Apr 24/2013 

# A700-26-010 Page 1 of 1 

# ALERT SERVICE BULLETIN INFORMATION SHEET
MODEL BD-700-1A10 (BD-700)

ATA 26-21
FIRE PROTECTION

SPECIAL CHECK/REPLACEMENT – FIRE EXTINGUISING SYSTEM – INSPECTION OF CHECK TEE, PART NO 446651

Service Bulletin No.: A 700-26-010 Issue: Basic Dated: A pr 18/2013 The following data is supplied for information only. No revision to the Service Bulletin is necessar y

. Keep this Information Sheet with subject Service Bulletin.

This Alert Service Bulletin Information Sheet is issued to inform operators of a typographical error in Section (3).(b) of Paragraph 2.C., PART B: Inspection and/or Replacement of Check Tee Fitting(s) and is corrected to read as follows: 2.C. PART B: Inspection and/or Replacement of Check Tee Fitting(s)

. (3) Carry out the accomplishment instructions in the attached Kidde Aerospace and Defense Service Bulletin, 446651-26-494. a) If the check tee fitting failed the depth check, remove and replace the check tee fitting. Refer to TASKS 26-21-45-000-801 and 26-21-45-400-801. b) If the check tee fitting passed to depth check, re-identify the check tee fitting in accordance with Kidde Aerospace and Defense Service Bulletin, 446651-26-494 and go to step 2.C.(4).Basic Issue: Apr 18/2013 

# A700-26-010 Page 1 of 1



# ALERT SERVICE BULLETIN SUMMARY

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

### MODEL BD-700-1A10 (BD-700)

ATA 26-21
FIRE PROTECTION

SPECIAL CHECK/REPLACEMENT – FIRE EXTINGUISHING SYSTEM – INSPECTION OF CHECK TEE, PART NO. 446651 The information below is provided for y our reference. For full details, please see corresponding paragraph contained within this bulletin. 

# ALERT

SPECIFIED TIME COMPLIANCE 

## COMPLIANCE TIME Within 100 flight hours from this Service Bulletin release date (Basic Issue)

EFFECTIVITY: A/C Serial No. 9001 to 9312, 9314 to 9380 and 9384 to 9429

MANPOWER: Refer to Paragraph 1.F. CONTINUED AIRWORTHINESS (CAW) FLEET CAMPAIGN YES NO

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 YES NO
PREREQUISITE SERVICE BULLETINS: N/A

To place an order for parts, please call Bombardier Aerospace Parts Services at:
514-855-2999 or 1-866-538-1247Refer 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 Bombardi er Inc. and/or its affiliates and may not be reproduced or copi ed in any form or by any means without the prior written consent of Bombardier Inc. and/or its affiliates. © 2013 Bombardier Inc. All rights reserved Learjet, Challenger, Global, are registered trademarks of Bombardier Inc. or its subsidiaries. Basic Issue: Apr 18/2013 

# A700-26-010 Page 1 of 10 

# ALERT SERVICE BULLETIN

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

### MODEL BD-700-1A10 (BD-700)

ATA 26-21
FIRE PROTECTION

SPECIAL CHECK/REPLACEMENT – FIRE EXTINGUISHING SYSTEM – INSPECTION OF CHECK TEE, PART NO. 446651



### 1. PLANNING INFORMATION
NOTE : Before performing PART B, make sure your schedule allows a minimum of 24 hours downtime, should a replacem ent check tee fitting be required. A. Effectivity BD-700-1A10 aircraft, Serial No. 9001 to 9312, 9314 to 9380 and 9384 to 9429

. All other subsequent BD-700-1A10 aircraft are scheduled for the modification in production. NOTE : The instructions given in this Alert 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). Before you do this bulletin, examine all STC, STA or equivalent action changes to make sure that this bulletin can be completed.
B. Reason This Alert Service Bulletin introduces an inspection of the three check tee fittings installed in the engine and APU fire exti nguishing system. It was reported that a check tee fitting was found with two balls insta lled. Only one ball is installed in the body of the check tee fitting. If two balls ar e installed in the body of the check tee fitting, the flow of the fire extinguishing agent is partially re stricted. This restriction can cause insufficient concentration of fire extinguishing agent necessary to suppress an engine or APU fire.MODEL BD-700-1A10 (BD-700)

Basic Issue: Apr 18/2013 

# A700-26-010 Page 2 of 10 C. Description This Alert Service Bulletin gives instructions in PART A to:

–Open the aft equipment-c ompartment door (311BB),

–Visually check the serial numbers, and

–Close the aft equipment-compartment door (311BB). This Alert Service Bulletin gives instructions in PART B to:

