# Bombardier Service Bulletin 700-36-6002

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## Details

- Manufacturer: [Bombardier](https://openairdocs.org/service-documents/bombardier.md)
- Type: Service bulletin (Service Bulletin)
- Number: 700-36-6002
- Page: https://openairdocs.org/service-documents/bombardier/sb-700-36-6002

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## Text (55 pages)

Rights: © Bombardier Inc. Filed by the FAA in regulations.gov docket FAA-2023-2000; AD 2024-03-08 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

SPECIAL CHECK/REWORK – BLEED-AIR LEAK-DETECTION SYSTEM –
SPECIAL CHECK ON THE KIDDE LEAK DETECTION LOOP ELEMENTS
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
Within 120 months or 2000 flight hours
whichever comes first from this Service
Bulletin release date (Basic Issue)
EFFECTIVITY: A/C Serial No. 9313, 9381, 9432 to 9860, 9863 to 9871, 9873 to 9997,and 60005 to 60045
MANPOWER: Refer to Paragraph 1.F.
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 NOYES
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 Aviation Parts Services at:
514−855−2999 or 1−866−538−1247
SERVICE BULLETIN SUMMARY
my.businessaircraft.bombardier.com
MODEL BD−700−1A10 (BD−700)
ATA 36−12
PNEUMATIC
Basic Issue: Dec 23/2022 700−36−6002
Page 1 of 1
This Service Bulletin is available at:

### Page 2

SPECIAL CHECK/REWORK – BLEED-AIR LEAK-DETECTION SYSTEM –
SPECIAL CHECK ON THE KIDDE LEAK DETECTION LOOP ELEMENTS
1. PLANNING INFORMATION
NOTES: 1. To reduce operator downtime due to aircraft set−up, access, close−out
and return to service testing, Bombardier is recommending that the work is
done at the 120 month scheduled maintenance event while still respecting
the Service Bulletin compliance time. Refer to Paragraph 1.F.
2. Minimum manpower requirement is two (2) to perform this Service
Bulletin. However, a third person may be required to assist with heat gun
operation.
3. Do not perform this test procedure when the ambient temperature around
the aircraft is below 0°C (32°F).
4. Testing to be performed in a hangar (well ventilated) or tarmac conditions
with no precipitation.
5. Send all Test Results to Bombardier Customer Support Engineering
through the SRPSA form to SRPSA@aero.bombardier.com or through
Salesforce for BAS Facilities.
6. Before you do this Service Bulletin, examine all STC, STA or
equivalent action changes to make sure that this Service Bulletin can
be completed.
SERVICE BULLETIN
my.businessaircraft.bombardier.com
MODEL BD−700−1A10 (BD−700)
ATA 36−12
PNEUMATIC
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.
 2022 Bombardier Inc.  All rights reserved
Learjet, Challenger, Global, are registered trademarks of Bombardier Inc. or its subsidiaries.
Basic Issue: Dec 23/2022 700−36−6002
Page 1 of 52
This Service Bulletin is available at:

### Page 3

A. Effectivity
BD−700−1A10 aircraft, Serial No. 9313, 9381, 9432 to 9860, 9863 to 9871, 9873 to
9997, and 60005 to 60045.
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 Aviation Service Bulletin(s).
B. Reason
1. Condition:
Sensing elements delivered by Kidde to LTS are not able to properly detect
leakages according to the temperature defined in the specification. Some of the
Leak Detection Loop (LDL) elements supplied by Kidde may be non−conforming
and these elements present a risk due to the inability to detect a bleed air leak.
2. Evidence:
ATP software used by Kidde to test the LDL elements has certain deficiency
within the test equipment which result to a probability of having certain
non−complaint LDL elements delivered to Bombardier.
3. Objective/Benefit:
This Service Bulletin introduces a procedure to test the serviceability (examine
the functionality) on each LDL element installed on the aircraft and to replace
those that have failed.
C. Description
This Service Bulletin gives instructions to:
− Gain access to the equipment bay,
− Gain access under the baggage bay,
− Remove the belly fairings,
− Gain access to the left wing root,
− Gain access to the right wing root,
− Do the heat gun temperature verification,
− Do the flight compartment setup,
− Do the test procedure at each location,
− Fill out Appendix A with test results, and
− Replace defective LDL element if needed.
MODEL BD−700−1A10 (BD−700)
Basic Issue: Dec 23/2022 700−36−6002
Page 2 of 52

### Page 4

D. Compliance
Recommended in less than 120 months or 2000 flight hours, whichever comes first
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. Standard
SRPSA fees may apply. Refer to the Services section of the Bombardier
customer portal for the latest prices, rates and fees.
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 700−00−6002.
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.
3. To reduce operator downtime due to aircraft set−up, access,
close−out and return to service testing, Bombardier is recommending
that the work is done at the 120 month scheduled maintenance event
while still respecting the Service Bulletin compliance time. Refer to
Paragraph 1.F.
1. If the aircraft is in scheduled heavy−maintenance: 55 total man−hours are
necessary to complete this Service Bulletin.
2. If the aircraft is outside scheduled heavy−maintenance: 140 total man−hours
are necessary to complete this Service Bulletin.
MODEL BD−700−1A10 (BD−700)
Basic Issue: Dec 23/2022 700−36−6002
Page 3 of 52

### Page 5

The labor required to do this Service Bulletin when the aircraft is in or outside
scheduled heavy−maintenance 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 120 months from its release date
(Basic Issue).
G. Material − Cost and Availability
No kit is necessary to do this special check/rework. The parts in Paragraph 3.B.
may be necessary to do this Service Bulletin. For material data, refer to
Paragraph 3.C.
The parts are available at no cost if:
− a no−charge purchase order is sent to Bombardier Aviation in less than 120
months from this Service Bulletin release date (Basic Issue).
NOTE: If material coverage is required due to part failure, a scrap certificate will
be required. Claims will not be approved without the necessary scrap
certificate. Please see scrap certificate form attached with Service Bulletin.
During or after the above free period, Smart Parts Plus does not pay for the part(s).
H. Tooling
The equipment and tools listed below are necessary to do this special
check/rework:
GSE REFERENCE NO. PART NO. DESCRIPTION
Commercially Available 07051 (Steinel)(or equivalent) Heat Gun Shield
Commercially Available HG2320E (Steinel)(or equivalent)
Heat Gun (capable of 0
to 350°C (32 to 662°F)
hot air delivery with
tolerance of ±10°F or
±5°C)
Commercially Available HH501BJK or Fluke 289(or equivalent)
Digital Multimeter
Type K input 32− 1100°F
(0−594°C)
Tolerance ±4°F (±2.2°C
or 0.75% (whichever is
greater)
32−104°F (0−40°C)
operate temp
MODEL BD−700−1A10 (BD−700)
Basic Issue: Dec 23/2022 700−36−6002
Page 4 of 52

### Page 6

GSE REFERENCE NO. PART NO. DESCRIPTION
Commercially Available KMQSS−062U−12(or equivalent)
Thermocouple
Type K input 32− 1100°F
(0−594°C) or greater
Tolerance ±4°F (±2.2°C
or 0.75% (whichever is
greater)
Commercially Available −
Green Sharpie marker or
equivalent permanent
marker
Commercially Available − Scraper, Non−Metallic
Commercially Available − Sharp Knife
Commercially Available −
Stopwatch Time
2 minutes (minimum),
1 second resolution (±5
secs over range)
Commercially Available − Walkie Talkies
Commercially Available − Wrench, Torque 10 to 35lbf in (1.13 to 3.95 Nm)
Commercially Available − Wrench, Torque 29 to 50lbf in (3.28 to 5.65 Nm)
Commercially Available − Wrench, Torque 55 to 85lbf in (6.21 to 9.60 Nm)
Commercially Available −
Wrench, Torque 162 to
179 lbf in (18.31 to 20.22
Nm)
Commercially Available −
Wrench, Torque 71.25 to
87.91 lbf ft (96.61 to
119.18 Nm)
NOTES: 1. Refer to the Global 6000 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 Global 6000 for
acceptable GSE equivalents.
MODEL BD−700−1A10 (BD−700)
Basic Issue: Dec 23/2022 700−36−6002
Page 5 of 52

### Page 7

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
No change.
J. Electrical Load Data
No change.
K. References
− TCCA Airworthiness Directive, (pending).
− Bombardier Aviation, Restriction and/or Special Instruction (RSI), C−01809.
− Bombardier Aviation, Restriction and/or Special Instruction (RSI), C−01813.
− Liebherr−Aerospace Toulouse SAS (LTS), Service Bulletin,
CFD−F1958−26−01, Initial Issue, dated May 6 2022.
− Kidde Aerospace and Defense SB CFD−26−1 Revision 6,
dated 28 February 2022.
− Kidde, procedure R−12586.
− Kidde, procedure R−12595.
− Bombardier Aviation, Standard Practices Manual (SPM), Chapter 20.
− Appendix A − Test Results.
− Appendix B − Test Matrix.
− Appendix C − Test Locations.
− Bleed Loop Scrap Certificate (Attached).
− Advisory Wire AW700−36−0826.
− Global 6000 BD−700 Aircraft Maintenance Manual (AMM), Chapters 6, 21, 24,
36, 45, 53 and 54.
L. Other Publications Affected
None.
M. Equivalent Service Bulletins
For the Global Express and Global Express XRS BD−700−1A10 aircraft, use
SB 700−36−026.
For the Global 5000 BD−700−1A11 aircraft, use SB 700−1A11−36−005.
For the Global 5000 BD−700−1A11 Featuring Global Vision Flight Deck aircraft,
use SB 700−36−5002.
MODEL BD−700−1A10 (BD−700)
Basic Issue: Dec 23/2022 700−36−6002
Page 6 of 52

