Basic Issue: Mar 29/2012 700-1A11-52-019

Page 1 of 1 

SERVICE BULLETIN SUMMARY 

This Service Bulletin is available at: 

www.cic.bombardier.com

MODEL BD-700-1A11 (BD-700)

ATA 52-41 

DOORS 

MODIFICATION – AFT EQUIPMENT-COMPARTMENT DOOR – 

MODIFICATION TO PREVENT FUEL INGRESS INTO THE AFT EQUIPMENT BAY 

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. 9127 to 9383, 9389 to 9400, 9404 to 9431 and 9998 

MANPOWER: 8 man-hours 

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
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: Mar 29/2012 700-1A11-52-019

Page 1 of 20 

SERVICE BULLETIN 

This Service Bulletin is available at: 

www.cic.bombardier.com 

MODEL BD-700-1A11 (BD-700)

ATA 52-41 

DOORS 

MODIFICATION – AFT EQUIPMENT-COMPARTMENT DOOR – 

MODIFICATION TO PREVENT FUEL INGRESS INTO THE AFT EQUIPMENT BAY 

1. PLANNING INFORMATION 

A. Effectivity 

BD-700-1A11 aircraft, Serial No. 9127 to 9383, 9389 to 9400, 9404 to 9431 

and 9998. 

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). 

Before you do this bulletin, examine all STC, STA or equivalent 

action changes to make sure that this bulletin can be completed. 

B. Reason 

Several cases have been reported where fluid from the aft fuel tank drain was 

found to run back along the center line of the aircraft and entered the aft 

equipment bay via the slot in the door latch mechanism. 

This Service Bulletin provides instructions to install a cover to the aft equipment 

bay door latch mechanism. This modification will reduce the risk of drain mast 

fluids from entering and accumulating in the aft equipment bay. 

C. Description 

This Service Bulletin gives instructions to: 

– Remove the aft equipment-compartment door, 

– Do the modification to the door, 

– Install the door, and 

– Do the necessary tests to make sure that the system operates correctly. 
MODEL BD-700-1A11 (BD-700) 

Basic Issue: Mar 29/2012 700-1A11-52-019

Page 2 of 20 

D. Compliance 

Recommended – Within 24 months from this Service Bulletin release date 

(Basic Issue). 

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. 

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. 

8 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) 

or Authorized Service Facilities (ASF), and 

(ii) this Service Bulletin is scheduled in less than 24 months from its 

release date (Basic Issue). 
MODEL BD-700-1A11 (BD-700) 

Basic Issue: Mar 29/2012 700-1A11-52-019

Page 3 of 20 

G. Material - Cost and Availability 

Kit 700K52-042 is necessary to do this modification. Only the U.S. domestic 

price is shown: 

KIT NO. PRICE 

700K52-042 $720.00 

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. 

75 kits were available when this Service Bulletin was released. Sufficient kits will 

be kept for the estimated amount of orders. 

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). 

During or after the above free period, Smart Parts Plus does not pay for the kit. 

H. Tooling 

No equipment or special tools are necessary. 

I. Weight and Balance 

WEIGHT MOMENT 

+0.45 pounds (0.204 kg) +411.7 pound-inches (4.74 kg m) 

J. Electrical Load Data 

No change. 

K. References 

– Bombardier Aerospace, Modification Summary, 700T97601, Rev. E. 

– Bombardier Aerospace, Kit Drawing KGS991-9040, Rev. D. 

– Global 5000 BD-700 Aircraft Maintenance Manual, Chapters 6 and 52. 

– Global 5000 BD-700 Structural Repair Manual (SRM), Chapter 51. 

L. Other Publications Affected 

None. 
MODEL BD-700-1A11 (BD-700) 

Basic Issue: Mar 29/2012 700-1A11-52-019

Page 4 of 20 

M. Equivalent Service Bulletins 

– For the Global Express and XRS BD-700-1A10 (BD-700) aircraft, use 

SB 700-52-042. 

– For the Global 6000 BD-700-1A10 (BD-700) aircraft, use SB 700-52-6007. 

– For the Global 5000 BD-700-1A11 (BD-700) Featuring Global Vision Flight 

Deck aircraft, use SB 700-52-5007. 

2. ACCOMPLISHMENT INSTRUCTIONS 

NOTES: 1. All TASKs given in the procedures that follow are from the Global 5000 

BD-700 Aircraft Maintenance Manual unless otherwise specified. 

