# Bombardier Service Bulletin 650-32-002

Copy: Revision 02 ("650-32-002 Rev02"), 16 pages: PDF https://openairdocs.org/files/sha256/8d/98/8d98d5f5e07f45782c1a642f90981f46fab4d4552cdb90aa6d6b5adb4071392d; text https://openairdocs.org/service-documents/bombardier/sb-650-32-002/file/8d98d5f5e07f.md. Rights: © Bombardier Inc. Filed by the FAA in regulations.gov docket FAA-2019-0186; AD 2019-15-01 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: 650-32-002
- Latest revision known: 650-32-002, Revision 02, dated May 10, 2018 (OpenAirDocs)
- Page: https://openairdocs.org/service-documents/bombardier/sb-650-32-002

## ADs that cite it (1) (OpenAirDocs)

Newest first, with the revision each names, as OpenAirDocs read it from the AD's text.

- [AD 2019-15-01](https://openairdocs.org/ad/2019-15-01.md), effective Sep 19, 2019: Revisions 01 and 02

Also cited in [1 proposed AD](https://openairdocs.org/service-documents/bombardier/sb-650-32-002/proposed.md).

## Text (16 pages)

Rights: © Bombardier Inc. Filed by the FAA in regulations.gov docket FAA-2019-0186; AD 2019-15-01 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication. Each page's text from the PDF; open the PDF at a page with #page=N.

### Page 1

Discard the Revision 01 of this Service Bulletin dated Feb 05/2018, and replace in its
entirety with this Revision 02.
Service Bulletin No. 650−32−002
Date of Basic Issue Dec 18/2017
Revision No. 01 Dated Feb 05/2018
Revision No. 02 Dated May 10/2018
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. Change, in Paragraph 2.A.(5), the AMM reference to, AMM 12−00−04−862−804.
2. Change, in Paragraph 2.C.(1), the AMM reference to, AMM 07−10−01−581−801.
3. Change, in Paragraph 2.C.(3), the AMM reference to, AMM 12−20−04−640−802.
4. Make miscellaneous minor changes, as necessary, with no change of context.
SERVICE BULLETIN
MODEL CL−600−2B16
650−32−002
Page 1 of 1
REVISION TRANSMITTAL SHEET

### Page 2

SPECIAL CHECK/MODIFICATION - EXTENSION AND RETRACTION, MAIN GEAR -
INSPECTION AND REPLACEMENT IF NECESSARY OF THE SIDE STAY ACTUATOR
SPLIT BALL BEARING
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
SPECIFIED TIME COMPLIANCE
COMPLIANCE TIME
Refer to Paragraph 1.D.
EFFECTIVITY: AC Serial No.6050 to 6091
MANPOWER: PART A: 0.5 man−hour, PART B: Up to 6.5 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 CL−600−2B16
ATA 32−32
LANDING GEAR
Basic Issue: Dec 18/2017
Revision 02: May 10/2018
650−32−002
Page 1 of 1
This Service Bulletin is available at:

### Page 3

SPECIAL CHECK/MODIFICATION - EXTENSION AND RETRACTION, MAIN GEAR -
INSPECTION AND REPLACEMENT IF NECESSARY OF THE SIDE STAY ACTUATOR
SPLIT BALL BEARING
1. PLANNING INFORMATION
NOTES:1 . Before you do this bulletin, examine all STC, STA or equivalent
action changes to make sure that this 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 650−00−002.
3. A completed Certificate of Scrap, for the removed split ball bearing, Part
No. 104467672, must be submitted within six weeks of the incorporation of
this Service Bulletin to Triumph Actuation Systems − Yakima.
Send a scanned copy of the completed Certificate of Scrap by e−mail to:
JLRoybal@triumphgroup.com and RFarabee@triumphgroup.com. Make
sure to include the Part Number and Serial Number of the top assembly in
the subject line of the e−mail.
If the Certificate of Scrap is not received within six weeks of the
incorporation of this Service Bulletin, the operator will be charged, by
Triumph Actuation Systems − Yakima, for the replacement split ball
bearing.
SERVICE BULLETIN
my.businessaircraft.bombardier.com
MODEL CL−600−2B16
ATA 32−32
LANDING GEAR
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.
 2017−2018 Bombardier Inc.  All rights reserved
Learjet, Challenger, Global, are registered trademarks of Bombardier Inc. or its subsidiaries.
Basic Issue: Dec 18/2017
Revision 02: May 10/2018
650−32−002
Page 1 of 12
This Service Bulletin is available at:

### Page 4

A. Effectivity
CL−600−2B16 aircraft Serial No. 6050 to 6091
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).
B. Reason
Bombardier Aerospace was informed by its supplier that some MLG side stay
actuators were supplied with a non conforming split ball bearing, Part No.
104467672. Material properties of the non conforming split ball bearings do not
meet the requirements of AMS4640H.
This Service Bulletin introduces a Special Check/Modification, that gives
instructions to verify the serial number of both side stay actuators installed on the
aircraft, and replace any non conforming split ball bearing if necessary. The
replacement of the discrepant split ball bearings will greatly reduce the risk of
bearing seizure. The benefits to the operator are improved reliability or reduced
maintenance costs.
C. Description
This Service Bulletin gives instructions in PART A to:
− Verify the serial number of the LEFT and RIGHT side stay actuator, and
− Take the appropriate action.
This Service Bulletin gives instructions in PART B to:
− Remove the existing discrepant split ball bearing,
− Install a new split ball bearing, and
− Do the necessary tests to make sure the system operates correctly.
D. Compliance
Recommended at or before 3750 flight cycles or within 48 months from Service
Bulletin release date (Basic Issue).
NOTES: 1. For units with more than 3350 flight cycles (since new) at the time of
Service Bulletin release date (Basic Issue), comply within 12 months
or 400 flight cycles, whichever comes first.
2. 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 get an approved disposition to complete this Service
Bulletin.
MODEL CL−600−2B16
Basic Issue: Dec 18/2017
Revision 02: May 10/2018
650−32−002
Page 2 of 12

### Page 5

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
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
650−00−002.
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 man−hours and should be considered for
planning purposes before you schedule this Service Bulletin.
0.5 man−hour is necessary to do PART A of this Special Check/Modification.
Bombardier Aerospace does not pay for the labor to do PART A of this Special
Check/Modification.
Up to 6.5 man−hours are necessary to do PART B of this Special
Check/Modification and are divided as follows:
− 2.5 man−hours per side, and
− 1.5 man−hours for the testing.
The labor required to do PART B of this Special Check/Modification 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 at or before 3750 flight cycles or within 48
months from Service Bulletin release date (Basic Issue).
NOTE: For units with more than 3350 flight cycles (since new) at the time of
Service Bulletin release date (Basic Issue), schedule within 12 months or
400 flight cycles, whichever comes first.
MODEL CL−600−2B16
Basic Issue: Dec 18/2017
Revision 02: May 10/2018
650−32−002
Page 3 of 12

### Page 6

G. Material − Cost and Availability
No kit is necessary to do PART B of this. For material data, refer to Paragraph 3.
For the part necessary to do PART B of this Special Check/Modification, refer to
Paragraph 3.B.
This part is available at no cost if:
− a no−charge purchase order is sent to Bombardier Aerospace in less than 48
months from this Service Bulletin release date (Basic Issue).
NOTE: For units with more than 3350 flight cycles (since new) at the time of
Service Bulletin release date (Basic Issue), purchase order must be sent
within 12 months from this Service Bulletin release 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 650−00−002.
A completed Certificate of Scrap, for the removed split ball bearing, Part No.
104467672, must be submitted within six weeks of the incorporation of this Service
Bulletin to Triumph Actuation Systems − Yakima.
Send a scanned copy of the completed Certificate of Scrap by e−mail to:
JLRoybal@triumphgroup.com and RFarabee@triumphgroup.com. Make sure to
include the Part Number and Serial Number of the top assembly in the subject line
of the e−mail.
If the Certificate of Scrap is not received within six weeks of the incorporation of this
Service Bulletin, the operator will be charged, by Triumph Actuation Systems −
Yakima, for the replacement split ball bearing.
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
During or after the above free period, Smart Parts Plus does not pay for the parts.
MODEL CL−600−2B16
Basic Issue: Dec 18/2017
Revision 02: May 10/2018
650−32−002
Page 4 of 12