### Page 8

For the Global 6500 BD−700−1A10 aircraft, use SB 700−36−6501.
For the Global 5500 BD−700−1A11 aircraft, use SB 700−36−5501.
2. ACCOMPLISHMENT INSTRUCTIONS
NOTES: 1. All TASKs given in the procedures that follow are from the Global 6000
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 6000 BD−700−1A10 Aircraft Maintenance Manual (AMM),
Chapter 6.
A. Aircraft Setup
(1) Open the AFT equipment bay access door (311BB).
(2) Remove the AFT fuselage floor−panel (251BLF). Refer to
AMM 53−41−01−000−801.
(3) Remove the pylon access panels (412CB, 413DB, 422CB and 423DB). Refer
to AMM 54−52−01−000−801.
(4) Set the circuit breakers that follow to LOCKED. Refer to
AMM 24−00−00−863−801:
SYSTEM NAME CIRCUIT BREAKER
NAME
BUS NAME
ENGINE L ENG IGN 1 BATT
ENGINE L ENG IGN 2 BATT
ENGINE R ENG IGN 1 BATT
ENGINE R ENG IGN 2 BATT
(5) Remove the LHS and RHS pre−cooler exchangers. Refer to
AMM 36−11−13−000−801.
(6) Remove tailcone access panel (310BZ). Refer to AMM 53−50−01−000−801.
(7) Remove the belly fairing access−panels (185BL, 186BR, 185CL and 186CR).
Refer to AMM 53−61−19−000−801.
(8) Remove the main landing gear (MLG) wheel bins (165AZ and 166AZ). Refer to
AMM 53−30−01−000−801.
(9) Remove the MLG center fairing panel (185AB). Refer to
AMM 53−61−17−000−801.
(10) Remove the under−wing fairings (183AL, 183BL, 184BR and 184AR). Refer to
AMM 53−61−05−000−801.
MODEL BD−700−1A10 (BD−700)
Basic Issue: Dec 23/2022 700−36−6002
Page 7 of 52

### Page 9

(11) Remove the forward wing−to−fuselage fairings (181AL, 181BL and 182BR).
Refer to AMM 53−61−01−000−801.
(12) Connect and energize external AC power. Refer to AMM 24−41−00−861−801.
B. Heat Gun Temperature Verification
WARNING: THE LEAK DETECTION LOOP ELEMENTS MUST NOT BE
EXPOSED TO DC VOLTAGES/CURRENTS.
WARNING: HEAT GUN SHOULD NOT BE USED NEAR FLAMMABLE LIQUIDS
OR IN AN EXPLOSIVE ENVIRONMENT (FUMES, GASES OR
DUST). REMOVE MATERIALS OR DEBRIS THAT MAY BECOME
IGNITED FROM WORK AREA.
WARNING: DO NOT LEAVE TOOL UNATTENDED WHILE RUNNING OR
COOLING DOWN. OTHERWISE RISK OF FIRE.
CAUTION: DO NOT USE A METER THAT APPLIES A DC VOLTAGE. DO NOT
USE INSULATION RESISTANCE “MEGGER” TESTERS OR
DIELECTRIC VOLTAGE “HYPOT” TESTERS. THESE WILL
DAMAGE THE LEAK DETECTION LOOP ELEMENTS.
CAUTION: WHEN HEATING LEAK DETECTION LOOP ELEMENTS, THE HEAT
GUN SHALL BE POSITIONED SUCH THAT THE HEAT IS NOT
APPLIED WITHIN 1 INCH (2.5 CM) OF LEAK DETECTION LOOP
ELEMENT WHITE GROMMETS.
CAUTION: DO NOT DIRECT HEAT GUN AIRSTREAM AT CLOTHING, HAIR
OR OTHER BODY PARTS.
CAUTION: ALWAYS HOLD HEAT GUN BY PLASTIC ENCLOSURE. THE
METAL NOZZLE REQUIRES APPROXIMATELY 20 MINUTES TO
COOL TO WHERE IT CAN BE TOUCHED. DO NOT TOUCH
NOZZLE OR ACCESSORY TIPS UNTIL COOL.
CAUTION: DO NOT STORE HEAT GUN UNTIL NOZZLE HAS COOLED TO
ROOM TEMPERATURE. PLACE TOOL IN A CLEAR AREA AWAY
FROM COMBUSTIBLE MATERIALS WHILE COOLING.
CAUTION: DO NOT CUT OFF HEAT GUN AIRFLOW BY PLACING NOZZLE
TOO CLOSE TO WORK PIECE. KEEP INTAKE VENTS CLEAN AND
CLEAR OF OBSTRUCTIONS.
CAUTION: USE SHIELD MATERIALS AROUND THE HEATED AREA TO
PREVENT DAMAGE OR FIRE.
MODEL BD−700−1A10 (BD−700)
Basic Issue: Dec 23/2022 700−36−6002
Page 8 of 52

### Page 10

CAUTION: PLACE TOOL ON A LEVEL SURFACE WHEN TOOL IS NOT
HANDHELD. PLACE CORD IN A POSITION THAT WON'T CAUSE
TIPPING. KEEP A FULLY CHARGED FIRE EXTINGUISHER
NEARBY.
NOTES: 1. Testing to be performed in a hangar (well ventilated) or tarmac
conditions with no precipitation.
2. Do not perform this test procedure when the ambient temperature
is below 0°C (32°F).
3. Minimum manpower requirement is two (2). However, a third
person may be required to assist with heat gun operation.
4. To ensure that the heat gun temperature is consistent during all
testing, this verification procedure shall be performed prior to
testing the first sensing element of each alarm set point and
repeated after every 4 hours of testing or when the sensing
element set point changes or when the ambient conditions in the
test location change but not less than once per shift.
(1) The heat gun nozzle deflector shall be securely attached to the heat gun as
shown in Figure 1 and Figure 3.
SB700−36−6501_022
Temperature & Airflow
Figure 1
MODEL BD−700−1A10 (BD−700)
Basic Issue: Dec 23/2022 700−36−6002
Page 9 of 52

### Page 11

(2) Connect the thermocouple wire to the digital meter and set the meter to
measure temperature in °C. Refer to Figure 2.
SB700−36−6501_024
Figure 2
(3) Place the thermocouple at the center of the heat protection shield (not touching
the shield) at the approximate location the 1 or 2 LDL element(s) will be
placed. Refer to Figure 3.
MODEL BD−700−1A10 (BD−700)
Basic Issue: Dec 23/2022 700−36−6002
Page 10 of 52

### Page 12 (OCR)

BOMBARDIER
GLOBAL 6000
MODEL BD-700-1A10 (BD-700)
Testing a single loop
Sensing  Heatgun outlet
element
+ 1-1.25"
- 1.25-1.5" -
Testing two loops
Sensing  Heatgun outlet
element
* 1-1.25"
- 1.25-1.5" -
SB700-36-6501_023
Figure 3
Basic Issue: Dec 23/2022  700-36-6002
Page 11 of 52

### Page 13

(4) Turn ON the heat gun and set airflow rate to maximum on the heat gun if the
setting is available.
(5) Set the heat gun temperature so that the thermocouple reads the
thermocouple test temperature value specified in Table 1 for the correct salt
type letter.
(6) Verify and record that the center thermocouple temperature value is within the
thermocouple test temperature value tolerance specified in Table 1.
TABLE 1
SALT TYPE TEMPERATURE SETPOINT
THERMOCOUPLE
TEMPERATURE
1.05*SP+5°C
A 124°C
255°F
135°C (−0, +17°C)
275°F (−0, +30°F)
C 154°C
310°F
167°C (−0, +17°C)
332°F (−0, +30°F)
NOTES: 1. It is recommended that the heat gun setting temperature be
initially set high enough such to achieve a thermocouple test
temperature that uses approximately ½ the allowable
temperature tolerance defined in Table 1
2. For heat guns with a digital display, the heat gun display
temperature will typically be higher than the temperature at the
thermocouple.
3. During heat gun temperature settings calibration to achieve the
thermocouple test temperature, the thermocouple temperature
will slightly vary up and down according to the thermal regulation
of the heat gun. The temperature values recorded should be the
average of the observed results.
(7) Move and place the thermocouple approximately 0.33 inch (0.85 cm) from the
centerline of the heat protection shield left or right at the approximate location
the sensing element will be place as shown in Figure 3.
NOTES: 1. If measuring the 2nd location right of centerline, route
thermocouple from the right. If measuring the 2nd location left of
centerline, route thermocouple from the left.
2. The heat gun 2nd or off−axis location may be below the lower
limit in the Table 1 as the temperature may reduce near the
edges left or right of center test position.
(8) Record the second or off−axis thermocouple value.
(9) Calculate the two (2) point average temperature of the center point and second
or off−axis thermocouple readings.
MODEL BD−700−1A10 (BD−700)
Basic Issue: Dec 23/2022 700−36−6002
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### Page 14

EXAMPLE
SALT TYPE
LETTER
CENTER
THERMOCOUPLE
TEMPERATURE
(T CENTER)
2ND LOCATION
(OFF AXIS)
THERMOCOUPLE
TEMPERATURE
(T 2ND)
2 PT AVERAGE
THERMOCOUPLE
TEST
TEMPERATURE
A 290°F / 143°C 260°F / 127°C 275°F / 135°C
Formula: 2pt Average Thermocouple Test Temperature
= (T center + T 2nd)/2
= (290°F + 260°F)/2
= 275°F
(10) If the above 2 point (pt) average thermocouple test temperature value is not
within the tolerance allowed in Table 1 using a center and left off axis position
or center and right off axis position, attempt steps (3) through (9) trying the
opposite side of the tested center and left or right off axis position until the 2 pt
average thermocouple test temperature value is within the tolerance limits.
This will mitigate some heat gun variability. If the testing is not successful,
replace the heat gun with one with a more uniform output.
NOTE: It is recommended this value be near or approximately at the
mid−point of the temperature range defined by the tolerance in
Table 1.
C. Flight Compartment Setup
(1) Obey all electrical/electronic safety precautions. Refer to
AMM 24−00−00−910−801.
(2) Set aircraft power ON and verify that no L BLEED FAULT, R BLEED FAULT,
WING A/ICE FAULT, and TRIM AIR FAULT Advisory CAS messages are
displayed.
(3) Conduct BMC initiated Built In Test (IBIT). Refer to AMM 45−47−00−970−803:
BMC #1 IBIT
− Select BLEED MANAGEMENT CONTROLLER #1 on LRU selection
display.
− Select TEST tab and select L BMC TEST.
− Make sure that all preconditions are met and select CONTINUE.
− Verify that no L BLEED FAULT, R BLEED FAULT, WING A/ICE FAULT,
and TRIM AIR FAULT Advisory CAS messages are displayed.
BMC #2 IBIT
− Select BLEED MANAGEMENT CONTROLLER #2 on LRU selection
display.
MODEL BD−700−1A10 (BD−700)
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### Page 15