2. All references made to zones, access panels and/or doors, are from the 

Global 5000 BD-700 Aircraft Maintenance Manual, Chapter 6. 

A. Aircraft Setup 

Remove the aft equipment –compartment door. Refer to TASK 52-41-00-000-801. 

B. Modification 

(1) Do the modification to the door as follows (refer to drawing KGS991-9040): 

(a) Position the packer, item 5 to the door skin panel and mark off the 

position of the five holes to suit the installation of five rivets, item 11 and 

two off holes for the installation of the bolt, item 9. 

(b) Use hole pattern and drill five holes diameter 0.128 in (3.25 mm) and two 

holes diameter 0.1535 in (3.89 mm) through packer, item 5 and door skin. 

(c) Remove existing two off rivets and replace with rivets item 11. Refer to 

note R4 and to SRM Chapter 51-42-08. 

(d) Wet assemble the packer to the door skin with five rivets, item 11. Refer 

to SRM Chapters 51-23-04 and 51-42-08. 

(e) Remove existing six fasteners and open holes to diameter 0.1535 in 

(3.89 mm). 

(f) Temporarily center position the cover, item 3 and packers, item 4 about 

aft equipment-compartment door latch system. 

(g) Use the six holes in the door structure and mark off the position on cover 

and packers. Drill eight holes diameter 0.1535 in (3.89 mm) in the cover 

and packers, item 4. 

(h) Assemble cover and packers with A/nuts, items 7 and 8, and rivets, item 

10. Refer to SRM Chapter 51-42-08. 

NOTE: Verify the minimum clearance of 0.010 in (0.25 mm) between the 

latch assy and packers. Trim if necessary. Apply primer and 

topcoat to the reworked area. 

(i) Use bolts, item 9 and wet install the cover/packers assembly to the aft 

equipment – compartment door. 
MODEL BD-700-1A11 (BD-700) 

Basic Issue: Mar 29/2012 700-1A11-52-019

Page 5 of 20 

(j) Use PR 1422 and do the sealing around mating edge of cover assy and 

door area. Refer to SRM Chapter 51-23-04. 

NOTE: Perform a visual inspection of the seal. 

(2) Install the aft equipment-compartment door. Refer to TASK 52-41-00-400-801. 

(3) Do an operational test of the door. Refer to TASK 52-41-00-710-801. 

C. Close-out 

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 700K52-042 is necessary to do this Service Bulletin and contains the parts that 

follow: 

NEW 

PART NO. 

QTY ITEM USED 

PART NO. 

INSTRUCTIONS - 

DISPOSITION 

B0205001AD3-7A 16 Rivet - - 

B0205001AD4-4A 7 Rivet - - 

KGS991-9040-5 2 Packer - - 

KGS991-9040-7 1 Packer - - 

KGS991-9040-9 1 Blister Cover - - 

MS21075-06N 6 A/Nut Double 

Lug, Floating 

- - 

NAS1789C06 2 A/Nut Single 

Lug, Floating 

- - 

NAS7401-6 8 Bolt, CSK Head - - 

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. 
MODEL BD-700-1A11 (BD-700) 

Basic Issue: Mar 29/2012 700-1A11-52-019

Page 6 of 20 

B. Parts 

No 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) 

Polyurethane 

Topcoat 

WHITE 

17875 

STD595 As 

Necessary 

Code: A 

Sealant PR1422 BAMS552-002 As 

Necessary 

Code: A 

Primer 10P4-2 Green. BAMS 565-001 

Grade A 

As 

Necessary 

Code: B 

Solvent Diestone DLS 

or 

Diestone HFP 

or 

HFE-71DA

- As 

Necessary 

Code: C 

Cloth, Lint Free - - As 

necessary 

Code: D 

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 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. 
MODEL BD-700-1A11 (BD-700) 

Basic Issue: Mar 29/2012 700-1A11-52-019

Page 7 of 20 

SUPPLIERS ADDRESSES BY CODES 

Code: A 

PRC-Desoto International 

5676 Timberlea Blvd. 

Mississauga, Ontario 

Canada, L4W 4M6 

Tel.: (905) 629-7999 

Code: B 

Akzo Nobel Aerospace Coatings Inc 

1 East Water Street, Waukegan 

Il, 60085 

Tel.:1-847-623-4200 

Fax: 847-625-3200 

Code: C 

MagChem Inc 

1271 Ampere 

Boucherville, Que. 