### Page 7

H. Tooling
The equipment and tools listed below are necessary to do this Special
Check/Modification:
GSE REFERENCE NO. PART NO. DESCRIPTION
07−10−01 G600−070001−1 Pad, Jacking
07−10−02 02−1036−0111 Jack, Main Wing
07−10−03 02−1032−0111 Jack, Fwd Fuselage
07−10−06 03−5800−8000 Support, Rear Fuselage
10−10−09 W88F36 Wheel Chocks, Rubber
24−00−24 S4933959−501 Tag, Circuit Breaker
Commercially Available − Wrench, Torque
Refer to the Standard Practices Manual (SPM), Wiring Manual (WM), Chapter 20,
and the table that follows for the tools applicable to the wiring modification:
NOTES: 1. Refer to the CH 650 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 acceptable GSE
equivalents.
I. Weight and Balance
No change.
J. Electrical Load Data
No change.
K. References
− Bombardier Aerospace, Restriction and/or Special Instruction (RSI), C−4230,
Rev. A−1.
− Bombardier Aerospace, Standard Practices Manual (SPM), Chapter 20.
− Bombardier Aerospace, SB 650−00−02, Service Bulletin Description and Policy.
− Safran Landing Systems, Service Bulletin SB19010−32−003.
− Triumph Actuation Systems − Yakima, Service Bulletin 19011−32−1.
− Triumph Actuation Systems − Yakima, Certificate of Scrap (attached).
− CH 650 Aircraft Maintenance Manual (AMM), Chapters 6, 7, 24, 29 and 32.
MODEL CL−600−2B16
Basic Issue: Dec 18/2017
Revision 02: May 10/2018
650−32−002
Page 5 of 12

### Page 8

L. Other Publications Affected
None.
M. Equivalent Service Bulletin
For the Challenger 604, refer to Service Bulletin 604−32−029.
For the Challenger 605, refer to Service Bulletin 605−32−006.
2. ACCOMPLISHMENT INSTRUCTIONS
NOTE: All references made to zones, access panels and/or doors, are from the
CH 650 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) Obey all hydraulic safety precautions. Refer to AMM 29−00−00−910−801.
(3) Obey all hydraulic technical precautions. Refer to AMM 29−00−00−910−802.
(4) Obey all landing−gear safety precautions. Refer to AMM 32−00−00−910−801.
(5) Release the hydraulic pressure from system No. 3. Refer to
AMM 12−00−04−862−804.
(6) Open and tag the circuit breakers that follow:
CB PANEL CB NO. NAME ZONE
CBP−1 B8 HYD PUMP 3B 221
CBP−2 P2 HYD SYS AC PUMP CONT3B 222
CBP−2 A2 HYD PUMP 3A 222
CBP−2 G4 HYD SYS AC PUMP CONT3A 222
MODEL CL−600−2B16
Basic Issue: Dec 18/2017
Revision 02: May 10/2018
650−32−002
Page 6 of 12

