On this page
ADs that cite it · 1
Newest first, with the revision each names, as OpenAirDocs read it from the AD’s text: check it against the AD.
Also cited in 1 proposed AD.
Text · 27
From the PDF’s text layer: layout, tables and figures are lost. The PDF is the document. © Bombardier Inc. Filed by the FAA in regulations.gov docket FAA-2019-0019; AD 2019-12-02 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.
Query with SQL
duckdb -csv -c "SELECT p.page, p.text_source, p.text, f.rights_holder, f.license FROM 'https://openairdocs.org/data/latest/service_document_file_page.parquet' p JOIN 'https://openairdocs.org/data/latest/service_document_file.parquet' f USING (file_sha256) WHERE p.file_sha256 = 'cff157df4b3f3c066531b9956969eeebb5517fe0e0355577a4fcf08a51daa059' ORDER BY p.page"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT p.page, p.text_source, p.text, f.rights_holder, f.license FROM 'https://openairdocs.org/data/latest/service_document_file_page.parquet' p JOIN 'https://openairdocs.org/data/latest/service_document_file.parquet' f USING (file_sha256) WHERE p.file_sha256 = 'cff157df4b3f3c066531b9956969eeebb5517fe0e0355577a4fcf08a51daa059' ORDER BY p.page
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
Discard the Revision 01 of this Service Bulletin dated Aug 21/2018 and replace in its entirety with this Revision 02.
Service Bulletin No. 700−24−5014 Date of Basic Issue Apr 25/2018 Revision No. 01 Dated Aug 21/2018 Revision No. 02 Dated Sep 27/2018 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.B., the text from “VFG” to “High (VFG and Hydraulic)”.
2. Revise, in Paragraph 1.G., the policy to purchase the Kit No. 700K24−6014. Removed the “ordered during new aircraft warranty period” statement.
3. Revise, in Paragraph 1.H., the GSE Reference No. to 20X−10−01 for the Circuit Breaker Tag.
4. Revise, in Paragraph 2.B., the step 2.B.1.(C)(ii) to keep the clamp, wire spacer and washer for later installation (step (c)(vii)).
5. Change, in Paragraph 2.B., to revise the text from “VFG” to “Hydraulic” in the steps
2.B.1.(e)(i), 2.B.1.(e)(iii) and the illustration title.
6. Revise, in Paragraph 2.C., to add Notes in the steps 2.C.1.(d), 2.C.1.(f), 2.C.1.(h) and
2.C.1.(k)
7. Revise, in Paragraph 2.C., the step 2.C.1.(f), to install the new contacts with crimp adaptors.
SERVICE BULLETIN MODEL BD−700−1A11 (BD−700) 700−24−5014 Page 1 of 2
REVISION TRANSMITTAL SHEET
8. Revise, in Paragraph 3.C., to add the consumable.
9. Make miscellaneous minor changes, as necessary, with no change of context.
MODEL BD−700−1A11 (BD−700) 700−24−5014 Page 2 of 2
MODIFICATION - VARIABLE FREQUENCY GENERATOR (VFG) -
MODIFICATION TO THE VFG CABLES INSTALLATION, REAR FUSELAGE 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
RELIABILITY/DISPATCHABILITY/COST AVOIDANCE
COMPLIANCE TIME Within 24 months from this Service Bulletin release date (Basic Issue) EFFECTIVITY: A/C Serial No. 9386, 9401 and 9445 to 9831 MANPOWER: Up to 5 man−hours, Part A: 3 man−hours, Part B: 2 man−hours.
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 YES NO 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−700−1A11 (BD−700) ATA 24−00
ELECTRICAL POWER Basic Issue: Apr 25/2018 Revision 02: Sep 27/2018 700−24−5014 Page 1 of 1 This Service Bulletin is available at:
MODIFICATION - VARIABLE FREQUENCY GENERATOR (VFG) -
MODIFICATION TO THE VFG CABLES INSTALLATION, REAR FUSELAGE
1. 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. This Service Bulletin is covered by a dedicated schedule. Dedicated schedules are used to reserve and manage inventory due to limited availability of rotable stock, parts and/or kits. Parts are limited, therefore, advance part scheduling with our In−Service Implementation Team (ISIT) is recommended prior to a maintenance visit. Please contact your Regional Manager (RM), Field Service Representative (FSR) or Customer Service Representative (CSR) to schedule your aircraft as there is a limited availability. The parts will be allocated on a first come first serve basis.
