# Bombardier Service Bulletin 604-34-065 Copy: U.S. DOT/FAA - Bombardier Service Bulletin (b) ("U.S. DOT/FAA - Bombardier Service Bulletin (b)"), 16 pages: PDF https://openairdocs.org/files/sha256/c3/1a/c31a2d939adc9ecab24c0df3e7aa4911f1115bc9aa3684b706e54392d7d268bb; text https://openairdocs.org/service-documents/bombardier/sb-604-34-065/file/c31a2d939adc.md. Rights: © Bombardier Inc. Filed by the FAA in regulations.gov docket FAA-2013-0332; AD 2013-22-05 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication. ## Details - Manufacturer: [Bombardier](https://openairdocs.org/service-documents/bombardier.md) - Type: Service bulletin (Service Bulletin) - Number: 604-34-065 - Latest revision known: 604-34-065, Revision 02, dated December 20, 2012 (OpenAirDocs) - Page: https://openairdocs.org/service-documents/bombardier/sb-604-34-065 ## ADs that cite it (1) (OpenAirDocs) Newest first, with the revision each names, as OpenAirDocs read it from the AD's text. - [AD 2013-22-05](https://openairdocs.org/ad/2013-22-05.md), effective Dec 5, 2013: Revisions 01 and 02 Also cited in [1 proposed AD](https://openairdocs.org/service-documents/bombardier/sb-604-34-065/proposed.md). ## Text (16 pages) Rights: © Bombardier Inc. Filed by the FAA in regulations.gov docket FAA-2013-0332; AD 2013-22-05 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication. Some pages are OCR from a scan. OCR can misread letters and numbers. Each page's text from the PDF; open the PDF at a page with #page=N. ### Page 1 604-34-065 Page 1 of 1 SERVICE BULLETIN REVISION TRANSMITTAL SHEET MODEL CL-600-2B16 Discard Revision 01 of this Service Bulletin dated Oct 15/2012 and the Information Sheet dated Oct 24/2012, and replace in its entirety with this Revision 02. Service Bulletin No. 604-34-065 Date of Basic Issue Jul 31/2012 Revision No. 01 Dated Oct 15 /2012 Revision No. 02 Dated Dec 20 /2012 For aircraft that incorporated Revision 01 of this Service Bulletin, 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. For aircraft that have the Basic Issue incorporated, Revision 02 of this Service Bulletin must be entered in the log book in order to comply with the Airworthiness Directive. This revision is issued to: 1. Remove the note in Paragraph 1, to remove the dedicated campaign and incorporate the change related to the Information Sheet dated Oct 24/2012. 2. Add, in Paragraph 1.A ., Effectivity, NOTE 1. 3. Add a note in Paragraph 1.D., Complianc e, the TCCA Airworthiness Directive, CF-2012-30. 4. Remove the dedicated campaign information note in Paragraph 1.G., Material – Cost and Availability. 5. Change, in Paragraph 1.K., the Modsum 600-6331, to Rev. A-1. 6. Add, in Paragraph 1.K., the TCCA Airworthiness Directive, CF-2012-30. 7. Make miscellaneous minor changes, as necessary, with no change of context. ### Page 2 Basic Issue: Jul 31/2012 604-34-065 Revision 02: Dec 20/2012 Page 1 of 1 SERVICE BULLETIN SUMMARY This Service Bulletin is available at: www.cic.bombardier.com MODEL CL-600-2B16 ATA 34-11 NAVIGATION MODIFICATION – PITOT-STATIC AND TEMPERATURE SENSING SYSTEM – REPLACEMENT OF PITOT-STATIC VISUAL DRAIN BOTTLES TO LARGER CAPACITY BOTTLES The information below is provided for your reference. For full details, please see corresponding paragraph contained within this bulletin. RECOMMENDED SPECIFIED TIME COMPLIANCE COMPLIANCE TIME Within 24 months from this Service Bulletin release date (Basic Issue). EFFECTIVITY: A/C Serial No. 5301 to 5665 MANPOWER: 6.5 man-hours 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 or kits, please call Bombardier Aerospace Parts