation ofthe Global 5000, it was discovered that the oxygen dispensing unit (ODU) has a length of lanyard that exceeds regulations. In an emergency, for certain individuals with specific physical characteristics and sitting in certain seat locations, the individual can don the oxygen mask and potentially not activate the oxygen flow. Ifoxygen supply is not provided, the individual may experience loss ofconsciousness within 8 - 10 seconds, and within four minutes, a fatal injury can occur. This Service Bulletin replaces the existing ODU lanyards with lanyards ofthe correct length that meets the safety requirements. C. Description This Service Bulletin gives instructions to:

- Get access to oxygen masks in the ODU,

- Replace the existing 17 or 20 inch (43.2 or 50.8 ems) lanyards with a 11 inch (27.9 ems) lanyard, and

- Install the oxygen masks in the ODU.

Basic Issue: Oct 22/2012 Revision 02: May 28/2013 

# 700-1A11-35-009 Page 5 of 13BOMBARDIER 

# GLOBAL 5000 MODEL BD-700-1A11 (BD-700) 

### D. Compliance Recommended in less than 750 flight hours or at the next "C" check, whichever comes first. NOTE: This Service Bulletin is subject to an Airworthiness Directive (AD), CF-2012-31, issued by Transport Canada. 

### E. Approval The technical content ofthis Service Bulletin has been approved under the authority ofthe Transport Canada Civil Aviation (TCCA). NOTES: 1. The technical content ofthis Service Bulletin is accepted by the FAA under the Canada/USA bilateral Aviation Safety Agreement. 2. The technical content ofthis Service Bulletin is accepted by EASA underthe Canada/EU bilateral Aviation Safety Agreement. 

### F. Manpower NOTES: 1. The man-hours given are estimates to help you schedule the tasks given in this bulletin. The estimates 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 estimates, refer to SB 700-1A11-00-002. 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 labor estimates 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. 16 man-hours are necessary to do this modification. The labor required to do this Service Bulletin is at no cost if: (i) the work is done at Bombardier Business Aviation Services (BBAS) orAuthorized Service Facilities (ASF), and (ii) this Service Bulletin is scheduled in less than 750 flight hours or at the next C check, whichever comes first, from its release date (Basic Issue).

Basic Issue: Oct 22/2012 Revision 02: May 28/2013 

# 700-1A11-35-009 Page 6 of 13BOMBARDIER 

# GLOBAL 5000 MODEL BD-700-1A11 (BD-700) G. Material - Cost and Availability No kit is necessary to do this modification. The materials necessary to do this modification are listed in Paragraph 3.C. The parts necessary to do this modification are listed in Paragraph 3.B. 736 parts were available when this Service Bulletin was released . Sufficient parts will be kept for the estimated amount of orders. The parts can be purchased by sending a purchase order to Bombardier Aerospace Parts Services, Montreal. These parts are available at no cost, if a no-charge purchase order is sent to Bombardier Aerospace in less than 15 months, from this Service Bulletin release date (Basic Issue) . During or after the above free period , Smart Parts Plus does not pay for the parts. H. Tooling No equipment or special tools are necessary. 

### I. Weight and Balance No change. J. Electrical Load Data No change. K. References

- Transport Canada (TC) STC SA05-60, Issue 1 (not attached) .

- ACS - NAI , Modification Data Summary H1 0800 Rev. NC (not attached).

- Bombardier Instructions for Continued Airworthiness (IFCA) , BAS67058005 (attached) .

- BombardierAerospace , Drawing BAS67039070, Rev. A.

- Global 5000 BD-700-1A11 Aircraft Maintenance Manual, Chapters 6, 24 and 35. L. Other Publications Affected None. M. Equivalent Service Bulletin None.

Basic Issue: Oct 22/2012 Revision 02: May 28/2013 

# 700-1A11-35-009 Page 7 of 13BOMBARDIER 

# GLOBAL 5000 MODEL BD-700-1 A11 (BD-700) 

### 2. ACCOMPLISHMENT INSTRUCTIONS NOTES: 1. All TASKs given in the procedures that follow are from the Global 5000 BD-700-1A11 Aircraft Maintenance Manual (AMM) unless otherwise specified . 2. All references made to zones, access panels and/or doors, are from the Global 5000 BD-700-1A11 Aircraft Maintenance Manual (AMM) , Chapter 6. A. Aircraft Setup (1) Obey all oxygen system safety precautions. Refer to TASK 35-00-00-910-801. (2) Obey all electrical/electronic safety precautions. Refer to TASK 24-00-00-91 0-801 . (3) In the flight compartment, on the PASSENGER OXYGEN control panel , set the CLOSED/NORMAL/OVERRIDE SELECTOR to CLOSED. B. Modification NOTE: All the oxygen masks will deploy at one time. (1) Use tape to secure the interior trim cover on the ODU cover to prevent the masks from dropping. Make a loop in the in the middle ofthe tape so that the ODU covers unlatching can be confirmed. (2) In the flight compartment, on the PASSENGER OXYGEN control panel , set the CLOSED/NORMAL/OVERRIDE SELECTOR to OVERRIDE and then CLOSED. NOTE : When the CLOSED/NORMAL/OVERRIDE SELECTOR is put in the OVERRIDE position , all the oxygen masks will drop from their ODU . The passenger oxygen system is pressurized. When you put the CLOSED/NORMAL/OVERRIDE SELECTOR to the CLOSED position , oxygen pressure is shutoff, and only residue pressure exists in the oxygen lines. (3) Carefully lower the two oxygen masks from the ODU. (4) In Fwd Lavatory Headliner (1 ODU), Entrance Headliner (2 ODU) and Aft Lavatory PSU (1 ODU) , remove and discard the existing oxygen mask lanyards, Part Nos. 8431564-503 or 8431564-505, from between the oxygen mask ring and manifold pin ring . (5) Install the new lanyards, Part No. 8431564-507. Refer to drawing BAS67039070, sheet 3, Item 30. (6) In cabin for each ODU 's, measure the length ofthe two lanyards and if they are not 11 ± 0.25 inches, remove and discard the existing oxygen mask lanyards, Part Nos. 8431564-503 or 8431564-505, from between the oxygen mask ring and manifold pin ring .