Canada, J4B 5Z5 

Tel.: (450) 655-1344 

or 

3M Product Information Center 

3M Center, 

Building 0304-01-01 

St. Paul, MN 55144-1000 

U.S.A. 

Tel.: 1-888-364-3577 

Fax: 1-800-713-6329 

Code: D 

Commercially Available 

D. Publications 

No publications required. 
MODEL BD-700-1A11 (BD-700) 

PL KGS991-9040– Kit – GX – Aft Equipment Bay Door Latch – Lock Sealing 

(Sheet 1 of 4, Rev. D) 

Basic Issue: Mar 29/2012 700-1A11-52-019

Page 8 of 20 
MODEL BD-700-1A11 (BD-700) 

PL KGS991-9040– Kit – GX – Aft Equipment Bay Door Latch – Lock Sealing 

(Sheet 2 of 4, Rev. D) 

Basic Issue: Mar 29/2012 700-1A11-52-019

Page 9 of 20 
MODEL BD-700-1A11 (BD-700) 

PL KGS991-9040– Kit – GX – Aft Equipment Bay Door Latch – Lock Sealing 

(Sheet 3 of 4, Rev. D) 

Basic Issue: Mar 29/2012 700-1A11-52-019

 Page 10 of 20 
MODEL BD-700-1A11 (BD-700) 

PL KGS991-9040– Kit – GX – Aft Equipment Bay Door Latch – Lock Sealing 

(Sheet 4 of 4, Rev. D) 

Basic Issue: Mar 29/2012 700-1A11-52-019

Page 11 of 20 
KGS991-9040– Kit – GX – Aft Equipment Bay Door Latch – Lock Sealing 

(Sheet 1 of 5, Rev. D) 

Basic Issue: Mar 29/2012 700-1A11-52-019

Page 12 of 20
KGS991-9040– Kit – GX – Aft Equipment Bay Door Latch – Lock Sealing 

(Sheet 1 of 5, Rev. D - continued) 

Basic Issue: Mar 29/2012 700-1A11-52-019

Page 13 of 20
KGS991-9040– Kit – GX – Aft Equipment Bay Door Latch – Lock Sealing 

(Sheet 2 of 5, Rev. D) 

Basic Issue: Mar 29/2012 700-1A11-52-019

Page 14 of 20
KGS991-9040– Kit – GX – Aft Equipment Bay Door Latch – Lock Sealing 

(Sheet 2 of 5, Rev. D - continued) 

Basic Issue: Mar 29/2012 700-1A11-52-019

Page 15 of 20
KGS991-9040– Kit – GX – Aft Equipment Bay Door Latch – Lock Sealing 

(Sheet 3 of 5, Rev. D) 

Basic Issue: Mar 29/2012 700-1A11-52-019

Page 16 of 20
KGS991-9040– Kit – GX – Aft Equipment Bay Door Latch – Lock Sealing 

(Sheet 3 of 5, Rev. D - continued) 

Basic Issue: Mar 29/2012 700-1A11-52-019

Page 17 of 20
KGS991-9040– Kit – GX – Aft Equipment Bay Door Latch – Lock Sealing 

(Sheet 4 of 5, Rev. D) 

Basic Issue: Mar 29/2012 700-1A11-52-019

Page 18 of 20
KGS991-9040– Kit – GX – Aft Equipment Bay Door Latch – Lock Sealing 

(Sheet 4 of 5, Rev. D - continued) 

Basic Issue: Mar 29/2012 700-1A11-52-019

Page 19 of 20
KGS991-9040– Kit – GX – Aft Equipment Bay Door Latch – Lock Sealing 

(Sheet 5 of 5, Rev. D) 

Basic Issue: Mar 29/2012 700-1A11-52-019

Page 20 of 20
SERVICE BULLETIN EVALUATION FORM 

(Your ideas will help us provide better bulletins) 

SERVICE BULLETIN: 700-1A11-52-019 ISSUE: Basic DATED: Mar 29/2011 

TITLE: Modification – Aft Equipment-Compartment Door – Modification to Prevent Fuel Ingress 

into the Aft Equipment Bay 

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
SERVICE BULLETIN INCORPORATION SHEET – 

“700-1A11-52-019” 

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 

700-1A11-52-019 Basic - 

- - - 

- - - 

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 

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

Bombardier Business Aircraft Customer Services (BBACS) 

P.O. Box 6087, Station Centre-ville 

Montreal, Québec, Canada H3C 3G9 

Attention: Customer Support Department, Maintenance Engineering 

-- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- -- --