–Disconnect one of the two discharge lines from check tee fitting,

–Measure the depth to the ball in the body of the check tee fitting,

–Replace the check tee fitting if it fails the depth check, or re-identify the check tee fitting if it passes the depth check,

–Connect the discharge line to the check tee fitting and

–Close the aft equipment-compartment door (311BB). D. Compliance This Alert Service Bulletin is reco mmended within 100 flight hours from this Service Bulletin release date (Basic Issue). NOTES : 1. The issuance of an Airworthiness Directive to incorporate this Alert Service Bulletin is expected to be released by Transport Canada Civil Aviation.
2. This Alert Service Bulletin is in reference to Advisory Wire AW700-26-0424. E. Approval The technical content of this Alert Service Bulletin has been approved under the authority of Transport Canada Civil Aviation (TCCA) Design Approval Organization (DAO) No. DAO #93-Q-02. NOTES : 1. The technical content of this Alert Service Bulletin is accepted by the FAA under the Canada/USA bilateral Aviation Safety Agreement. 2. The technical content of this Alert Service Bulletin is accepted by EASA in accordance with established procedures.MODEL BD-700-1A10 (BD-700)

Basic Issue: Apr 18/2013 

# A700-26-010 Page 3 of 10 F. Manpower NOTES : 1. The man-hours given are estimates to help you schedule the tasks given in this bulletin. The estimate s 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 t he manpower estimates, refer to SB 700-00-002. 2. This Alert 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 Alert Service Bulletin. PART A : 1 man-hour is necessary to do the vis ual inspection of the serial numbers on three check tee fittings. PART B : for suspect serial numbers, 1 man-hour per check tee fitting, is necessary to do the depth check and re-identify or replace check tee fitting. A maximum of four man-hours is permitted if all three check t ee fittings are visually and depth checked, and re-identified or replaced. The labor required to do this Alert Service Bulletin is at no cost if: (i) the work is done at Bombardier Business Aviation Services (BBAS) or Authorized Service Facilities (ASF), and (ii) this Alert Service Bulletin is scheduled in less than 100 flight hours from its release date (Basic Issue). G. Material - Cost and Availability No kit is necessary to do this special c heck/replacement. For material data, refer to Paragraph 3. The parts in Paragraph 3.B. are necessary to do this special check/replacement. For the parts necessary to do this Alert Se rvice Bulletin, refer to Kidde Aerospace and Defense, Service Bulletin, 446651-26-494 and Paragraph 3.B. of this Service Bulletin. Sufficient parts will be kept for the es timated amount of defective parts. The check tee fitting(s) is available at no cost if a no-charge purchase order is sent to Bombardier Aerospace in less t han 100 flight hours from this Alert Service Bulletin release date (Basic Issue).MODEL BD-700-1A10 (BD-700)

Basic Issue: Apr 18/2013 

# A700-26-010 Page 4 of 10 Return the defective units for disposal to Bombardier Aerospace at one of the two addresses given below: Learjet – Core Returns 8219 West Irving, Bldg 9, Dock 9, Wichita, KS 67209 USA
or Distribution Centre Frankfurt – Core Returns Bombardier Aerospace Germany GmbH Hans-Boeckler-Strasse 9 GROSS-GERAU Hesse 64521 Germany

Refer to your Material Return Author ization (MRA) form to find the applicable return address. During or after the above free period, Smart Parts Plus does not pay for the parts. H. Tooling The equipment and tools listed below are necessary to do this inspection and modification:

GSE REFERENCE NO. PART NO. DESCRIPTION 20X-10-01 S4933959-501 Tag, Circuit Breaker - - Wrench, Torque 0 to 25 lbf in (0 to 2.82 Nm) - - Wrench, Torque 0 to 50 lbf ft (0 to 68 Nm) I. Weight and Balance No change.
J. Electrical Load Data No change.MODEL BD-700-1A10 (BD-700)

Basic Issue: Apr 18/2013 

# A700-26-010 Page 5 of 10 K. References

–Transport Canada Civil Aviation Airworthiness Directive is pending.

–Bombardier Aerospace, Restriction and/or Special Instruction (RSI), C-01620, Rev. - - 1.

–Kidde Aerospace & Defense, Service Bulletin 446651-26-494 (attached).

–Advisory Wire AW700-26-0424.

–Global Express BD-700-1A10 Aircraft Maintenance Manual (AMM), Chapters 6, 24 and 26.

–Global Express BD-700-1A10 Aircraft I llustrated Parts Catalog (AIPC), Chapter 26.

–Global Express BD-700-1A10 Illustrat ed Tool and Equipment Manual (ITEM), Chapter 20.

–Global Express XRS BD-700-1A10 Aircraft Maintenance Manual (AMM), Chapters 6, 24 and 26.