− Select TEST tab and select R BMC TEST.
− Make sure that all preconditions are met and select CONTINUE.
− Verify that no L BLEED FAULT, R BLEED FAULT, WING A/ICE FAULT,
and TRIM AIR FAULT Advisory CAS messages are displayed.
SB700−36−6501_021
D. Test Procedure
(1) Position one person in the flight compartment to monitor EICAS indications and
one or two person at the test site with heat gun. Refer to Appendix C for test
site locations.
NOTES: 1. Multiple LDL element locations cannot be tested at once.
2. Operators can begin testing at any LDL element location.
(2) Refer to Appendix B to determine details of LDL elements that are to be tested
(includes salt types of LDL elements).
(3) If an LDL element has been marked on one (1) face of its connector hex nut or
with a date code outside of A0448 through A2104 (inclusive), then this LDL
element DOES NOT require testing (ref LTS VSB CFD−F1958−26−01).
(4) For aircraft equipped with the humidifier system, LDL elements MT147A,
MT147B, MT148A and MT148B must be tested.
MODEL BD−700−1A10 (BD−700)
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### Page 16

(5) Depending on salt type of LDL element being tested (ref Appendix A for salt
type), set heat gun temperature per Table 1, column 3.
TABLE 1
SALT TYPE TEMPERATURE SETPOINT
THERMOCOUPLE
TEMPERATURE
1.05*SP+5°C
A 124°C
255°F
135°C (−0, +17°C)
275°F (−0, +30°F)
C 154°C
310°F
167°C (−0, +17°C)
332°F (−0, +30°F)
(6) Allow the heat gun to preheat for a minimum of 30 seconds to reach the
appropriate stable test temperature as stated in column 3 of Table 1. Ensure
that the exhaust of the heat gun is directed in a safe direction.
CAUTION: MAKE SURE NOT TO AFFECT THE LEAK DETECTION LOOP
ELEMENTS POSITION AND THAT THEY ARE STILL INSTALLED
AS PER AMM 36-12-00-910-801.
CAUTION: USE SHIELD MATERIALS AROUND THE HEATED AREA TO
PREVENT DAMAGE OR FIRE. APPLY PROTECTIVE BARRIERS IF
NECESSARY.
NOTES: 1. PT04: Use caution, the wiring harness is very close to this test
point.
2. PT83 and PT85 can be done from the AFT equipment bay door
looking FWD on LHS and RHS.
3. PT114: It is acceptable to move the test location 5 in (127 mm) in
any direction due to tool access.
4. Test points FWD of pre−cooler (PT54, PT55, PT56) can be done
passing by panel 412CB/422CB and using the heat gun without
nozzle deflector.
Test PT54, PT55, PT56 using heat shielding and the single LDL
element method.
MODEL BD−700−1A10 (BD−700)
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### Page 17

(7) Position the heat gun at the LDL element test location over both of the LDL
elements using the deflector sleeve per Figure 3. Make sure the deflector
sleeve is not touching the LDL element.
NOTES: 1. If there is insufficient space to allow the heat gun to heat both
LDL element without contact with the LDL element or clashing
with surrounding structure/systems, it is permitted to use two heat
guns in the same location.
2. For each LDL element, position a heat gun at the LDL element
test location over the LDL element using the deflector sleeve per
Figure 3. Make sure the defector sleeve is not touching the LDL
element).
(8) Heat the LDL element location with heat gun for no more than 120 seconds (2
minutes).
(9) Verify L BLEED LEAK, R BLEED LEAK, TRIM AIR LEAK or WING A/ ICE
LEAK EICAS message is posted as applicable depending on the LDL element
being tested.
(10) Stop applying heat to LDL elements upon EICAS detection or before 120
seconds time−out.
NOTE: If EICAS message does not post, re−position heat gun and repeat
heating (steps (7) to (9)) prior to going to step (11), single channel test
method.
(11) PASS/FAIL criteria:
(a) PASS: A heated LDL element results in L BLEED LEAK, R BLEED LEAK,
TRIM AIR LEAK or WING A/ ICE LEAK EICAS message before the 120
second time−out, as applicable depending on the LDL element being
tested.
(b) FAIL: A heated LDL element DOES NOT result in L BLEED LEAK, R
BLEED LEAK, TRIM  AIR LEAK or WING A/ ICE LEAK EICAS message
before the 120 second time−out, as applicable depending on the LDL
element being tested. To determine which LDL element has failed, test the
failed test point again using the following single channel test procedures.
(i) Depower L BMC CH A and B from EMSCDU. Refer to Appendix B to
determine which LDL element is active by depowering L BMC.
(ii) Repeat steps (7) to (9).
(iii) If L BLEED LEAK, R BLEED LEAK, TRIM AIR LEAK or WING A/ ICE
LEAK EICAS message is posted before the 120 second time−out, as
applicable depending on the LDL element being tested, continue
testing on remaining locations of active LDL element. If all locations of
active LDL element triggered L BLEED LEAK, R BLEED LEAK, TRIM
AIR LEAK or WING A/ ICE LEAK EICAS message before the 120
second time−out, as applicable depending on the LDL element being
tested, mark one (1) face of one (1) connector hex nut with one (1)
GREEN mark to indicate that the active LDL element has been
thermally tested and verified PASS at all locations. Refer to Figure 4.
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### Page 18

SOCKET TYPE END PIN TYPE END
Figure 4
(iv) If LDL element fails due to the 120 second time−out, then the LDL
element must be removed. The failed LDL element to be red tagged
and removed from aircraft. Serviceable LDL element (per LTS VSB
CFD−F1958−26−01) shall be installed. Refer to applicable chapter of
AMM 36−12−01.
NOTE: It is prohibited to install any failed LDL element.
a If a LDL element fails, mark the LDL element as failed in
Appendix A and record the LDL element Serial No. and Batch
No./Date Code in Appendix A.
b If material coverage is required due to part failure, a scrap
certificate will be required. Claims will not be approved without
the necessary scrap certificate. Please see scrap certificate form
attached with Service Bulletin.
(v) Power L BMC CH A and CH B and depower R BMC CH A and CH B
from EMSCDU. Refer to Appendix B to determine which LDL element
is active by depowering R BMC.
(vi) Repeat steps (7) to (9).
(vii) If R BLEED LEAK, L BLEED LEAK, TRIM AIR LEAK or WING A/ ICE
LEAK EICAS message is posted before the 120 second time−out, as
applicable depending on the LDL element being tested, continue
testing on remaining locations of active LDL element. If all locations of
active LDL element triggered R BLEED LEAK, L BLEED LEAK, TRIM
AIR LEAK or WING A/ ICE LEAK EICAS message before the 120
second time−out, as applicable depending on the LDL element being
tested, mark one (1) face of one (1) connector hex nut with one (1)
GREEN mark to indicate that the active LDL element has been
thermally tested and verified PASS at all locations. Refer to Figure 4.
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### Page 19

(viii) If a LDL element fails due to the 120 second time−out, then the LDL
element must be removed. The failed LDL element to be red tagged
and removed from aircraft. Serviceable LDL element (per LTS VSB
CFD−F1958−26−01) shall be installed. Refer to applicable chapter of
AMM 36−12−01.
NOTE: It is prohibited to install any failed LDL element.
a If a LDL element fails, mark the LDL element as failed in
Appendix A and record the LDL element Serial No. and Batch
No./Date Code in Appendix A.
b If material coverage is required due to part failure, a scrap
certificate will be required. Claims will not be approved without
the necessary scrap certificate. Please see scrap certificate form
attached with Service Bulletin.
(ix) Power R BMC CH A and CH B from EMSCDU.
(12) To reset the faults, do as follows then proceed to step 13:
(a) For TRIM AIR LEAK select Trim AIR switch to OFF and back to ON.
(b) For L or R BLEED LEAK select L and R ENGINE BLEED switches to OFF
and back to AUTO.
(c) For WING A/ICE LEAK select WING A/ICE to OFF and back to AUTO.
NOTE: If fault does not clear, wait 10 seconds and do the reset
procedure again.
(13) Repeat steps (2) to (12) until each paired LDL element test location presented
in Appendix C is tested and results recorded in Appendix A. Remove any
protection thermal blankets or protection aids and advance to the next LDL
element candidate to be tested.
(14) For each LDL element that has been thermally tested and verified PASS at all
test locations shown in Appendix C, mark one (1) face of one connector hex
nut with one (1) GREEN mark. Refer to Figure 4.
(15) When testing is completed, turn off heat gun.
E. Testing
(1) Test procedure is part of the pre−cooler installation task in Paragraph 2.F.(9).
Refer to AMM 36−11−13−400−801.
F. Close−out
(1) Remove all tools, equipment and unwanted materials from the aircraft.
(2) Remove external AC power. Refer to AMM 24−41−00−861−802.
(3) Install the forward wing−to−fuselage fairings (181AL, 181BL and 182BR).
Refer to AMM 53−61−01−400−801.
(4) Install the under−wing fairings (183AL, 183BL, 184BR and 184AR). Refer to
AMM 53−61−05−400−801.
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### Page 20

(5) Install the MLG wheel bins (165AZ and 166AZ). Refer to
AMM 53−30−01−400−801.
(6) Install the MLG center fairing panel (185AB). Refer to
AMM 53−61−17−400−801.
(7) Install the belly fairing access−panels (185BL, 186BR, 185CL and 186CR).
Refer to AMM 53−61−19−400−801.
(8) Install tailcone access panel (310BZ). Refer to AMM 53−50−01−400−801.
(9) Install the LHS and RHS pre−cooler exchangers. Refer to
AMM 36−11−13−400−801.
(10) Set the circuit breakers that follow to IN. Refer to AMM 24−00−00−863−802:
SYSTEM NAME CIRCUIT BREAKER
NAME
BUS NAME
ENGINE L ENG IGN 1 BATT
ENGINE L ENG IGN 2 BATT
ENGINE R ENG IGN 1 BATT
ENGINE R ENG IGN 2 BATT
(11) Install the pylon access panels (412CB, 413DB, 422CB and 423DB). Refer to
AMM 54−52−01−400−801.
(12) Install the AFT fuselage floor−panel (251BLF). Refer to
AMM 53−41−01−400−801.
(13) Close the AFT equipment bay access door (311BB).
G. 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).
For information, corrections, comments and/or feedback regarding Service Bulletins
released on the Customer Portal, please contact the Service Bulletin Group at the
following email address:
bbad_SBgroup@aero.bombardier.com
3. MATERIAL INFORMATION
A. Kit
No kits required.
MODEL BD−700−1A10 (BD−700)
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### Page 21