Basic Issue: Oct 22/2012 Revision 02: May 28/2013 

# 700-1A11-35-009 Page 8 of 13BOMBARDIER 

# GLOBAL 5000 MODEL BD-700-1A11 (BD-700) (7) Install the new lanyards, Part No. B431564-507. Refer to drawing BAS67039070, sheet 3, Item 30. (8) Re-identify reworked ODU boxes as "Post SB 700-1A11-35-009" by ink stamp, per best shop practices. It is permissible to re-identify reworked ODU's with "Post SB 700-1A11-35-009" identification inside of box if more accessible. (9) Install the interior trim cover on the ODU box cover and install the cover. 

### C. Testing None. 

### D. Close-out Remove all tools, equipment and unwanted materials from the aircraft. 

### E. 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 ofour 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 No kits required. 

### B. Parts The part that follows is necessary to do this Service Bulletin and is available from Bombardier Aerospace Parts Services, Montreal: NEW QTY ITEM USED INSTRUCTIONS - PART NO. PART NO. DISPOSITION B431564-507 32 Lanyard B431564-503 

### & Discard Assembly B431564-505 NOTE: The part number for the item listed above is subject to change without revision to this Service Bulletin . In case ofdiscrepancy between this list and any other list, the Illustrated Parts Catalog prevails and shall be used to determine the latest part number.

Basic Issue: Oct 22/2012 Revision 02: May 28/2013 

# 700-1A11-35-009 Page 9 of 13C. Material BOMBARDIER 

# GLOBAL 5000 MODEL BD-700-1A11 (BD-700) The material that follows, or equivalent, is necessary to do this Service Bulletin. It can be purchased from a local supplier. Bombardier Aerospace does not pay for this consumable.

DESCRIPTION PART SPECIFICATION QUANTITY SUPPLIER No./NAME (See Note) Tape, Masking 

## - - As Code:A Necessary NOTES: 1. Refer to the table that follows for each supplier's 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 ofthis 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
D. Publications No publications required.

Basic Issue: Oct 22/2012 Revision 02: May 28/2013 Code: A Commercially Available



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- LANYARD REPLACEMENT**~** '--

- **~** IBOMBARDIER BOI"'BAROIER 

### GLOBALSOOO CUSTOMER SERVICES BUSINESS AIRCRAFT 

### SERVICE BULLETIN EVALUATION FORM

(Your ideas will help us provide better bulletins) SERVICE BULLETIN: 700-1A11-35-009 ISSUE: Rev. 02 DATED: May 28/2013 TITLE: Modification - Passenger Oxygen System - Change Lanyard on Mask for Correct Length

In an effort to improve the quality of our technical communications, we are replacing the standard Service Bulletin Evaluation Form with an on-line Service Bulletin Survey and we are requesting your feedback. Please take a moment to fill out our easy on-line Service Bulletin survey: 

### http://csefeedback.aero.bombardier.comBOMBARDIER SOMBAR0/ £ 1'1 

### GLOBAL5000 CUSTOMER SERVICES BUSINESS AIRCRAFT 

## SERVICE BULLETIN INCORPORATION SHEET- "700-1A11-35-009" 0::: 

## z : Upon completion ofthe Service Bulletin, please fill-in, fax to



### ~ 0 • (514) 855-8798 or e-mail to Fracas at fracas.montreal@aero.bombardier.com 0:::(/) <( Cl) : 

### Ifyour aircraft is registered on CAMP and you are reporting to them,



### ~ **~** · please do notsend the incorporation sheetto Bombardier. Ifyour aircraft 0 

## => : is on another tracking system, please contact Bombardier to make a::1 Cl) : 

### arrangements for automated data submission. COMPLIED WITH Service Bulletin Rev. *Parts YES NO N/A Remarks/Reason Number Completed 700-1A11-35-009 02 

## 0 0 0 0 0 0 0 0 0 Actual hours to accomplish Service Bulletin: *NOTES: 1 . Where the Service Bulletin is divided into a number of parts (e.g., PARTS A, B, C, D, etc.) which can be carried out separately, indicate only those parts completed at this time. 2. For repetitive checks (usually PART A) only the initial check should be reported unless otherwise stated in the Service Bulletin. 3. When more than one part is carried out at the same time, each part should be reported . Aircraft Serial No. Airframe Hours: S.B. Incorporation date Facility Incorporating S.B. (dd/mm/yy) Aircraft Reg. No. Airframe Landings Service Order No.



### ------- Name --------- Signature Signature not required if sent by E-Mail Date (dd/mm/yy)

# 0~ Bombardier Business Aircraft Customer Services (BBACS) P.O. Box 6087, Station Centre-ville Montreal, Quebec, Canada H3C 3G9 Attention: Customer Support Department, Maintenance Engineering