Services at: 514-855-2999 or 1-866-538-1247 ### Page 3 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. © 2012 Bombardier Inc. All rights reserved Challenger*, Global Express*, Global Express XRS*, Global 5000*, Learjet* are Trademarks of Bombardier Inc. Basic Issue: Jul 31/2012 604-34-065 Revision 02: Dec 20/2012 Page 1 of 11 SERVICE BULLETIN This Service Bulletin is available at: www.cic.bombardier.com MODEL CL-600-2B16 ATA 34-11 NAVIGATION MODIFICATION – PITOT-STATIC AND TEMPERATURE SENSING SYSTEM – REPLACEMENT OF PITOT-STATIC VISUAL DRAIN BOTTLES TO LARGER CAPACITY BOTTLES 1. PLANNING INFORMATION A. Effectivity CL-600-2B16 aircraft, Serial No. 5301 to 5665. NOTES: 1. If you have incorporated the Basic I ssue, you meet the intent of this Revision 02. If the Basic Issue was entered in the log book, you can enter Revision 02 in the aircraft log book without doing any physical changes to the aircraft. 2. 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). Before you do this bulletin, examine all STC, STA or equivalent action changes to make sure that this bulletin can be completed. B. Reason There is a possibility, when flying into adverse weather conditions, of water ingress in the pitot and static lines. The presence of water in the pitot and static lines could restrict the air passage which can result in fluctuating and incorrect flight display data for airspeed and altitude indications. This Service Bulletin replaces the current drain bottle assemblies related to the pitot and static lines with an improved design and larger capacity drain bottles. Replacement of the drain bottle assemblies will reduce incorrect flight display data for airspeed or altitude. ### Page 4 MODEL CL-600-2B16 Basic Issue: Jul 31/2012 604-34-065 Revision 02: Dec 20/2012 Page 2 of 11 C. Description This Service Bulletin gives instructions to: – Get access to the cockpit under floor, – Remove the existing drain bottles and fittings, – Install the new drain bottles and fittings, and – Do the necessary tests to make sure that the system operate(s) correctly. D. Compliance Recommended within 24 months from this Service Bulletin release date (Basic Issue). NOTE: This Service Bulletin is in reference to TCCA Airworthiness Directive, CF-2012-30. E. Approval The technical content of this 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 Service Bulletin is accepted by the FAA under the Canada/USA bilateral Aviation Safety Agreement. 2. The technical content of this Service Bulletin is accepted by the JAA and by EASA in accordance with established procedures. 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 604-00-002. 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. 6.5 man-hours are necessary to do this modification. Bombardier Aerospace does not pay for the labor to do this modification. ### Page 5 MODEL CL-600-2B16 Basic Issue: Jul 31/2012 604-34-065 Revision 02: Dec 20/2012 Page 3 of 11 G. Material - Cost and Availability Kit 605K34-027 is necessary to do this modification. Only the U.S. domestic price is shown: KIT NO. PRICE 605K34-027 $2,939.30 The above price can change. For the price outside of the U.S., refer to the last applicable Spare Parts Price Catalog. This data is also available from Bombardier Business Aviation Services (BBAS) at the addresses shown in the catalog. Bombardier Aerospace does not pay for the kit to do this modification. Smart Parts Plus pays for the kit for up to 12 months from Service Bulletin distribution date (basic issue). H. Tooling GSE REFERENCE NO. PART NO. DESCRIPTION GSE 24−00−24 - Tag, Circuit Breaker Commercially Available - Torque Wrench NOTES: 1. Refer to the CL-604 Illustrated Tool and Equipment Manual to make sure that you use the correct equipment configuration. 