B. Parts
The parts that follow may be necessary to do this Service Bulletin and are available
from Bombardier Aviation Parts Services, Montreal:
NEW PART NO. QTY ITEM USED PART
NO.
INSTRUCTIONS
- DISPOSITION
GG474−1022−1 4 Gasket GG474−1022−1 Discard
GG584−1030−1 A/R LDL element GG584−1030−1 Refer to
Paragraph 1.G.
GG584−1030−3 A/R LDL element GG584−1030−3 Refer to
Paragraph 1.G.
GG584−1030−4 A/R LDL element GG584−1030−4 Refer to
Paragraph 1.G.
GG584−1031−1 A/R LDL element GG584−1031−1 Refer to
Paragraph 1.G.
GG584−1031−2 A/R LDL element GG584−1031−2 Refer to
Paragraph 1.G.
GG584−1037−1 A/R LDL element GG584−1037−1 Refer to
Paragraph 1.G.
GG584−1037−3 A/R LDL element GG584−1037−3 Refer to
Paragraph 1.G.
GG584−1039−3 A/R LDL element GG584−1039−3 Refer to
Paragraph 1.G.
GG584−1039−5 A/R LDL element GG584−1039−5 Refer to
Paragraph 1.G.
GG584−1039−6 A/R LDL element GG584−1039−6 Refer to
Paragraph 1.G.
GG584−1040−1 A/R LDL element GG584−1040−1 Refer to
Paragraph 1.G.
GG584−1040−3 A/R LDL element GG584−1040−3 Refer to
Paragraph 1.G.
GG584−1041−1 A/R LDL element GG584−1041−1 Refer to
Paragraph 1.G.
GG584−1041−2 A/R LDL element GG584−1041−2 Refer to
Paragraph 1.G.
MODEL BD−700−1A10 (BD−700)
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### Page 22

NEW PART NO. QTY ITEM USED PART
NO.
INSTRUCTIONS
- DISPOSITION
GG584−1041−3 A/R LDL element GG584−1041−3 Refer to
Paragraph 1.G.
GG584−1043−7 A/R LDL element GG584−1043−7 Refer to
Paragraph 1.G.
GG584−1044−3 A/R LDL element GG584−1044−3 Refer to
Paragraph 1.G.
GG584−1045−3 A/R LDL element GG584−1045−3 Refer to
Paragraph 1.G.
GG584−1046−3 A/R LDL element GG584−1046−3 Refer to
Paragraph 1.G.
GG584−1046−4 A/R LDL element GG584−1046−4 Refer to
Paragraph 1.G.
GG584−1048−1 A/R LDL element GG584−1048−1 Refer to
Paragraph 1.G.
GG584−1048−3 A/R LDL element GG584−1048−3 Refer to
Paragraph 1.G.
GG584−1049−1 A/R LDL element GG584−1049−1 Refer to
Paragraph 1.G.
GG584−1049−3 A/R LDL element GG584−1049−3 Refer to
Paragraph 1.G.
GG584−1050−3 A/R LDL element GG584−1050−3 Refer to
Paragraph 1.G.
GG584−1051−3 A/R LDL element GG584−1051−3 Refer to
Paragraph 1.G.
GG584−1052−1 A/R LDL element GG584−1052−1 Refer to
Paragraph 1.G.
GG584−1053−1 A/R LDL element GG584−1053−1 Refer to
Paragraph 1.G.
GG584−2118−1 A/R LDL element GG584−2118−1 Refer to
Paragraph 1.G.
MODEL BD−700−1A10 (BD−700)
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### Page 23

NEW PART NO. QTY ITEM USED PART
NO.
INSTRUCTIONS
- DISPOSITION
GG584−2118−3 A/R LDL element GG584−2118−3 Refer to
Paragraph 1.G.
NOTES: 1. The part numbers for the items listed above are 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.
2. If material coverage is required due to part failure, a scrap certificate
will be required. Claims will not be approved without the necessary
scrap certificate. Please see scrap certificate form attached with
Service Bulletin.
C. Material
The materials that follow, or equivalent, are necessary to do this Service Bulletin.
These can be purchased from a local supplier. Bombardier Aviation does not pay
for these consumables.
DESCRIPTION PART
NO./NAME
SPECIFICATION QUANTITY SUPPLIER
(SEE
NOTE)
Compound,
Sealing, Low
Shrinkage,
Pressure and
Environmental
AC−665
B−1/2, B−2
− As Necessary Code: A
Compound,
Sealing, Non
Chromated,
Pressure and
Environmental
AC−735 B−2
AC−380
B−1/2, B−2
− As Necessary Code: A
Tape,
Polyurethane
Protective
8681 − As Necessary Code: A
Compound,
Leak
Detection,
Oxygen
Systems
− MIL−PRF−25567
Type I
As Necessary Code: B
Protective
Coating
Humiseal
1B15
− As Necessary Code: C
MODEL BD−700−1A10 (BD−700)
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### Page 24

DESCRIPTION PART
NO./NAME
SPECIFICATION QUANTITY SUPPLIER
(SEE
NOTE)
RTV Silicone,
High
Temperature
− MIL−A−46106
Type I, Grade III
As Necessary Code: D
Sealant, Heat
Resistant
RTV 736 − As Necessary Code: D
PTFE
Release
Agent, Liquid
Form
MS−143H
MS−143TE
MS−143XD
− As Necessary Code: E
Seal and Coat
Compound
Pro Seal 870
CL A
MIL−PRF−81733
Type I, Class 1,
Grade A
As Necessary Code: F
Seal and Coat
Compound
Pro Seal 870
CL B
MIL−PRF−81733
Type II, Class 1,
Grade A
As Necessary Code: F
Sealing,
Compound
PR1428 B1/2 − As Necessary Code: F
Cloth,
Cleaning,
Low−Lint
− − As Necessary Code: G
Lockwire CRES 0.032
in (0.81 mm)
MS20995C32 As Necessary Code: G
Oil,
Lubricating
Brayco 885
Cosmolubric
270−A
Royco 885
Univis P−12
MIL−L−6085 As Necessary Code: G
Synthetic
Detergent,
Liquid Form
(Compound to
Hand−Wash
Dishes)
P−D−410 Type II As Necessary Code: G
Tape, Cellular
Foam,
Silicone
HT−805A − As Necessary Code: G
MODEL BD−700−1A10 (BD−700)
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Page 23 of 52

### Page 25

DESCRIPTION PART
NO./NAME
SPECIFICATION QUANTITY SUPPLIER
(SEE
NOTE)
Tape,
Insulation,
High
Temperature,
Glass Fiber
− MIL−I−19166 As Necessary Code: G
Tape, Liquid
Barrier (Water
Seal)
P−306L − As Necessary Code: G
Tape, PTFE
Sealant
AMS 3255 Class 2 As Necessary Code: G
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
3M Specialty Adhesives
3211 Chestnut Expressway E.
Springfield, MO
U.S.A., 68502
Tel.: (417) 869−3501
www.3M.com
Code: B
American Gas & Chemical Co. Ltd.
220 Pegasus Ave.
Northvale, NJ
U.S.A., 07647−1904
Tel.: (201) 767−7300
www.amgas.com
Code: C
Chase Corporation
201 Zeta Drive
Pittsburgh, PA
U.S.A., 15238
Tel.: (412) 828−1500
www.chasecorp.com
Code: D
Dow Corning
760 Hodgenville Road
Elizabethtown, KY
U.S.A., 42701
Tel.: (270) 706−8100
www.dow.com
MODEL BD−700−1A10 (BD−700)
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### Page 26

SUPPLIERS ADDRESSES BY CODES
Code: E
Miller Stephenson Chemical Co.
55 Backus Ave.
Danbury, CT
U.S.A., 06810−7328
Tel.: (203) 743−4447
www.miller−stephenson.com
Code: F
PRC−Desoto Intl.
11601 United St.
Mojave, CA
U.S.A., 93501−7048
Tel.: (661) 678−4209
www.ppgaerospace.com
Code: G
Commercially Available
D. Publications
No publications required.
MODEL BD−700−1A10 (BD−700)
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### Page 27

PT01
MT202
MT182
LDL A
LDL B
GG584−1030−1
GG584−1030−1
R BLEED
R BLEED
A
A
LDL B GG584−1030−1 R BLEED A
MT202 LDL A
LDL B
GG584−1030−1
GG584−1030−1
R BLEED
R BLEED
A
A
MT202 LDL A
LDL B
GG584−1030−1
GG584−1030−1
R BLEED
R BLEED
A
A
MT202 LDL A
LDL B
GG584−1030−1
GG584−1030−1
R BLEED
R BLEED
A
A
MT202 LDL A
LDL B
GG584−1030−1
GG584−1030−1
R BLEED
R BLEED
A
A
MT202 LDL A
LDL B
GG584−1030−1
GG584−1030−1
R BLEED
R BLEED
A
A
MT202 LDL A
LDL B
GG584−1030−1
GG584−1030−1
R BLEED
R BLEED
A
A
MT202 LDL A
LDL B
GG584−1030−1
GG584−1030−1
R BLEED
R BLEED
A
A
MT202 LDL A
LDL B
GG584−1030−1
GG584−1030−1
R BLEED
R BLEED
A
A
MT202 LDL A
LDL B
GG584−1030−1
GG584−1030−1
R BLEED
R BLEED
A
A
MT202 LDL A
LDL B
GG584−1030−1
GG584−1030−1
R BLEED
R BLEED
A
A
MT202 LDL A
LDL B
GG584−1030−1
GG584−1030−1
R BLEED
R BLEED
A
A
MT194 LDL A
LDL B
GG584−1037−1
GG584−1045−3
L BLEED
L BLEED
A
A
LDL A
LDL B
GG584−1037−1
GG584−1045−3
L BLEED
L BLEED
A
A
MT182
MT182
MT182
MT182
MT182
MT182
MT182
MT182
MT182
MT182
MT182
MT182
MT174
MT194
MT174
LDL A (BMC 1)
LDL B (BMC 2)LOCATION DESIGNATOR PASS/FAIL ZONE SALT TYPE
APPENDIX A − TEST RESULTS
PT02
PT03
PT04
PT05
PT06
PT07
PT08
PT09
PT10
PT11
PT12
PT13
PT14
PT15
MT202 LDL A GG584−1030−1 R BLEED A
LDL ELEMENT PART NUMBER LDL ELEMENT SERIAL NUMBER(Required for failed units only) BATCH NUMBER/DATE CODE(Required for failed units only)
MODEL BD−700−1A10 (BD−700)
Appendix A − Test Results
(Sheet 1, Rev. NC)
Basic Issue: Dec 23/2022 700−36−6002
Page 26 of 52