For more information on dedicated schedules, refer to SB 700−00−5002.
A. Effectivity BD−700−1A11 aircraft, Serial No. 9386, 9401 and 9445 to 9831.
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).
SERVICE BULLETIN my.businessaircraft.bombardier.com MODEL BD−700−1A11 (BD−700) ATA 24−00
ELECTRICAL POWER 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: Apr 25/2018 Revision 02: Sep 27/2018 700−24−5014 Page 1 of 22 This Service Bulletin is available at:
B. Reason
1. Condition:
During visual inspection of the Aft Equipment Bay, low clearance condition between the High (VFG and Hydraulic) power feeder cables and adjacent hydraulic lines and/or fuel lines were found in several locations. This condition may lead to physical contact between the VFG Power feeder cables, hydraulic system lines and/or fuel lines. Physical contact or chaffing could result in deterioration of the hydraulic line and/or fuel line wall thickness and VFG power feeder cables insulation thickness.
2. Evidence:
To this date, evidence of physical contact between the VFG power feeder cables and the hydraulic lines and/or fuel lines was never reported.
3. Objective/Benefit:
The objective of this Service Bulletin, is to provide customers with instructions to achieve the minimum required clearance between the VFG power feeder cables and the adjacent hydraulic and/or fuel lines. This will eliminate the risk of physical contact/chaffing. The benefits to the operator are improved reliability and reduced maintenance cost.
C. Description This Service Bulletin gives instructions in PART A to:
− Get access to the aft compartment area , and − Modify the VFG power feeder cables routing as instructed in this Service Bulletin.
This Service Bulletin gives instructions in PART B to:
− Cut the wires at the connectors of the AC Hydraulic Motor Pump, − Modify the VFG harness routing to meet the installation and clearance requirements, and − Do the necessary tests to make sure that the AC Hydraulic Motor Pump operate(s) correctly.
D. Compliance Recommended within 24 months from 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.
MODEL BD−700−1A11 (BD−700) Basic Issue: Apr 25/2018 Revision 02: Sep 27/2018 700−24−5014 Page 2 of 22
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 EASA under the Canada/EU bilateral Aviation Safety Agreement.
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 700−00−5002.
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.
Up to 5 man−hours are necessary to do this modification and are divided as follows:
− 3 man−hours are necessary to do Part A of this Service Bulletin.
− 2 man−hours are necessary to do Part B of this Service Bulletin (if required), including the testing.
The labor required to do PART A of 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 in less than 24 months from its release date (Basic Issue).
The labor required to do PART B of 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 in less than 24 months from its release date (Basic Issue).
G. Material − Cost and Availability Kit 700K24−6014 is necessary to do this modification.
MODEL BD−700−1A11 (BD−700) Basic Issue: Apr 25/2018 Revision 02: Sep 27/2018 700−24−5014 Page 3 of 22
KIT NO. PRICE 700K24−6014 Please contact Bombardier Aerospace Parts Services, in Montreal, for delivery lead times and confirmation of prices.
This kit is available at no cost if:
− a no−charge purchase order is sent to Bombardier Aerospace in less than 24 months from this Service Bulletin release date (Basic Issue).
In addition to the kit shown above, the parts in Paragraph 3. may be necessary to do this PART B of this Service Bulletin.
These parts are available at no cost if:
− a no−charge purchase order is sent to Bombardier Aerospace in less than 24 months from this Service Bulletin release date (Basic Issue).
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 For those aircraft in new aircraft warranty at the time of Service Bulletin distribution, Smart Parts Plus does not pay for the kit at any time.
For those aircraft out of new aircraft warranty at the time of Service Bulletin distribution, Smart Parts Plus pays for the kit for up to 24 months from the Service Bulletin distribution date (Basic Issue).