### Page 9

B. PART A − Special Check
(1) Verify the serial number of the LEFT and RIGHT MLG side stay actuator
assemblies, Messier Bugatti Dowty (M−B−DT) Part No. 19010−103 and
19010−105 (Triumph Actuation Systems − Yakima (TASY), Part No.
19011−103 and 19011−105) for applicability.
(2) If the serial number is not listed in Table 1 or Table 2, no further action is
required.
(3) If the serial number is listed in Table 1 or Table 2, continue to Paragraph 2.C.
TABLE 1 - SIDE STAY ACTUATOR ASSEMBLY M-B-DT, PART NO.
19010-103 (TASY PART NO. 19011-103) IMPACTED SERIAL NO.
00113, 00120, 00177, 00183, 00184, 00203, 00204, 00226, 00263, 00274,
00297, 00314, 00315, 00322, 00323, 00541
TABLE 2 - SIDE STAY ACTUATOR ASSEMBLY M-B-DT, PART NO.
19010-105 (TASY PART NO. 19011-105) IMPACTED SERIAL NO.
00222, 00312G, 00620, 00688, 00693G, 00755, 00766, 00857, 00882,
01092, 01341, 01344, 01354, 01359, 001361 to 01363, 01367, 01368,
01370, 01371, 01373 to 01376, 01382 to 01384, 01387, 01388, 01393,
01397, 01401, 01403 to 01406, 01409 to 01411, 01413 to 01421, 01423 to
01425, 01429, 01430, 01435, 01440,01442, 01446
C. PART B− Modification − Replacement of the Split Ball Bearing
NOTE: 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 get an approved disposition to complete this Service Bulletin.
(1) Lift the complete aircraft with jacks. Refer to AMM 07−10−01−581−801.
(2) Replace the split ball bearing as follows, refer to Figure 1:
(a) Remove and discard the cotter pin (1). Refer to
SPM−MM 20−50−00−000−802.
(b) Remove and discard the nut (2).
(c) Remove and discard the washers (3) and (4).
(d) Support the MLG side brace actuator (7), per best shop practices.
(e) Remove the side brace pin assembly (6).
(f) Remove the split ball bearing, Part No. 104467672, from the rod end
assembly and discard.
(g) Install the new split ball bearing, Part No. 104467672, in the rod end
assembly. Make sure that the witness marks on the bearing faces are
matched together.
MODEL CL−600−2B16
Basic Issue: Dec 18/2017
Revision 02: May 10/2018
650−32−002
Page 7 of 12

### Page 10

(h) Apply a layer of grease on the side brace pin assembly (6).
(i) Install the side brace pin assembly (6) through the main fitting.
NOTE: Make sure the flat areas on the side brace pin assembly (6) line
up with the flat areas in the lock plate (5).
(j) Hold the head of the side brace pin assembly (6) in position to prevent
rotation and forward −and−aft movement.
(k) Install the new washers (3) and (4).
(l) Install the new nut (2).
(m) Torque the nut (2) from 20 to 40 lb ft (27.12 to 54.23 Nm). Refer to
SPM−MM 20−21−00−910−801.
(n) Install the new cotter pin (1). Refer to SPM−MM 20−50−00−400−802.
(3) Lubricate the spherical bearing. Refer to AMM  12−20−04−640−802.
(4) Identify the reworked Side Stay Actuator with the Service Bulletin identifier
number (19011−32−1) with permanent ink per best shop practices. Refer to
Figure 2.
(5) Apply one coat of polyurethane clear coat over the ink marking per best shop
practices. Refer to Figure 2.
D. Testing
(1) Remove the tags and close the circuit breakers that follows:
CB PANEL CB NO. NAME ZONE
CBP−1 B8 HYD PUMP 3B 221
CBP−2 P2 HYD SYS AC PUMP CONT3B 222
CBP−2 A2 HYD PUMP 3A 222
CBP−2 G4 HYD SYS AC PUMP CONT3A 222
(2) Do the Functional Test of the Landing Gear Extension and Retraction System.
Refer to AMM 32−30−00−720−801.
(3) Do the operational test of the Landing−Gear Emergency Extension. Refer to
AMM 32−34−00−710−801.
E. Close−out
NOTE: The steps in the Close−out section of this Service Bulletin, except for the
return−to−service tests, are recommended steps. The steps give a
recommendation to install components removed during the Aircraft Setup.
This recommendation is to make sure that the aircraft is safe and ready to
return to service. Alternative steps can be used at the operator’s
discretion.
MODEL CL−600−2B16
Basic Issue: Dec 18/2017
Revision 02: May 10/2018
650−32−002
Page 8 of 12