### Page 28

GG584−1037−1 L BLEED A
GG584−1037−1
GG584−1045−3
L BLEED
L BLEED
A
A
L BLEED
L BLEED
A
A
L BLEED
L BLEED
C
C
MT194
MT194
MT174
PT16
LDL A
LDL B
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A (BMC 1)
LDL B (BMC 2)LOCATION DESIGNATOR PASS/FAIL ZONE SALT TYPE
APPENDIX A − TEST RESULTS
PT17
PT18
PT19
PT20
PT21
PT22
PT23
PT24
PT25
PT26
PT27
PT28
PT29
PT30
LDL A
GG584−1037−1 L BLEED AMT194
GG584−1045−3 L BLEED AMT174
GG584−1045−3 L BLEED AMT174
C
C
C
C
C
C
A
C
C
A
A
A
A
A
A
A
A
A
A
A
MT195 GG584−1043−7
MT175 GG584−1043−7
MT195 GG584−1043−7
GG584−1043−7
MT195 GG584−1043−7
GG584−1043−7
MT195 GG584−1043−7
GG584−1043−7
MT196 GG584−1053−1
GG584−1053−1
MT175
MT175
MT175
MT176
GG584−1053−1
GG584−1053−1
GG584−1053−1
GG584−1053−1
GG584−1053−1
GG584−1053−1
GG584−1053−1
GG584−1053−1
GG584−1053−1
GG584−1053−1
MT196
MT176
MT196
MT176
MT196
MT176
MT196
MT176
MT196
MT176
L BLEED
L BLEED
L BLEED
L BLEED
L BLEED
L BLEED
L BLEED
L BLEED
L BLEED
L BLEED
L BLEED
L BLEED
L BLEED
L BLEED
L BLEED
L BLEED
L BLEED
L BLEED
L BLEED
L BLEED
LDL ELEMENT PART NUMBER LDL ELEMENT SERIAL NUMBER(Required for failed units only) BATCH NUMBER/DATE CODE(Required for failed units only)
GG584−1053−1
GG584−1053−1
MT196
MT176
LDL A
LDL B
MT195 GG584−1043−7
MT175 GG584−1043−7
MODEL BD−700−1A10 (BD−700)
Appendix A − Test Results
(Sheet 2 of 9, Rev. NC)
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### Page 29

A
PT31
LDL A
LDL B
LDL B
LDL A (BMC 1)
LDL B (BMC 2)LOCATION DESIGNATOR PASS/FAIL ZONE SALT TYPE
APPENDIX A − TEST RESULTS
PT32
LDL A
A
A
A
L BLEED
L BLEED
L BLEED
L BLEED
GG584−1053−1
GG584−1053−1
GG584−1053−1
GG584−1053−1
MT196
MT176
MT196
MT176
LDL ELEMENT PART NUMBER LDL ELEMENT SERIAL NUMBER(Required for failed units only) BATCH NUMBER/DATE CODE(Required for failed units only)
ALDL A
PT33
MT148 GG584−1048−3 TRIM
MT148B
MT147 LDL B
LDL A GG584−1037−3(Humidifier option)
MT147B LDL B GG584−1037−3(Humidifier option)
GG584−1048−1
ATRIM
ATRIM
ATRIM
A
A
LDL A
PT34
MT148 GG584−1048−3
TRIM
TRIM
MT147 LDL B
LDL A GG584−2118−3(Humidifier option)
MT147A LDL B GG584−2118−1(Humidifier option)
GG584−1048−1 A
ATRIM
TRIM
MT148A
A
A
LDL A
PT35
MT148 GG584−1048−3
TRIM
TRIM
MT147 LDL B
LDL A GG584−2118−3(Humidifier option)
MT147A LDL B GG584−2118−1(Humidifier option)
GG584−1048−1 A
ATRIM
TRIM
MT148A
MODEL BD−700−1A10 (BD−700)
Appendix A − Test Results
(Sheet 3 of 9, Rev. NC)
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### Page 30

LDL A (BMC 1)
LDL B (BMC 2)LOCATION DESIGNATOR PASS/FAIL ZONE SALT TYPE
APPENDIX A − TEST RESULTS
LDL ELEMENT PART NUMBER LDL ELEMENT SERIAL NUMBER(Required for failed units only) BATCH NUMBER/DATE CODE(Required for failed units only)
A
A
LDL A
PT36
MT148 GG584−1048−3
TRIM
TRIM
MT147 LDL B
LDL A GG584−2118−3(Humidifier option)
MT147A LDL B GG584−2118−1(Humidifier option)
GG584−1048−1 A
ATRIM
TRIM
MT148A
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
PT37
PT38
PT39
PT40
PT41
PT42
PT43
PT44
PT45
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
GG584−1037−3
GG584−1049−3
MT210
MT190
TRIM
TRIM
TRIM
TRIM
TRIM
TRIM
GG584−1037−3
GG584−1049−3
MT210
MT190
GG584−1037−3
GG584−1049−3
MT210
MT190
TRIM
TRIM
GG584−1037−3
GG584−1049−3
MT210
MT190
GG584−1037−3
GG584−1049−3
MT210
MT190
GG584−1037−3
GG584−1049−3
MT210
MT190
GG584−1037−3
GG584−1049−3
MT210
MT190
GG584−1049−1
GG584−1049−1
MT101
MT102
TRIM
TRIM
TRIM
TRIM
TRIM
TRIM
TRIM
TRIM
TRIM
TRIM
GG584−1037−3
GG584−1049−3
MT210
MT190
MODEL BD−700−1A10 (BD−700)
Appendix A − Test Results
(Sheet 4 of 9, Rev. NC)
Basic Issue: Dec 23/2022 700−36−6002
Page 29 of 52

### Page 31

A
A
A
A
A
A
A
PT46
LDL A
LDL B
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A (BMC 1)
LDL B (BMC 2)LOCATION DESIGNATOR PASS/FAIL ZONE SALT TYPE
APPENDIX A − TEST RESULTS
PT47
PT48
PT49
PT50
PT51
PT52
PT53
PT54
PT55
PT56
PT57
PT58
PT59
PT60
LDL A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
MT101
MT101
MT101
MT201
MT201 R BLEED
R BLEED
MT193 GG584−1039−5
GG584−1040−1
L BLEED
L BLEED
GG584−1039−6
GG584−1041−1
MT102
MT102
MT102
MT181
MT181
MT173
MT199
MT179
R BLEED
R BLEED
GG584−1049−1
GG584−1049−1
GG584−1049−1
GG584−1049−1
GG584−1049−1
GG584−1049−1
MT193 GG584−1039−5
GG584−1040−1
L BLEED
L BLEEDMT173
MT201
MT181
MT193 GG584−1039−5
GG584−1040−1MT173
MT104 GG584−1049−1
GG584−1049−1MT106
GG584−1046−4
GG584−1051−3
MT200
MT180
GG584−1041−2
GG584−1046−3
MT192
MT172
TRIM
TRIM
TRIM
TRIM
TRIM
TRIM
TRIM
TRIM
TRIM
TRIM
R BLEED
R BLEED
L BLEED
L BLEED
L BLEED
L BLEED
R BLEED
R BLEED
R BLEED
R BLEED
R BLEED
R BLEED
GG584−1040−1
GG584−1041−3
GG584−1040−1
GG584−1041−3
GG584−1040−1
GG584−1041−3
LDL ELEMENT PART NUMBER LDL ELEMENT SERIAL NUMBER(Required for failed units only) BATCH NUMBER/DATE CODE(Required for failed units only)
LDL A
LDL B
MT101
MT102
GG584−1049−1
GG584−1049−1
LDL A
LDL B
MT101
MT102
GG584−1049−1
GG584−1049−1
MODEL BD−700−1A10 (BD−700)
Appendix A − Test Results
(Sheet 5 of 9, Rev. NC)
Basic Issue: Dec 23/2022 700−36−6002
Page 30 of 52

### Page 32

A
A
A
A
A
A
A
PT61
LDL A
LDL B
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A (BMC 1)
LDL B (BMC 2)LOCATION DESIGNATOR PASS/FAIL ZONE SALT TYPE
APPENDIX A − TEST RESULTS
PT62
PT63
PT64
PT65
PT66
PT67
PT68
PT69
PT70
PT71
PT72
PT73
PT74
PT75
LDL A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
MT191
MT191
R BLEED
R BLEED
MT171
MT171
GG584−1040−3
GG584−1037−3
MT191
MT171
GG584−1041−2
GG584−1046−3
MT192
MT172
GG584−1046−4
GG584−1051−3
MT200
MT180
L BLEED
L BLEED
GG584−1040−3
GG584−1037−3
MT191
MT171
MT191
MT171
GG584−1040−3
GG584−1037−3
GG584−1040−3
GG584−1037−3
GG584−1040−3
GG584−1037−3
GG584−1039−6
GG584−1041−1
MT199
MT179
MT199
MT179
MT199
MT179
L BLEED
L BLEED
L BLEED
L BLEED
L BLEED
L BLEED
L BLEED
L BLEED
L BLEED
L BLEED
R BLEED
R BLEED
R BLEED
R BLEED
R BLEED
R BLEED
L BLEED
L BLEED
L BLEED
L BLEED
L BLEED
L BLEED
R BLEED
R BLEED
R BLEED
R BLEED
GG584−1039−6
GG584−1041−1
GG584−1039−6
GG584−1041−1
LDL ELEMENT PART NUMBER LDL ELEMENT SERIAL NUMBER(Required for failed units only) BATCH NUMBER/DATE CODE(Required for failed units only)
LDL A
LDL B
GG584−1041−2
GG584−1046−3
MT192
MT172
LDL A
LDL B
GG584−1041−2
GG584−1046−3
MT192
MT172
GG584−1046−4
GG584−1051−3
MT200
MT180
GG584−1046−4
GG584−1051−3
MT200
MT180
LDL A
LDL B
MT191
MT171
GG584−1040−3
GG584−1037−3
MODEL BD−700−1A10 (BD−700)
Appendix A − Test Results
(Sheet 6 of 9, Rev. NC)
Basic Issue: Dec 23/2022 700−36−6002
Page 31 of 52