2. Refer to the Introduction of the publication listed in NOTE 1 for acceptable GSE equivalents. I. Weight and Balance No change. J. Electrical Load Data No change. K. References – Bombardier Aerospace, Modification Summary, 600-6258, Rev. B1. – Bombardier Aerospace, Modifica tion Summary, 600-6331, Rev. A-1. – Bombardier Aerospace, Restriction and/or Special Instruction (RSI), C-4082, Rev. A. – Bombardier Aerospace, Standard Pr actices Manual (SPM), Chapter 20. – Bombardier Aerospace, Structural Repair Manual (SRM), Chapter 51. – CL-604 Aircraft Maintenance Manual (AMM), Chapters 6, 24, 34 and 51. – TCCA Airworthiness Directive, CF-2012-30. L. Other Publications Affected – CL-604 Aircraft Illustrated Part s Catalog (AIPC), Chapter 34. ### Page 6 MODEL CL-600-2B16 Basic Issue: Jul 31/2012 604-34-065 Revision 02: Dec 20/2012 Page 4 of 11 M. Equivalent Service Bulletins For the CL-601 Challenger aircraft, use SB 601-0617. For the CL-605 Challenger aircraft, use SB 605-34-027. 2. ACCOMPLISHMENT INSTRUCTIONS NOTES: 1. All TASKs given in the procedures that follow are from the CL-604 Aircraft Maintenance Manual unless otherwise specified. 2. All references made to zones, access panels and/or doors, are from the CL-604 Aircraft Maintenance Manual, Chapter 6. A. Aircraft Setup (1) Obey all electrical/electronic safety precautions. Refer to TASK 24-00-00-910-801. (2) Open and tag the circuit breakers that follow: CB PANEL CB NO. NAME ZONE CBP−2 A14 HEATERS R PITOT 222 CBP−2 A15 HEATERS R STATIC 222 CBP−3 B4 HEATERS L PITOT 221 CBP−3 B6 HEATERS PITOT STBY 221 CBP−3 B7 HEATERS L STATIC 221 (3) Open the main avionics-compartment door. B. Modification – Replacem ent of ADC Drain Bottles NOTE: Refer to the Standard Practice Manual for torquing of plumbing line fittings. Refer to TASK 20−22−00−910−801. (1) When applicable, remove the necessary equipments to gain access to the drain bottles. (2) In the forward avionics compartment, r eplace the drain bottles for the pitot and static lines of the ADCs as follows: (a) With a wrench, remove the old drain bottles (1) and (2) attached to the pitot line and the static line of the ADCs. Refer to Figure 1. (b) On the pitot line of the ADCs, remove and discard the old tee fittings (3), retain the existing washers. Refer to Figure 1. (c) Install the new tee fittings, Part No. AS1033W040406 (3) with the retained washers on the pitot line of the ADCs. Refer to Figure 1. (d) Install an adaptor assembly, Part No. 5QM5A06-07 (4) to the tee fittings, Part No. AS1033W040406 (3). Refer to Figure 1. (e) Do the pitot line P1 contamination removal. Refer to TASK 34-11-01-100-801. ### Page 7 MODEL CL-600-2B16 Basic Issue: Jul 31/2012 604-34-065 Revision 02: Dec 20/2012 Page 5 of 11 (f) Do the pitot line P2 contamination removal. Refer to TASK 34-11-01-100-802. (g) Do the pilot’s S1/S2 static line contamination removal. Refer to TASK 34-11-01-100-803. (h) Do the copilot’s S1/S2 static line contamination removal. Refer to TASK 34-11-01-100-804. (i) Install the new drain bottle Part No. 50036-001 (1) and (2) to the adaptor assembly, Part No. 5QM5A06-07 (4). Refer to Figure 1. NOTE: Make sure that a click sound is heard when you push the drain bottles (1) and (2) into the adaptor assemblies (4). (3) Remove and replace the old drain bottle bracket with a new drain bottle bracket, Part No. 604-52268-1 or -1S (6) as shown in Figure 2. NOTES: 1. Ensure that the new bracket is prepared for bonding as per SPM MM 51-24-05-100-801. 