### Page 11

(1) Remove all tools, equipment and unwanted materials from the aircraft.
(2) Lower the complete aircraft. Refer to AMM 07−10−01−586−801.
F. 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. Kits
No kit required.
B. Parts
The part(s) that follow(s) may be necessary to do this Special Check/Modification
and is/are available from Bombardier Aerospace Parts Services, Montreal:
NEW PART NO. QTY ITEM USED PARTNO. INSTRUCTIONS- DISPOSITION
DMK379−101 Up to2 Kit, MessierDowty − −
NOTE: The part number(s) for the item(s) listed above are/is subject to change
without revision to this 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.
C. Material
The materials that follow, or equivalent, may be necessary to do this Special
Check/Modification. They can be purchased from a local supplier. Bombardier
Aerospace does not pay for these consumable.
MODEL CL−600−2B16
Basic Issue: Dec 18/2017
Revision 02: May 10/2018
650−32−002
Page 9 of 12

### Page 12

DESCRIPTION PARTNO./NAME SPECIFICATION QUANTITY
SUPPLIER
(SEE
NOTE)
Clear Coat,
Polyurethane
CT: 4 hours
PF−6
Series PH36
or
PG−6 Series
− As Necessary Code: A
Grease,
Aircraft and
Instrument,
Gear and
Actuator
Screw
Aeroshell 33 MIL−PRF−23827CType I As Necessary Code: B
NOTES: 1. Refer to the table that follows for each suppliers 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.
SUPPLIERS ADDRESSES BY CODES
Code: A
Axon Hentzen Aerospace
307 Echelon Road
Greenville, SC,29605−5234
U.S.A.
Tel.: 416−746−2233
www.hentzen.com
Code: B
Shell Canada Limited
400 4th Avenue S.W.
Calgary, Alberta
Canada, T2P 0J4
Tel.: 1−877−656−3111
www.shell.ca
D. Publications
No publications required.
MODEL CL−600−2B16
Basic Issue: Dec 18/2017
Revision 02: May 10/2018
650−32−002
Page 10 of 12

### Page 13

7
LSB3232_001
4
5
6
3 2
1
MODEL CL−600−2B16
Split Ball Bearing Replacement
FIGURE 1
Basic Issue: Dec 18/2017
Revision 02: May 10/2018
650−32−002
Page 11 of 12

### Page 14

LSB3232_011
SIDE STAY ACTUATOR
CANADAIR P/N
M−B−DT P/N
TASY P/N
INSP.
604−85001−
SER. NO.19010 −
19011 −
DATE
DESIGNED AND MANUFACTURED BY
TRIUMPH ACTUATION − YAKIMA, LLC
FSCM 97415
19011−32−1
CYLINDER ASSEMBLY
IDENTIFICATION PLATE
POLYURETHANE
COATINGINK MARKING
Messier−Bugatti−Dowty
MODEL CL−600−2B16
Ink Marking Detail
FIGURE 2
Basic Issue: Dec 18/2017
Revision 02: May 10/2018
650−32−002
Page 12 of 12

### Page 15

650−32−002 Rev. 02 May 10/2018
SPECIAL CHECK/MODIFICATION − EXTENSION AND RETRACTION,
MAIN GEAR − INSPECTION AND REPLACEMENT IF NECESSARY OF
THE SIDE STAY ACTUATOR SPLIT BALL BEARING
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 at:
http://csefeedback.aero.bombardier.com
SERVICE BULLETIN EVALUATION FORM
(Your ideas will help us provide better bulletins)
SERVICE BULLETIN: ISSUE: DATED:
TITLE:

### Page 16

SERVICE BULLETIN INCORPORATION SHEET − "650−32−002"
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.
650−32−002 02
COMPLIED WITH
YES    NO    N/A
Actual hours to accomplish Service Bulletin:
* NOTES:
Aircraft Serial No. Aircraft Reg. No.
Airframe Hours: Airframe Landings
S.B. Incorporation Date Service Order No.
Facility incorporating S.B.
Name Signature Date
BOMBARDIER
SUBMISSION
Service Bulletin
Number
Rev. * Parts
Completed
Remarks/Reason
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.
(dd/mm/yy)
Signature not required if sent by E−Mail (dd/mm/yy)

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