# Bombardier Service Bulletin 601R-24-131

Copy: No revision named ("601R-24-131"), 17 pages: PDF https://openairdocs.org/files/sha256/b7/8a/b78a35addb5cd560946a5074eace43d654092cfc45dff2c5a95f1ace2d9d515f; text https://openairdocs.org/service-documents/bombardier/601r-24-131/file/b78a35addb5c.md. Rights: © Bombardier Inc. Filed by the FAA in regulations.gov docket FAA-2019-0877; AD 2020-03-23 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: 601R-24-131
- Page: https://openairdocs.org/service-documents/bombardier/601r-24-131

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

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

- [AD 2020-03-23](https://openairdocs.org/ad/2020-03-23.md), effective Apr 2, 2020: No revision named

Also cited in [1 proposed AD](https://openairdocs.org/service-documents/bombardier/601r-24-131/proposed.md).

## Text (17 pages)

Rights: © Bombardier Inc. Filed by the FAA in regulations.gov docket FAA-2019-0877; AD 2020-03-23 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

SB 601R- - - 24- - - 131
Page 1 of 17
Jun 28/2012
SERVICE BULLETIN
T echnical
Publications
THIS SERVICE BULLETIN IS SENT TO EACH OPERATOR. IF THE OPERATOR HAS LEASED AIRCRAFT ,
TRANSFERRED SPARES IN THE LAST SIX MONTHS, SEND THIS SERVICE BULLETIN TO THE NEW
OWNER, UNLESS CONFIRMATION WAS RECEIVED THAT BOMBARDIER COMMERCIAL AIRCRAFT
HAS INCLUDED THE NEW OPERATOR ON THE DISTRIBUTION LIST .
SEND THIS SERVICE BULLETIN TO THE LESSEE. IF THE OPERATOR HAS SOLD AIRCRAFT OR
ATA SYSTEM: 24- - -21 NUMBER: 601R - - -24- - -131
S U B J E C T: E l e c t r i c a l P o w e r --- P r i m a r y A C --- G e n e r a t i o n S y s t e m --- I n s p e c t i o n f o r
Chafing and Installation of Protective Conduit on the Generator Power
Cables
1. PLANNING INFORMATION
A. Effectivity
(1) Aircraft Affected:
Service: CL- - - 600- - - 2B19 aircraft with serial numbers 7075, 7136,
7140, 7152, 7176, 7180, 7351, 7730, 7755, 7763, 8043, 8046
thru 8049, 8051 thru 8057, 8060, 8063, 8065 thru 8069, 8071
thru 8094, 8096 thru 8100, 8102, and 8104.
Production: Aircraft with 8106 and subsequent serial numbers will have
an equivalent modification incorporated before delivery.
NOTE: The instructions 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 Service Bulletins. Before you do this service
bulletin, examine all STC, STA or e quivalent action changes to make
sure you can complete this service bulletin.

### Page 2

SERVICE BULLETIN 601R- - -24- - -131
SB 601R- - - 24- - - 131
Page 2 of 17
Jun 28/2012
B. Reason
(1) Condition
The generator power cables can rub against the support brackets of the
auxiliary-aft fuel tank. Damage can occur to the insulation sleeve of the
generator power cables. This can cause a short circuit, arcing, and a
malfunction of one or both main generators.
(2) Evidence
A fouling condition was found between the generator power cables and the
support brackets of the auxiliary-aft fuel tank during a quality control
inspection in production.
(3) Objective/Benefit
This service bulletin gives the procedure to do a visual inspection and to
repair the generator power cables, if damages are found. Also, to install
protective conduits and edging grommets on the potential chafing areas.
Installation of protective conduits and edging grommets will prevent damage
to the generator power cables.
C. Description
Circuit breakers are opened. The cargo-compartment door is opened. If necessary,
the ceiling panels between FS559.00+80.00 and FS574.00 are removed.
A visual inspection of the generator power cables is done. If the insulation sleeve of
the generator power cables is damaged and the wire strands of the generator
power cables are not damaged, the generator power cables are repaired. If the
wire strands of the generator power cables are damaged, the T echnical Help Desk
is called to get a disposition. Protective conduits are installed on the generator
power cables and edging grommets are installed on the fuel tank support-brackets.
The circuit breakers are closed. If removed, the ceiling panels are installed. The
cargo-compartment door is closed. If the generator power cables were repaired,
the operational test of the left and/or right Integrated Drive Generator (IDG) is done.
D. Compliance
Recommended Service Bulletin.
Bombardier recommends that this service bulletin be done before July 31, 2016,
unless otherwise directed by the airworthiness authority of the operator.
This service bulletin does not affect Airworthiness Limitations (AWLs) or Damage
T olerance Inspections (DTIs).