### Page 33

GG584−1049−1
GG584−1049−1
MT104
MT106
GG584−1049−1
GG584−1049−1
GG584−1039−3
GG584−1037−3
R BLEED
R BLEED
R BLEED
R BLEED
R BLEED
R BLEED
MT104
MT106
MT103
MT105
A
A
A
A
A
A
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A (BMC 1)
LDL B (BMC 2)LOCATION DESIGNATOR PASS/FAIL ZONE SALT TYPE
APPENDIX A − TEST RESULTS
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
PT76
PT77
PT78
PT79
PT80
PT81
PT82
PT83
PT84
PT85
PT86
PT87
PT88
PT89
PT90
MT206
MT209
MT189
MT186
GG584−1031−1
GG584−1031−1
MT208
MT188
GG584−1044−3
GG584−1044−3
R BLEED
R BLEED
GG584−1049−1
GG584−1049−1
R BLEED
R BLEED
L BLEED
L BLEED
MT104
MT106
GG584−1050−3
GG584−1050−3
L BLEED
L BLEED
R BLEED
R BLEED
L BLEED
L BLEED
L BLEED
L BLEED
R BLEED
R BLEED
L BLEED
L BLEED
L BLEED
L BLEED
LDL ELEMENT PART NUMBER LDL ELEMENT SERIAL NUMBER(Required for failed units only) BATCH NUMBER/DATE CODE(Required for failed units only)
A
A
L BLEED
L BLEED
LDL A
LDL B
MT191
MT171
GG584−1040−3
GG584−1037−3
A
A
L BLEED
L BLEED
LDL A
LDL B
MT191
MT171
GG584−1040−3
GG584−1037−3
GG584−1031−2
GG584−1031−2
MT205
MT185
GG584−1049−1
GG584−1049−1
MT104
MT106
MT103
MT105
GG584−1039−3
GG584−1037−3
MT103
MT105
GG584−1039−3
GG584−1037−3
GG584−1049−1
GG584−1049−1
MT104
MT106
MT209
MT189
GG584−1044−3
GG584−1044−3
MODEL BD−700−1A10 (BD−700)
Appendix A − Test Results
(Sheet 7 of 9, Rev. NC)
Basic Issue: Dec 23/2022 700−36−6002
Page 32 of 52

### Page 34

A
A
A
A
A
A
PT91
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A (BMC 1)
LDL B (BMC 2)LOCATION DESIGNATOR PASS/FAIL ZONE SALT TYPE
APPENDIX A − TEST RESULTS
PT92
PT93
PT94
PT95
PT96
PT97
PT98
PT99
PT100
PT101
PT102
PT103
PT104
PT105
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
L BLEED
L BLEED
R BLEED
MT208
MT188
GG584−1031−1
GG584−1031−1
L BLEED
L BLEED
GG584−1030−4
GG584−1030−4
GG584−1030−4
GG584−1030−4
GG584−1030−4
GG584−1030−4
R BLEED
R BLEED
R BLEED
R BLEED
MT204
MT184
GG584−1030−3
GG584−1030−3
R BLEED
R BLEED
MT204
MT184
MT204
MT184
MT207
MT187
LDL ELEMENT PART NUMBER LDL ELEMENT SERIAL NUMBER(Required for failed units only) BATCH NUMBER/DATE CODE(Required for failed units only)
LDL A
LDL B
A
A
MT206
MT186
R BLEED
R BLEED
GG584−1050−3
GG584−1050−3
LDL A
LDL B
A
A
L BLEED
L BLEED
MT209
MT189
GG584−1044−3
GG584−1044−3
MT206
MT186
GG584−1050−3
GG584−1050−3
MT209
MT189
GG584−1044−3
GG584−1044−3
R BLEED
MT205
MT185
GG584−1031−2
GG584−1031−2
R BLEED
R BLEED
MT205
MT185
GG584−1031−2
GG584−1031−2
R BLEED
R BLEED
L BLEED
L BLEED
MT208
MT188
GG584−1031−1
GG584−1031−1
GG584−1030−4
GG584−1030−4
R BLEED
R BLEED
MT204
MT184
GG584−1030−4
GG584−1030−4
R BLEED
R BLEED
MT204
MT184
L BLEED
L BLEED
MT208
MT188
GG584−1031−1
GG584−1031−1
L BLEED
L BLEED
MODEL BD−700−1A10 (BD−700)
Appendix A − Test Results
(Sheet 8 of 9, Rev. NC)
Basic Issue: Dec 23/2022 700−36−6002
Page 33 of 52

### Page 35

A
A
A
A
A
A
A
PT106
LDL A
LDL B
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A
LDL B
LDL A (BMC 1)
LDL B (BMC 2)LOCATION DESIGNATOR PASS/FAIL ZONE SALT TYPE
APPENDIX A − TEST RESULTS
PT107
PT108
PT109
PT110
PT111
PT112
PT113
PT114
PT115
PT116
PT117
PT118
LDL A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
GG584−1030−3
GG584−1030−3
MT207
MT187
GG584−1030−3
GG584−1030−3
L BLEED
L BLEED
L BLEED
L BLEED
MT207
MT187
LDL ELEMENT PART NUMBER LDL ELEMENT SERIAL NUMBER(Required for failed units only) BATCH NUMBER/DATE CODE(Required for failed units only)
GG584−1030−3
GG584−1030−3
MT207
MT187
L BLEED
L BLEED
R BLEED
R BLEED
MT98
MT100
GG584−1052−1
GG584−1053−1
R BLEED
R BLEED
MT98
MT100
GG584−1052−1
GG584−1053−1
L BLEED
L BLEED
MT97
MT99
GG584−1052−1
GG584−1053−1
L BLEED
L BLEED
MT97
MT99
GG584−1052−1
GG584−1053−1
L BLEED
L BLEED
MT97
MT99
GG584−1052−1
GG584−1053−1
L BLEED
L BLEED
MT97
MT99
GG584−1052−1
GG584−1053−1
L BLEED
L BLEED
MT97
MT99
GG584−1052−1
GG584−1053−1
R BLEED
R BLEED
MT98
MT100
GG584−1052−1
GG584−1053−1
R BLEED
R BLEED
MT98
MT100
GG584−1052−1
GG584−1053−1
R BLEED
R BLEED
MT98
MT100
GG584−1052−1
GG584−1053−1
MODEL BD−700−1A10 (BD−700)
Appendix A − Test Results
(Sheet 9 of 9, Rev. NC)
Basic Issue: Dec 23/2022 700−36−6002
Page 34 of 52

### Page 36

MT97 111/112/113/115/117 GG584−1052−1 L BLEED 1A
DESIGNATOR ZONE BMC
MT207 105/106/107/108 GG584−1030−3 L BLEED 1A
MT208 84/95/97/104 GG584−1031−1 L BLEED 1A
MT209 88/90/92/94 GG584−1044−3 L BLEED 1A
MT103 80/85/86 GG584−1039−3 L BLEED 1A
MT191 61/62/69/70/71/75/76/77 GG584−1040−3 L BLEED 1A
MT192 60/63/64/65 GG584−1041−2 L BLEED 1A
MT193 53/54/56 GG584−1039−5 L BLEED 1A
MT194 14/15/16/17/18 GG584−1037−1 L BLEED 1A
MT195 20/21/22/23/24 GG584−1043−7 L BLEED 1 C
MT196 19/25/26/27/28/29/30/31/32 GG584−1053−1 L BLEED 1A
MT99 L BLEED 2A
MT187 L BLEED 2A
MT189 L BLEED 2A
MT188 L BLEED 2A
MT105 L BLEED 2A
MT171 L BLEED 2A
MT172 L BLEED 2A
MT173 L BLEED 2A
MT174 L BLEED 2A
MT175 L BLEED 2 C
MT176 L BLEED 2A
111/112/113/115/117
105/106/107/108
88/90/92/94
84/95/97/104
80/85/86
61/62/69/70/71/75/76/77
60/63/64/65
53/54/56
14/15/16/17/18
20/21/22/23/24
19/25/26/27/28/29/30/31/32
GG584−1053−1
GG584−1030−3
GG584−1044−3
GG584−1031−1
GG584−1037−3
GG584−1037−3
GG584−1046−3
GG584−1040−1
GG584−1043−7
GG584−1053−1
APPENDIX B − TEST MATRIX
L BLEED LOOP
TEST LOCATION
(APPENDIX C)
SALT
TYPE
LDL ELEMENT
PART NUMBER
GG584−1045−3
MODEL BD−700−1A10 (BD−700)
Appendix B − Test Matrix
(Sheet 1 of 3, Rev. NC)
Basic Issue: Dec 23/2022 700−36−6002
Page 35 of 52