This Service Bulletin is covered by a dedicated schedule. Dedicated schedules are used to reserve and manage inventory due to limited availability of rotable stock, parts and/or kits. Parts are limited, therefore, advance part scheduling with our In−Service Implementation Team (ISIT) is recommended prior to a maintenance visit. Please contact your Regional Manager (RM), Field Service Representative (FSR) or Customer Service Representative (CSR) to schedule your aircraft as there is a limited availability. The parts will be allocated on a first come first serve basis.
For more information on dedicated schedules, refer to SB 700−00−5002.
H. Tooling No equipment or special tools are necessary to do PART A of this Service Bulletin.
The equipment and tools listed below are necessary to do PART B of this Service Bulletin:
MODEL BD−700−1A11 (BD−700) Basic Issue: Apr 25/2018 Revision 02: Sep 27/2018 700−24−5014 Page 4 of 22
GSE REFERENCE NO. PART NO. DESCRIPTION 20X−10−01 S4933959−501 Tag, Circuit Breaker 20X−50−03 BM203 Terminator Tool Commercially Available M22520/23−01 or 400−B−1 Crimp Tool, Pneumatic Indent Commercially Available M22520/23−04 or 414DA−4N Die Assy. #4 Commercially Available M22520/23−11 or 4112 Positioner #4 Commercially Available M81969/29−03 or M81969/14−07 Insertion/Extraction Tool NOTES: 1. Refer to the Global 5000 Featuring Global Vision Flight Deck 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 GL 5000 GVFD, for acceptable GSE equivalents.
3. This list is provided for quick reference. In case of discrepancy between this list and the tools called in the SPM, WM, Chapter 20, then the tools called in the SPM, WM prevail. Other approved alternative tools are acceptable and can also be used.
I. Weight and Balance
WEIGHT MOMENT +0.15 pounds (0.068 kg) +134 pound−inches (1.543 kgm) J. Electrical Load Data No change.
K. References − Bombardier Aerospace, Modification Summary, R700T400679, Rev. D.
− Bombardier Aerospace, Restriction and/or Special Instruction (RSI), C−01698, Rev. A−1.
− Bombardier Aerospace, Kit Drawing KGC991−1558, Rev. B.
MODEL BD−700−1A11 (BD−700) Basic Issue: Apr 25/2018 Revision 02: Sep 27/2018 700−24−5014 Page 5 of 22
− Bombardier Aerospace, Standard Practices Manual (SPM), Chapter 20.
L. Other Publications Affected None.
M. Equivalent Service Bulletins For the Global Express and Global Express XRS BD−700−1A10 aircraft, use SB 700−24−089.
For the Global 5000 BD−700−1A11 aircraft, use SB 700−1A11−24−028.
For the Global 6000 BD−700−1A10 aircraft, use SB 700−24−6014.
2. ACCOMPLISHMENT INSTRUCTIONS NOTES: 1. All TASKs given in the procedures that follow are from the Global 5000 BD−700−1A11 Featuring Global Vision Flight Deck 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 Featuring Global Vision Flight Deck Aircraft Maintenance Manual (AMM), Chapter 6.
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.
(1) Obey all electrical/electronic safety precautions. Refer to AMM 24−00−00−910−801.
(2) Open the aft equipment−compartment door (311BB).
B. PART A − Modification − Installation of Additional Clamps NOTES: 1. 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.
2. If you find damaged cables that cannot be repaired per Standard Practices Manual (SPM), submit an SRPSA for an approved disposition.
MODEL BD−700−1A11 (BD−700) Basic Issue: Apr 25/2018 Revision 02: Sep 27/2018 700−24−5014 Page 6 of 22
(1) Do the modifications as follow, and as shown on Kit Drawing KGC991−1558:
(a) At the first location, View A, between FS945.50 and FS966.00, and between STGR 9L and 10L, refer to Figure 1, do as follows:
NOTE: Applicable to aircraft serial no. 9386, 9401 and 9445 to 9790 only.
(i) Install the Fairlead assembly, Part No. GD478−1056−1 (5), on the hydraulic lines.
(ii) Install the wire spacer, Part No. GD517−4349−1 (8), and the clamp, Part No. MS21919WDE15 (7), on the VFG cables.