2. Use the appropriate size HiLite fasteners as supplied in the kit. It is permissible to use the supplied oversized HiLite fasteners if necessary. 3. When rivets are removed, re-install appropriate diameter rivets supplied in kit. Refer to Structural Repair Manual, Chapter, 51- 42-08 and Chapter, 51-42-36. 4. When installing the bracket, make sure to have an edge distance no lower than 1.3 times the fastener diameter on any of the 4 holes. 5. Refer to the SPM MM 20-22-00- 910-801 for torquing of plumbing line fittings. (4) Once bracket is installed, perform a visual inspection using 10X magnification and make sure that there are no visible cracks on the bracket around the fasteners. (5) Do the pitot Line P3 Contamination re moval. Refer to TASK 34-11-04-100-801. (6) Install the new drain bottle, Part No. 50036-002 (5) to the adapter, Part No. 5QM5A06-07 (10). Refer to Figure 2. (7) Remove the tags and close the circuit breakers that follow: CB PANEL CB NO. NAME ZONE CBP−2 A14 HEATERS R PITOT 222 CBP−2 A15 HEATERS R STATIC 222 CBP−3 B4 HEATERS L PITOT 221 CBP−3 B6 HEATERS PITOT STBY 221 CBP−3 B7 HEATERS L STATIC 221 ### Page 8 MODEL CL-600-2B16 Basic Issue: Jul 31/2012 604-34-065 Revision 02: Dec 20/2012 Page 6 of 11 C. Testing (1) Do a Leak Test of the P1 and Pilot’s S1 and copilot’s S2 Systems. Refer to TASK 34-11-00-790-801. (2) Do a Leak Test of the P2 and Pilot’s S2 and copilot’s S1 Systems. Refer to TASK 34-11-00-790-802. (3) Do a Leak Test of the P3 and S3 syst ems. Refer to TASK 34-11-00-790-803. D. Close-out (1) Remove all tools, equipment and unwanted materials from the aircraft. (2) Close the main avionics compartment door. 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 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 ### Page 9 MODEL CL-600-2B16 Basic Issue: Jul 31/2012 604-34-065 Revision 02: Dec 20/2012 Page 7 of 11 3. MATERIAL INFORMATION A. Kit Kit 605K34-027 is necessary to do this Service Bulletin and contains the parts that follow: NEW PART NO. QTY ITEM USED PART NO. INSTRUCTIONS - DISPOSITION 50036-001 4 Drain Bottle 50029-001 or 50030-001 or 9035000 or 9035001 or 9435014 or 9435015 Discard Old 50036-002 1 Drain Bottle 50030-001 or 50034-002 or 9435014 or 9035001 Discard Old 5QM5A06-07 5 Adapter - New 604-52268-1S 1 Bracket 604-52260-5 Discard Old AN924-6D 1 Nut AN924-4D Discard Old AS1033W040406 2 Tee AN783D6 Discard Old AS1037W0604 1 Adapter AN783D4 Discard Old B0203013-3 2 Kaynar Nut - New B0203038-3 2 Kaynar Nut (over size) - New B0206001AG6-3 2 Hi Lite Fastener - New HST110AG-6-3 2 Hi Lite Fastener (over size) - New MS20470AD4-6 2 Rivets - New MS20470AD5-7 2 Rivets - New NAS1149D0963J 1 Washer AN960JD716 Discard Old NOTES: 1. In case of discrepancy between this list and the “Service Bulletin Kit Parts List” contained in the respective kit, then the latter list prevails. 2. 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. ### Page 10 MODEL CL-600-2B16 Basic Issue: Jul 31/2012 604-34-065 Revision 02: Dec 20/2012 Page 8 of 11 B. Parts No additional parts required. C. Material The materials that follow, or equivalent, are necessary to do this Service Bulletin. These can be purchased from a local supplier. Bombardier Aerospace does not pay for these consumables. DESCRIPTION PART No./NAME SPECIFICATION QUANTITY SUPPLIER (See Note) Alodine 1200S MIL-C-81706 As Necessary Code: A Sealant CT: 1/2 hours Pro-Seal 870 A-1/2 MIL-PRF- 81733 Type I-1/2, Class 1, Grade A As Necessary Code: A Primer - MIL-P-23377F Type I As Necessary Code: B Solvent