### Page 37

MT98 109/110/114/116/118 GG584−1052−1 R BLEED 1A
DESIGNATOR ZONE BMC
MT204 99/100/101/102/103 GG584−1030−4 1A
MT205 82/96/98 GG584−1031−2 1A
MT206 89/91/93 GG584−1050−3 1A
MT104 57/78/79/81/83/87 GG584−1049−1 1A
MT199 58/72/73/74 GG584−1039−6 1A
MT200 59/66/67/68 GG584−1046−4 1A
MT201 51/52/55 GG584−1040−1 1A
MT202 1/2/3/4/5/6/7/8/9/10/11/12/13 1A
MT100 GG584−1053−1 2A
MT184 GG584−1030−4 2A
MT185 2A
MT186 2A
MT106 2A
MT179 2A
MT180 2A
MT181 2A
MT182 2A
GG584−1031−2
R BLEED
R BLEED
R BLEED
R BLEED
R BLEED
R BLEED
R BLEED
R BLEED
R BLEED
R BLEED
R BLEED
R BLEED
R BLEED
R BLEED
R BLEED
R BLEED
R BLEED
109/110/114/116/118
99/100/101/102/103
82/96/98
89/91/93
57/78/79/81/83/87
58/72/73/74
59/66/67/68
51/52/55
1/2/3/4/5/6/7/8/9/10/11/12/13
GG584−1050−3
GG584−1049−1
GG584−1041−1
GG584−1051−3
GG584−1041−3
GG584−1030−1
R BLEED LOOP
APPENDIX B − TEST MATRIX
TEST LOCATION
(APPENDIX C)
SALT
TYPE
LDL ELEMENT
PART NUMBER
GG584−1030−1
MODEL BD−700−1A10 (BD−700)
Appendix B − Test Matrix
(Sheet 2 of 3, Rev. NC)
Basic Issue: Dec 23/2022 700−36−6002
Page 36 of 52

### Page 38

MT148 33/34/35/36 GG584−1048−3 TRIM 1A
DESIGNATOR ZONE BMC
MT101 45/46/47/48/49/50 GG584−1049−1 1A
MT210 37/38/39/40/41/42/43/44 GG584−1037−3 1A
MT147 33/34/35/36 GG584−1048−1 2A
MT102 45/46/47/48/49/50 GG584−1049−1 2A
MT190 37/38/39/40/41/42/43/44 GG584−1049−3 2A
TRIM
TRIM
TRIM
TRIM
TRIM
TRIM LOOP
TEST LOCATION
(APPENDIX C)
SALT
TYPE
LDL ELEMENT
PART NUMBER
APPENDIX B − TEST MATRIX
MT148B 33 GG584−1037−3 TRIM 1A
DESIGNATOR ZONE BMC
TRIM LOOP (HUMIDIFIER OPTION)
TEST LOCATION
(APPENDIX C)
SALT
TYPE
LDL ELEMENT
PART NUMBER
MT148A 34/35/36 GG584−2118−3 1ATRIM
MT147B 33 GG584−1037−3 TRIM 2A
MT147A 34/35/36 GG584−2118−1 2ATRIM
MODEL BD−700−1A10 (BD−700)
Appendix B − Test Matrix
(Sheet 3 of 3, Rev. NC)
Basic Issue: Dec 23/2022 700−36−6002
Page 37 of 52

### Page 39 (OCR)

BOMBARDIER
GLOBAL 6000
MODEL BD-700-1A10 (BD-700)
Right Bleed Leak Detection Loop - Filtering and Flow Control (MT182 & MT202)
(7 Joint points, 4 Vent Holes)  Aft Fuse FS987.06 thru FS1020 RHS
Ref: PT09
(MT182, MT202)
GG468-4062 duct  Ref: PT10
(MT182, MT202)  Ref: PT12  *Pт04 (MT182, MT202)  PT03  (MT182, MT202)
PT05  (MT182, MT202)  GG468-4064 duct
(MT182, MT202)
Ref: PT11
PT06  (MT182, MT202)
(MT182, MT202)  PT02  PT01
PT07  (MT182, MT202) (MT182, MT202)
(MT182, MT202)
Ref: PT13
(MT182, MT202)
GG468-4056 duct
Right Bleed Leak Detection Loop (MT182 & MT202)
(2 Joint Points)  Aft Fuse FS987.06 thru FS1020 RHS
PT09
(MT182, MT202)
PT08
(MT182, MT202)  Ref: GG468-4064
Ref: PT02  sb700-36-026_021
-WD  (MT182, MT202)
Ref: PT01
(MT182, MT202)
Appendix C - Test Locations
(Sheet 1 of 15, Rev. NC)
Basic Issue: Dec 23/2022  700-36-6002
Page 38 of 52

### Page 40 (OCR)

BOMBARDIER
GLOBAL 6000
MODEL BD-700-1A10 (BD-700)
Right Bleed Leak Detection Loop - ECS Supply (MT182 & MT202)
(2 Vent Holes)  Aft Fuse FS987.06 thru FS1020 RHS
Ref: GG468-4064
PT10
(MT182, MT202)
PT11
(MT182, MT202)
UP
(Dwg View inverted to show up direction)  OUTB'D RHS
Right Bleed Leak Detection Loop - ECS Supply (MT182 & MT202)
(2 Vent Holes)  Aft Fuse FS987.06 thru FS1020 RHS
PT13
Ref: GG468-4062  (MT182, MT202)
Ref: GG468-4056
PT12
(MT182, MT202)
sb700-36-026_022
Appendix C - Test Locations
(Sheet 2 of 15, Rev. NC)
Basic Issue: Dec 23/2022  700-36-6002
Page 39 of 52

### Page 41 (OCR)

BOMBARDIER
GLOBAL 6000
MODEL BD-700-1A10 (BD-700)
Left Bleed Leak Detection Loop - HP Ground Duct (MT174 & MT194)
(2 Joint Points, 3 Vent Holes)  Aft Fuse FS987.06 thru FS1020 LHS
Ref: GG468-4066 HP ground.
PT17
PT14  (MT174, MT194)
(MT174, MT194)
Ref: PT14
(MT174, MT194)
PT15  Ref: PT15
(MT174, MT194)  HIGH PRESSURE  (MT174, MT194)
PT18
(MT174, MT194)
PT16
(MT174, MT194)  Ref: PT16
(MT174, MT194)
Left Bleed Leak Detection Loop - HP Ground Duct
Aft Fuse FS987.06 thru FS1020 LHS
APU  LH BLEED AIR
¿ O  FWO
PYLON
Reference View Only  sb700-36-026_023
Appendix C - Test Locations
(Sheet 3 of 15, Rev. NC)
Basic Issue: Dec 23/2022  700-36-6002
Page 40 of 52

### Page 42

sb700−36−026_024
PT22
(MT175, MT195)
PT21
(MT175, MT195)
PT24
(MT175, MT195)
PT23
(MT175, MT195)
PT20
(MT175, MT195)
Connects to HP ground
duct GG468−4066
Ref: PT24
(MT175, MT195)
PT19
(MT176, MT196)
PT25
(MT176, MT196)
PT27
(MT176, MT196)
PT26
(MT176, MT196)
PT28
(MT176, MT196)
PT29
(MT176, MT196)
PT30
(MT176, MT196)
Ref: PT32
(MT176, MT196)
Ref: PT31
(MT176, MT196)
Ref: GG468−4063
Ref: GG468−4061
Ref: GG468−4043
(MT175 & MT195)
(MT176, MT196)
(6 Joint Points, 3 Vent Holes)
Ref: PT19
(MT176, MT196)
MODEL BD−700−1A10 (BD−700)
Appendix C − Test Locations
(Sheet 4 of 15, Rev. NC)
Basic Issue: Dec 23/2022 700−36−6002
Page 41 of 52

### Page 43

sb700−36−026_025
Ref: PT27
(MT176, MT196)
Ref: PT28
(MT176, MT196)
PT32
(MT176, MT196)
Ref: GG468−4061
GG468−4043
PT31
(MT176, MT196)
(2 Vent Holes)
(MT176 & MT196)
MODEL BD−700−1A10 (BD−700)
Appendix C − Test Locations
(Sheet 5 of 15, Rev. NC)
Basic Issue: Dec 23/2022 700−36−6002
Page 42 of 52

### Page 44 (OCR)

BOMBARDIER
GLOBAL 6000
MODEL BD-700-1A10 (BD-700)
Trim Ducts
FS830 thru FS1020
Trim Ducts  148) FS830 thru FS861 (Baggage Underfloor)
2 Joint points  vent holes) Baggage underfloor
Ref: PT33
(MT147, MT148)
Re l  PT35
(MT147, MT148)
(MT147, MT148)  Ref: PT36  (MT147, MT148)  PT34  sb700-36-026_026
Appendix C - Test Locations
(Sheet 6 of 15, Rev. NC)
Basic Issue: Dec 23/2022  700-36-6002
Page 43 of 52

### Page 45

SB700−36−6501_027
PT36
(MT147A, MT148A)
PT33
(MT147B, MT148B)
PT34
(MT147A, MT148A)
PT35
(MT147A, MT148A)
(MT147A & MT148A, MT147B & MT148B)TRIM LOOP (HUMIDIFIER OPTION)
(2 Joint Points, 2 Vent Holes) 
PT33
(MT147, MT148)
PT36
(MT147, MT148)
PT33
(MT147, MT148)
(MT147 & MT148)
FS830 to FS861 UNDER BAGGAGE FLOOR
MODEL BD−700−1A10 (BD−700)
Appendix C − Test Locations
(Sheet 7 of 15, Rev. NC)
Basic Issue: Dec 23/2022 700−36−6002
Page 44 of 52

### Page 46

SB700−36−026_028
GG468−4057−1
GG468−4058−1
GG468−4059−5
GG468−4058−1
PT37
(MT190, MT210) PT38
(MT190, MT210)
PT42
(MT190, MT210)PT39
(MT190, MT210)
PT43
(MT190, MT210)
PT40
(MT190, MT210)
PT44
(MT190, MT210)
PT41
(MT190, MT210)
(MT190 & MT210)
MODEL BD−700−1A10 (BD−700)
Appendix C − Test Locations
(Sheet 8 of 15, Rev. NC)
Basic Issue: Dec 23/2022 700−36−6002
Page 45 of 52

### Page 47

SB700−36−026_029
Ref: GG468−4057
Ref: GG468−4058−1
Ref: PT41
(MT190, MT210)
PT47
(MT101, MT102)
PT46
(MT101, MT102)
BULKHEAD
PT45
(MT101, MT102)
PT48
(MT101, MT102) PT49(MT101, MT102)
PT50
(MT101, MT102)
(MT101 & MT102)
MODEL BD−700−1A10 (BD−700)
Appendix C − Test Locations
(Sheet 9 of 15, Rev. NC)
Basic Issue: Dec 23/2022 700−36−6002
Page 46 of 52