### Page 3

SERVICE BULLETIN 601R- - -24- - -131
SB 601R- - - 24- - - 131
Page 3 of 17
Jun 28/2012
E. Approval
The technical content of this service bulletin has been approved under the authority
of the TCCA Design Approval Organization No: DAO #93- - -Q- - -02.
F. M a n p o w e r
The man-hours given below are estimates for direct labor done by an experienced
crew on an aircraft prepared for maintenance.
These estimates do not include the time necessary for:
Administrative functions such as planning, liaising, familiarization, and report writing.
Non-productive elapsed time such as rest time, having meals, and crew shift changes.
Elapsed time such as for paint to dry, sealant to cure, and fuel tank venting.
Preparation for modification (unless speci fied in the Accomplishment Instructions)
such as cleaning and getting parts, tools, consumables, and ground equipment.
Quality assurance inspections, troubleshooting and/or correction of
discrepancies found when a task is done.
All other activities that are not considered by Bombardier as directly related to the
accomplishment of this procedure.
NOTE: For on-site labor assistance, please speak with a Fleet Services
representative for a quote. Contact the Fleet Services Team
through the CRC at 514-855-8500 or email at
thd.crj@aero.bombardier.com.
It will take an estimated 9.5 man-hours to complete this service bulletin. The
man-hours are divided in the table that follows:
TASK MAN-HOURS
(1) Job Set-Up 1.5
(2) Procedure 3.0
(3) T est 2.0
(4) Job Close-Out 3.0

### Page 4

SERVICE BULLETIN 601R- - -24- - -131
SB 601R- - - 24- - - 131
Page 4 of 17
Jun 28/2012
NOTE: These estimates do not include the man-hours necessary to do the repair
of the generator power cables. Add 1.0 hour for each repair of the
generator power cables between FS574.00 and FS559.00 + 112.00 and
add 2.0 hours for each repair of the generator power cables between
FS559.00 + 96.00 and FS559.00 + 80.00.
NOTE: These estimates do not include the man-hours necessary to remove and
install the furnishing panels or equipments that were installed with an
STC.
G. Material - - - Price and Availability
(1) The kit in the table that follows is available from Bombardier Commercial
Aircraft.
NOTE: For a list of kit contents, refer to paragraph 3.A.
KIT NUMBER NAME
601R24- - - 131K1 Protection of the Generator Power
Cable
(2) Refer to paragraph 3.B. for a list of consumables for this service bulletin.
For Business/Corporate Operators
All Business/Corporate operators (i.e. operators who do not have a commercial
airline operation) refer to SB 800-00-004 for commercial policy coverage and
logistics/planning arrangements (refer to www.cic.bombardier.com/technical
library/service bulletins/challenger/850/SB 800-00-004).
T o place an order for parts or kits, please call Bombardier Parts Logistics at
514-855-2999 or 1-866-538-1247.
H. T ooling - - - Price and Availability
There are no tool kits for this service bulletin. Refer to paragraph 3.C. for a list of
special tools and equipment for this service bulletin.

### Page 5

SERVICE BULLETIN 601R- - -24- - -131
SB 601R- - - 24- - - 131
Page 5 of 17
Jun 28/2012
I. Weight and Balance
WEIGHT ARM MOMENT ¡
+0 . 6l b + 662.8 in. + 0.398 (1000 lb-in.)
+0 . 2 7k g + 16.84 m + 0.0046 (1000 kg-m)
¡ The value in the Moment column is divided by 1000.
Refer to Weight and Balance Manual.
J. Electrical Load Data
Not changed.
K. References
Restriction and/or Special Instruction (RSI) C- - -A242.
Modification Summary TC601R18248, Revision A.
Repair Engineering Order (REO) 601R- - - 24- - - 21- - - 004.
Aircraft Maintenance Manual (AMM)
Structural Repair Manual (SRM)
Electrical/Electronic Components - - - Standard Practices Manual (ESPM)
Wiring Diagram Manual (WDM)
For Bombardier reference only: PCA 6582.
L. Other Publications Affected
None
M. Relationship Chart
Not applicable.