–Global Express XRS BD-700-1A10 Aircra ft Illustrated Parts Catalog (AIPC), Chapter 26.

–Global Express XRS BD-700-1A10 Illu strated Tool and Equipment Manual (ITEM), Chapter 20.

–Bombardier Aerospace, Standard Pr actices Manual (SPM), Chapter 20.
L. Other Publications Affected None. M. Equivalent Service Bulletins

–For the Global 5000 BD-700-1A11 airc raft, use Alert SB A700-1A11-26-003.

–For the Global 6000 BD-700-1A10 aircraft, use Alert SB A700-26-6002.

–For the Global 5000 BD-700-1A11 Featuri ng Global Vision Flight Deck aircraft, use Alert SB A700-26-5002.MODEL BD-700-1A10 (BD-700)

Basic Issue: Apr 18/2013 

# A700-26-010 Page 6 of 10 

### 2. ACCOMPLISHMENT INSTRUCTIONS
NOTES : 1. All TASKs given in the procedures that follow are from the Global Express or Global Express XRS 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 Express or Global Ex press XRS BD-700-1A10, Aircraft Maintenance Manual (AMM), Chapter 6. A. Aircraft Setup (1) Obey all the electrical/electronic safety precautions. Refer to TASK 24-00-00-901-801. (2) Set the circuit breakers that follo w to OUT (on aircraft pre SB 700-24-045) or LOCKED (on aircraft, Serial No. 9123 and subsequent or aircraft post SB 700-24-045) (refer to TASK 24-00-00-863-801):

SYSTEM NAME CIRCUIT BREAKER NAME BUS NAME
FIRE APU FIRE HANDLE BATT FIRE L ENG FIRE HANDLE BATT FIRE R ENG FIRE HANDLE BATT (3) Open and tag the circuit breakers that follow:

LOCATION CB NO. NAME ZONE
DCPC A1 FIREX CH A 130 DCPC A2 FIREX CH B 130 (4) Open the aft equipment-c ompartment door (311BB).
B. PART A: Serial Number Verification (1) Inspect and record the serial numbers on the two engines and one APU check tee fittings, Part No. 446651.

NOTE : For location of the three check tee fittings, refer to the AIPC Chapter 26-21-45. (2) If the recorded serial number(s) are 062 to 070, 117 to 133, 3728 to 3731, 3733 to 3760 and 3762 to 3776, then do Paragraph 2.C. PART B of this Alert Service Bulletin.

NOTE : Before performing PART B, make sure your schedule allows a minimum of 24 hours downtime, should a replacement check tee fitting be required.MODEL BD-700-1A10 (BD-700)

Basic Issue: Apr 18/2013 

# A700-26-010 Page 7 of 10 (3) If the recorded numbers are not on the list, then you have met the intent of this Alert Service Bulletin. Go to Paragraph 2.E. C. PART B: Inspection and/or Replacement of Check Tee Fitting(s) CAUTION : USE TWO WRENCHES WHEN YOU REMOVE/TORQUE THE HOSES/TUBES. USE ONE WRENCH TO HOLD THE FITTING, AND THE OTHER WRENCH TO LOOSEN/TORQUE THE COUPLING NUT. IF YOU DO NOT DO THIS, YOU CAN CAUSE DAMAGE TO THE COMPONENTS. (1) Disconnect the coupling nut on one of t he two discharge lines at the check tee fitting. (2) Carefully move the discharge line to the side of the check tee fitting. If necessary, loosen the screw(s) that secures the discharge line clamp(s) to the aircraft structure. (3) Carry out the accomplishment instructions in the attached Kidde Aerospace and Defense Service Bulletin, 446651-26-494. (a) If the check tee fitting failed the depth check, remove and replace the check tee fitting. Refer to T ASKS 26-21-45-000-801 and 26-21-45-400-801. (b) If the check tee fitting passed the dept h check, re-identify the check tee fitting in accordance with Kidde Aerospace and Defense Service Bulletin, 446651-26-494 and go to step 2.B.(4). (4) Apply sealant to the threads of the check tee fitting.