### Page 48 (OCR)

BOMBARDIER
GLOBAL 6000
MODEL BD-700-1A10 (BD-700)
Pylon Ducts  (RHS: MT181 & MT201)  (LHS: MT173 & MT193)
Pylon Access Panel  (4 Joint Points, 2 Vent Holes)
RHS.  Pylon Ducts
Ref: GG468-4053-1
LHS
Ref: GG468-4053-2  PT51
(MT181, MT201)
PT53
PT54  (MT173, MT193)
PT52  (MT173, MT193)
(MT181, MT201)
Ref; PT56
Ref: PT55  - (MT173, MT193)
(MT181, MT201)
Pylon Ducts  (LHS: MT173 & MT193)
(RHS: MT181 & MT201)
2 Vent holes
RHS
PT55
(MT181, MT201)
PT56
(MT173, MT193)  sb700-36-026_030
Ref: GG468-4053-1 LHS
Ref: GG468-4053-2 RHS  LH Shown - RH Opposite
LHS
Appendix C - Test Locations
(Sheet 10 of 15, Rev. NC)
Basic Issue: Dec 23/2022  700-36-6002
Page 47 of 52

### Page 49 (OCR)

BOMBARDIER
GLOBAL 6000
MODEL BD-700-1A10 (BD-700)
WAI Ducts  (LHS: MT171 & MT191, MT172 & MT192)  (RHS: MT104 & MT106, MT179 & MT199, MT180 & MT200)
Aft Bay Access - Section Access Behind ECS packs. (FS860 to FS1020)  (6 Joint Points)
GG468-4049-2
GG468-4048-3  LHS
Ref PT72
(MT179, MT199)
PT59
PT60
(MT180, MT200)  Ref PT69  (MT172, MT192)
PT58  Ref PT73  (MT171, MT191)
(MT179, MT199)  (MT179, MT199)  Ref PT70
GG468-4046-1  • Ref PT74  (MT171, MT191)
(MT179, MT199)  Ref PT71
(MT171, MT191)  GG468-4049-1
Ref PT75
RHS  • Ref PT78 (MT171, MT191)
PT57  (MT104, MT106)
(MT104, MT106)  Ref PT79  (MT171, MT191)  Ref PT76  PT61  GG468-4047-3
(MT104, MT106)  (MT171, MT191)
Ref PT77
(MT171, MT191) *
GG468-4045-1
PT62
* GG468-4060-2  (MT171, MT191)
GG468-4060-1
(LHS: MT172 & MT192)
WAI Ducts  (RHS: MT180 & MT200)
Aft Bay Access (6 Vent Holes)
PT64
(MT172, MT192)  PT65
LHS  (MT172, MT192)
PT63
(MT172, MT192)
PT67  PT68
(MT180, MT200)
PT66  (MT180, MT200)
(MT180, MT200)
RH Duct
Ref: GG468-4049-2
RHS
LH Duct  sb700-36-026_031
Ref: GG468-4049-1
Appendix C - Test Locations
(Sheet 11 of 15, Rev. NC)
Basic Issue: Dec 23/2022  700-36-6002
Page 48 of 52

### Page 50 (OCR)

BOMBARDIER
GLOBAL 6000
MODEL BD-700-1A10 (BD-700)
WAI Ducts  (LHS: MT171 & MT191)
(RHS: MT179 & MT199)
(6 Vent Holes)
RHS  FWD
AFT
PT74
PT72  PT73  (MT179, MT199)
RHS  (MT179, MT199)  (MT179, MT199)
Ref: GG468-4048-3
Y FWD
PT71
PT69  (MT171, MT191)
(MT171, MT191)
LHS
AFT
LHS
PT70  Ref: GG468-4047-3
(MT171, MT191)
WAI Ducts  (LHS: MT103 & MT105, MT171 & MT191)
(RHS: MT04 & MT106)
(7 Vent Holes)
PT75  PT76  FWD
(MT171, MT191)  (MT171, MT191)  PT79
AFT  (MT104, MT106)
PT77  FWD
LHS  (MT171, MT191)  RHS
Ref: GG468-4045-1
Ref: GG468-4046-1
PT80
(MT103, MT105)
•
AFT  PT78
(MT104, MT106)
Ref: GG468-4060-1 LHS
PT81  sb700-36-026_032
(MT104, MT106)
Ref: GG468-4060-2 RHS
Appendix C - Lest Locations
(Sheet 12 of 15, Rev. NC)
Basic Issue: Dec 23/2022  700-36-6002
Page 49 of 52

### Page 51 (OCR)

BOMBARDIER
GLOBAL 6000
MODEL BD-700-1A10 (BD-700)
WAI Ducts  (LHS: MT103 & MT105)  (RHS: MT104 & MT106)
RHS
LHS
Ref PT81
(MT104, MT106)
Ref PT80
- GG468-4060-2  (MT103, MT105)
GG468-4060-1
Ref PT83
(MT104, MT106)
Ref PT85
(MT103, MT105)
WAI Ducts  (RHS: MT104 & MT106, MT186 & MT206, MT185 & MT205)  (LHS: MT103 & MT105, MT189 & MT209, MT188 & MT208)
(5 JOINT POINTS 8 VENT HOLES)
PT83
(MT104, MT106)
PT87  PT85
(MT104, MT106) •  (MT103, MT105)
PT89  PT88
(MT186, MT206) (MT189, MT209)  PT86
PT91  * (MT103, MT105)
(MT186, MT206)
PT93  PT90
(MT186, MT206)  (MT189, MT209)
(MT185, MT205)  PT82  (MT189, MT209)  PT92  sb700-36-026_033
PT94
PT84  (MT189, MT209)
(MT188, MT208)
Appendix C - Test Locations
(Sheet 13 of 15, Rev. NC)
Basic Issue: Dec 23/2022  700-36-6002
Page 50 of 52

### Page 52 (OCR)

BOMBARDIER
GLOBAL 6000
MODEL BD-700-1A10 (BD-700)
WAI Ducts  (RHS: MT185 & MT205)  (LHS: MT188 & MT208)
(2 Joint Points 2 Vent Holes)
Between Wheelwells
LHS
PT95
(MT188, MT208)
Ref PT84
(MT188, MT208)
PT97
(MT188, MT208)
PT96  RHS
(MT185, MT205)
PT98
(MT185, MT205)
Ref: PT82
(MT185, MT205)
WAI Ducts  (LHS: MT188 & MT208, MT187 & MT207, MT97 & MT99)  (RHS: MT185 & MT205, MT184 & MT204, MT98 & MT100)
(10 Vent Holes)
GG468-4033-3 RHS
PT103  PT102  PT101  PT100
(MT184, MT204)  (MT184, MT204) (MT184, MT204)  (MT184, MT204)  PT99
(MT184, MT204)
Ref: PT110
(MT98, MT100)  Ref: PT98
These test locations may be adjusted +/- 2" for access  (MT185, MT205)
Ref: PT97
(MT188, MT208)
GG468-4032-1 LHS
Ref: PT111  PT108  PT107  PT106  PT105  (MT188, MT208)  PT104  sb700-36-026_034
(MT97, MT99)  (MT187, MT207)  (MT187, MT207)  (MT187, MT207)  (MT187, MT207)
Appendix C - Test Locations
(Sheet 14 of 15, Rev. NC)
Basic Issue: Dec 23/2022  700-36-6002
Page 51 of 52

### Page 53 (OCR)

BOMBARDIER
GLOBAL 6000
MODEL BD-700-1A10 (BD-700)
WAI Ducts  (LHS: MT97 & MT99)
(RHS: MT98 & MT100)
(4 Joint Points)
RHS
PT109
(MT98, MT100)
PT110
(MT98, MT100)  PT111
(MT97, MT99)
C
PT112
(MT97, MT99)
LHS
WAI Ducts  (LHS: MT97 & MT99)
(RHS: MT98 & MT100)
(6 Vent Holes)
Ref: PT111 (MT97, MT99) LH
Ref: PT110 (MT98, MT100) RH
GG468-4030-3 LHS
GG468-4030-4 RHS
Ref: PT112 (MT97, MT99) LH
Ref: PT109 (MT98, MT100) RH  GG468-4028-3 LHS
GG468-4028-4 RHS
neit  Close to
Ref: PT112 (MT97, MT99) LH  Wing
PT117 (MT97, MT99) LH  Ref: PT109 (MT98, MT100) RH
PT118 (MT98, MT100) RH
PT115 (MT97, MT99) LH
PT113 (MT97, MT99) LH  PT116 (MT98, MT100) RH  sb700-36-026_
PT114 (MT98, MT100) RH
Note: PT114 can be moved up to 5" for access
Appendix C - Test Locations
(Sheet 15 of 15, Rev. NC)
Basic Issue: Dec 23/2022  700-36-6002
Page 52 of 52

### Page 54

700−36−6002 Basic Dec 23/2022
SPECIAL CHECK/REWORK – BLEED−AIR LEAK−DETECTION SYSTEM –
SPECIAL CHECK ON THE KIDDE LEAK DETECTION LOOP ELEMENTS
bbad_SBgroup@aero.bombardier.com
NOTE: Please use Salesforce only for troubleshooting issues or when Engineering
deviation is necessary to accomplish the Service Bulletin modification.
SERVICE BULLETIN EVALUATION FORM
(Your ideas will help us provide better bulletins)
SERVICE BULLETIN: ISSUE: DATED:
TITLE:
For any information, correction(s), comment(s) and/or feedback regarding Service
Bulletins released on the Customer Portal, please contact the Service Bulletin Group
at the following email address:

### Page 55

SERVICE BULLETIN INCORPORATION SHEET − "700−36−6002"
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 you’re reporting Service Bulletin (SB) Incorporations to CAMP, sending
this Incorporation Sheet to Bombardier is not mandatory. If your aircraft is
on another tracking system, please contact Bombardier to make arrangements
for automated data submission.
700−36−6002 Basic
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
(Mandatory if N/A)
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.
4. Fill in ’Remark/Reason’ to explain compliance method when N/A is selected.(E.g. Part
not installed, N/A by effectivity, N/A by Part Serial Number, etc.
5. PCW means ’Previously Complied With’.
(dd/mm/yy)
Signature not required if sent by E−Mail (dd/mm/yy)

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