Diestone DLS or Diestone HFP or HFE-71DA - As Necessary Code: C 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 Se rvice 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. ### Page 11 MODEL CL-600-2B16 Basic Issue: Jul 31/2012 604-34-065 Revision 02: Dec 20/2012 Page 9 of 11 SUPPLIERS ADDRESSES BY CODES Code: A PRC-Desoto International 5430 San Fernando Road, PO Box 1800, Glendale, CA, 91209 Tel.: 1-800-228-5635 or 1-818-240-2060 Fax.: 1-818-549-7790 www.ppg.com/coatings/aerospace/ Code: B JacksonLea 1715 Conover Blvd East Conover NC 28613 U.S.A. Tel.: 1-800-438-6880 Tel.: (828) 464-1376 E-mail: cherman@jacksonlea.com Code: C MagChem Inc 1271 Ampere Boucherville, Que. Canada, J4B 5Z5 Tel.: (450) 655-1344 www.magchem.com D. Publications No publications required. ### Page 12 (OCR) CHALLENGÉR 604 MODEL CL-600-2B16 ADC 2 ADC 1 (REF) (REF) STATIC LINE (REF) PITOT LINE (REF) PITOT LINE STATIC LINE (REF) (REF) G ITEMS LIST Drain Bottle Part No. 1 50030-001 or 9035001 (Pre-Mod) 50036-001 (Post-Mod) Drain Bottle Part No. 2 50029-001 or 9035000 (Pre-Mod) 50036-001 (Post-Mod) 3 AN804-4D (Pre-Mod) Tee Fitting Part No. AS1033W040406 (Post-Mod) 4 Adapter Part No. 5QM5A06-07 (Post-Mod) PRE-MOD POST-MOD PRE-MOD POST-MOD Drawings and data contained herein are the exclusive property of Bombardler Inc. and their copy or reproduction by any third party s strictly forbidden. Pitot Static Drain Replacement Figure 1 Basic Issue: Jul 31/2012 604-34-065 Revision 02: Dec 20/2012 Page 10 of 11 ### Page 13 (OCR) CHÄLLENGÉŘ 604 MODEL CL-600-2B16 ITEMS LIST Drain Bottle Part No. 5 50030-001 or 50034-002 (Pre-Mod) 50036-002 (Post-Mod) 6 Bracket Part No. 604-5268-1 Post-Mod) Install the appropriate 7 Adapter Part No. AS1037W0604 (Post-Mod) size rivets Part No. MS20470AD4-6 or MS20470AD5-7, 8 Washer Part No. AN960JD716 (Pre-Mod) Washer Part No. NAS1149D0963J (Post-Mod) according to the holes size. supplied in the kit 9 Nut Part No. AN924-4D (Pre-Mod) 10 Nut Part No. AN924-6D (Post-Mod) Install the appropriate 10 Adapter Part No. 5QM5A06-07 (Post-Mod) size Hi Lite fasteners, Part No. B0206001AG6-3 or HST110AG-6-3, and nuts, Part No. B0203013-3 or B0203038-3, supplied in the kit according to the holes size. Drawings and data contained hereln are the exclusive property of Bombardler Inc. and thelr copy or reproduction by any third party is strictly forbidden. Pitot Static Drain Replacement Figure 2 Basic Issue: Jul 31/2012 604-34-065 Revision 02: Dec 20/2012 Page 11 of 11 ### Page 14 SERVICE BULLETIN EVALUATION FORM (Your ideas will help us provide better bulletins) SERVICE BULLETIN: 604-34-065 ISSUE: Rev. 02 DATED: Dec 20/2012 TITLE: Modification – Pitot-Static and Temperature Sensing System – Replacement of Pitot-Static Visual Drain Bottles to Larger Capacity Bottles 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.com ### Page 15 SERVICE BULLETIN INCORPORATION SHEET – “604-34-065” BOMBARDIER SUBMISSION Upon completion of the 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 604-34-065 02 - - - - - - - Actual hours to accomplish Service Bulletin: 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. * 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 ### Page 16 -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- Bombardier Business Aircraft Customer Services (BBACS) P.O. Box 6087, Station Centre-ville Montreal, Québec, Canada H3C 3G9 Attention: Customer Support Department, Maintenance Engineering -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain, except the copies of manufacturers’ service documents, which belong to their rights holders.