CAUTION : USE TWO WRENCHES WHEN YOU REMOVE/TORQUE THE HOSES/TUBES. USE ONE WRENCH TO HOLD THE FITTING, AND THE OTHER WRENCH TO LOOSEN/TORQUE THE COUPLING NUT. IF YOU DO NOT DO THIS, YOU CAN CAUSE DAMAGE TO THE COMPONENTS. (5) Connect the coupling nut to the discharge line to the check tee fitting. Torque the coupling nut between 30 to 35.83 lbf ft (40.68 to 48.59 Nm). Refer to SPM TASK 20-21-00-910-801. (6) If loosened, torque the screw(s) that se cures the fire-extinguishing discharge line to the aircraft structure between 10 to 13 lbf in (1.13 to 1.46 Nm). Refer to SPM, TASK 20-21-00-910-801.MODEL BD-700-1A10 (BD-700)

Basic Issue: Apr 18/2013 

# A700-26-010 Page 8 of 10 D. Testing No testing required.
E. Close-out (1) Set the circuit breakers that follow to IN (refer to TASK 24-00-00-863-802):

SYSTEM NAME CIRCUIT BREAKER NAME BUS NAME
FIRE APU FIRE HANDLE BATT FIRE L ENG FIRE HANDLE BATT FIRE R ENG FIRE HANDLE BATT (2) Remove the tags and close the circuit breakers that follow:

LOCATION CB NO. NAME ZONE
DCPC A1 FIREX CH A 130 DCPC A2 FIREX CH B 130 (3) Remove all tools, equipment and unwanted materials from the aircraft. (4) Close the aft equipment compartment door 311BB. F. Recording You can do each PART of this Alert Service Bulletin independently. When any PART of this Alert 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.comMODEL BD-700-1A10 (BD-700)

Basic Issue: Apr 18/2013 

# A700-26-010 Page 9 of 10 

### 3. MATERIAL INFORMATION

A. Kit No kits required.
B. Parts The parts that follow may be necessary to do this Alert Service Bulletin and are available from Bombardier Aero space Parts Services, Montreal:

NEW PART NO. QTY ITEM USED PART NO. INSTRUCTIONS - DISPOSITION
446651 3 (Note 2) Check Tee 446651 Refer to Paragraph 1.G.
NOTES : 1. The part number for the item listed above is subject to change without revision to this Alert Service Bulletin. In case of discrepancy between this list and any other list, the Illustrated Parts Catalog prevails and shall be used to determine the latest part number. 2. A maximum of three check tee fittings may be required for each aircraft. 3. The part listed in this table is also listed the Kidde Aerospace and Defense Service Bulletin, 446651-26-494.MODEL BD-700-1A10 (BD-700)

Basic Issue: Apr 18/2013 

# A700-26-010 Page 10 of 10 C. Material The materials that follow, or equivalent, are necessary to do this Alert Service Bulletin. They can be purchased from a local supplier. Bombardier Aerospace does not pay for these consumables.

DESCRIPTION PART No./NAME SPECIFICATION QUANTITY SUPPLIER (See Note) Coating, Epoxy, Clear - MIL-C-22750 As Necessary for PART B Code: A

Compound, Sealing, Pipe and Joint

Thread - TT-S-1732 As Necessary for PART B Code: A

Ink, Black,

Marking - A-A-208 Type IV As Necessary for PART B Code: A

Stamp, Rubber - - As Necessary for PART B Code: A

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 of this Alert 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 Commercially Available

D. Publications No publications required.

### SERVICE BULLETIN EVALUATION FORM (Your ideas will help us provide better bulletins)

SERVICE BULLETIN: A700-26-010 ISSUE: Basic DATED: Apr 18/2013

TITLE: Special Check/Replacement – Fire Extinguish ing System – Inspection of Check Tee, Part No. 446651

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. Pl ease take a moment to fill out our easy on-line Service Bulletin survey:



### http://csefeedback.aero.bombardier.com

### ALERT SERVICE BULLETIN INCO RPORATION SHEET – “A700-26-010”BOMBARDIERSUBMISSION Upon completion of the Alert Service Bulletin, please fill-in, fax to (514) 855-8798 or e-mail to Fracas at fracas.montreal@aero.bombardier.com
If your aircraft is registered on CAMP and you are reporting to them, please do not send the incorporation sheet to Bombardier. If your aircraft is on another tracking system, please contact Bombardier to make arrangements for automated data submission.

COMPLIED WITH Service Bulletin Number Rev. * Parts Completed YES NO N/A Remarks/Reason

A700-26-010 Basic PART A
“ “ PART B

- - -

Actual hours to accomplish Service Bulletin:

1. Where the Alert 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 Alert Service Bulletin. * NOTES :

3. When more than one part is carried out at the same time, each part should be reported.

Aircraft Serial No. Aircraft Reg. No. Airframe Hours: Airframe Landings S.B. Incorporation date Service Order No. (dd/mm/yy) Facility Incorporating S.B.
Name Signature Date (dd/mm/yy) Signature not required if sent by E-Mail-- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- --



### Bombardier Business Aircraft Customer Services (BBACS) P.O. Box 6087, Station Centre-ville Montreal, Québec, Canada H3C 3G9

Attention : Customer Support Department, Maintenance Engineering

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