(iii) Attach the fairlead assembly to the clamp with the bolt, Part No.
NAS6203−28 (3), the spacer, Part No. NAS43DD3−24FC (6), the washer, Part No. NAS1149D0316J (4) and the nut, Part No.
MS21042−3 (9), as shown in View A of kit drawing KGC991−1558.
(iv) Torque the bolt, 20 to 25 lbf in (2.26 to 2.82 Nm). Refer to SPM 20−21−00.
NOTES: 1. Make sure that you have a minimum clearance of 0.50 in (12.7 mm) between the VFG cables and the hydraulic lines, refer to SPM WM 20−12−00.
2. Make sure that there is no load generated on the hydraulic lines.
MODEL BD−700−1A11 (BD−700) Basic Issue: Apr 25/2018 Revision 02: Sep 27/2018 700−24−5014 Page 7 of 22
LOCATION NO.1 GSB2400_001 Modification of VFG Cables Installation Figure − 1
(b) At the second location, View B, between FS925.00 and FS945.50, on STGR 13L, refer to Figure 2, do as follows:
(i) Remove and discard the existing bolt that attaches the two clamps, Part No. MS21919WDE4 (if installed) and Part No. MS21919WDE15, on the standoff, Part No. B0204037AL−10W.
(ii) Keep the existing washer, Part No. AN960JD10L or NAS1149D0332J for later installation.
(iii) Install a new spacer, Part No. NAS43DD3−48FC (15), between the two clamps, and secure with a new bolt, Part No. NAS1801−3−18
(14) and previously removed washer, Part No. AN960JD10L or NAS1149D0332J on the standoff Part No. B0204037AL−10W, as shown on view B of Kit Drawing KGC991−1558.
(iv) Torque the new bolt, 20 to 25 lbf in (2.26 to 2.82 Nm). Refer to SPM 20−21−00.
NOTE: Make sure that you have a minimum clearance of 0.50 in
(12.7 mm) between the VFG cables and the fuel lines. Refer to SPM WM 20−12−00.
MODEL BD−700−1A11 (BD−700) Basic Issue: Apr 25/2018 Revision 02: Sep 27/2018 700−24−5014 Page 8 of 22
(c) At the third location, Detail F, at FS925.00 between STGR 15L and 16L, refer to Figure 2, do as follows:
(i) Remove the existing lower left generator run clamp, wire spacer and the attaching hardware from the APU FADEC run installation. Refer to Detail F, Pre mod.
(ii) Keep the clamp, wire spacer and washer for later installation (step
(c)(vii)) and discard the attaching bolt.
(iii) Install the removed APU FADEC run clamp with a new bolt Part No.
NAS1801−3−10 (26) and removed washer, Part No.
NAS1149D0332J, as shown in DETAIL F, Post Mod, on Kit Drawing KGC991−1558.
(iv) Torque the bolt, 20 to 25 lbf in (2.26 to 2.82 Nm). Refer to SPM 20−21−00.
(v) Remove the bolt, washer and spacer that holds the RAD/RAE/RBE, RAL/RBL/RBA and camera coax (if applicable) installation.
(vi) Discard the bolt and the spacer, keep the washer for later installation.
Refer to Detail F Pre mod.
(vii) Install the removed lower left generator run clamp and wire spacer on the RAD/RAE/RBE, RAL/RBL/RBA and camera coax (if applicable) installation with the new bolt, Part No. NAS1801−3−27 (28), removed washer Part No. NAS1149D0332J, new spacer, Part No. NAS 43DD3−48FC (29) and new spacer, Part No. NAS43DD3−16FC (30) as shown in DETAIL F, Post Mod, on Kit Drawing KGC991−1558.
(viii) Torque the bolt, 20 to 25 lbf in (2.26 to 2.82 Nm). Refer to SPM 20−21−00.
NOTE: Make sure that you have a minimum clearance of 0.50 in
(12.7 mm) between the VFG cables and the hydraulic lines.
Refer to SPM WM 20−12−00.
MODEL BD−700−1A11 (BD−700) Basic Issue: Apr 25/2018 Revision 02: Sep 27/2018 700−24−5014 Page 9 of 22