### Page 6

SERVICE BULLETIN 601R- - -24- - -131
SB 601R- - - 24- - - 131
Page 6 of 17
Jun 28/2012
2. ACCOMPLISHMENT INSTRUCTIONS
Reference Information
REFERENCE DESIGNATION
A M M 2 4 --- 0 0 --- 0 0 --- 9 1 0 --- 8 0 1 Electrical/Electronic Safety Precautions
A M M 2 4 --- 1 1 --- 0 1 --- 7 1 0 --- 8 0 1Operational T est of the Left IDG (With Engines
Started)
A M M 2 4 --- 1 1 --- 0 1 --- 7 1 0 --- 8 0 2Operational T est of the Right IDG (With Engines
Started)
A M M 2 5 --- 5 2 --- 0 1 --- 0 0 0 --- 8 0 1Removal of the Cargo Compartment Sidewall
Linings
A M M 2 5 --- 5 2 --- 0 1 --- 0 0 0 --- 8 0 2Removal of the Cargo Compartment Rear Bulk-
head Linings
A M M 2 5 --- 5 2 --- 0 1 --- 4 0 0 --- 8 0 1Installation of the Cargo Compartment Sidewall
Linings
A M M 2 5 --- 5 2 --- 0 1 --- 4 0 0 --- 8 0 2Installation of the Cargo Compartment Rear
Bulkhead Linings
E S P M 2 0 --- 0 0 --- 0 0 Standard Practices - - - Description and
Operation
E S P M 2 0 --- 1 2 --- 0 0 Wiring - - - Removal/Installation
S R M 5 1 --- 2 2 --- 3 8 Attaching Nylon Grommets and Nylon
Caterpillar- - -Protector Strips with Adhesive
S R M 5 1 --- 2 3 --- 0 0 Pressure, Environmental, Fuel T ank and Firewall
Sealing
S R M 5 1 --- 2 6 --- 0 0 Cleaning
T olerance Information
Linear T olerances Angular T olerance
X.XX in. (X.X mm) X.X in. (X mm)
+ / --- 0˚ 30”+/- - - 0.03 in. +/--- 0.1 in.
+ / --- 0 . 8 m m + / --- 3 m m
NOTE: The tolerances above apply to the dimensions given in this service
bulletin, except when specified differently.

### Page 7

SERVICE BULLETIN 601R- - -24- - -131
SB 601R- - - 24- - - 131
Page 7 of 17
Jun 28/2012
A. Job Set-Up
WARNING: OBEY ALL THE SAFETY PRECAUTIONS WHEN YOU DO
MAINTENANCE ON OR NEAR ELECTRICAL/ELECTRONIC
EQUIPMENT . IF YOU DO NOT OBEY THE SAFETY PRECAUTIONS,
INJURIES TO PERSONS AND/OR DAMAGE TO THE EQUIPMENT CAN
OCCUR.
(1) Obey all the electrical/electronic safety precautions (Refer
to AMM 24- - - 00- - - 00- - - 910- - - 801).
(2) Open, safety, and tag the circuit breakers that follow:
For Aircraft 7075, 7136, 7140, 7152, 7176, 7180, 7351, 7730, 7755, and 7763
CB PANEL CB NO. NAME ZONE
C B P --- 1 M2 ENG IGN A 221
C B P --- 1 M3 ENG IGN B 221
C B P --- 1 M4 ENG START R 221
C B P --- 1 M5 ENG START L 221
C B P --- 3 B7 ENG IGN A 221
C B P --- 4 B5 THRUST REV AUTO STOW 1 222
C B P --- 4 B6 THRUST REV AUTO STOW 2 222
C B P --- 4 B7 THRUST REV 1 222
C B P --- 4 B8 THRUST REV 2 222
C B P --- 5 B1 ENG IGN B 311
For Aircraft 8043, 8046 thru 8049, 8051 thru 8057, 8060, 8063, 8065 thru 8069, 8071 thru
8094, 8096 thru 8100, 8102, and 8104
CB PANEL CB NO. NAME ZONE
C B P --- 1 M3 ENG IGN B 221
C B P --- 1 M4 ENG START R 221
C B P --- 1 M5 ENG START L 221
C B P --- 3 B7 ENG IGN A 221

### Page 8

SERVICE BULLETIN 601R- - -24- - -131
SB 601R- - - 24- - - 131
Page 8 of 17
Jun 28/2012
CB PANEL ZONE NAMECB NO.
C B P --- 4 B5 THRUST REV AUTO STOW 1 222
C B P --- 4 B6 THRUST REV AUTO STOW 2 222
C B P --- 4 B7 THRUST REV 1 222
C B P --- 4 B8 THRUST REV 2 222
C B P --- 4 C6 ENG IGN A 222
C B P --- 5 B1 ENG IGN B 311
For all Aircraft
(3) Open the cargo-compartment door.
(4) Between FS559.00+80.00 and FS574.00, remove the applicable ceiling
panels to get access to the generator power cables (Refer to AMM
25- - - 52- - - 01- - - 000- - - 801).

### Page 9

SERVICE BULLETIN 601R- - -24- - -131
SB 601R- - - 24- - - 131
Page 9 of 17
Jun 28/2012
B. Procedure
NOTE: This procedure is applicable to the left and right sides. The procedure
that follows is written for the left side. The differences are given.
NOTE: This procedure is applicable to the generator power cables that are
identified as 1XA71A4AWHT / 1XA72A4BBLU / 1XA73A4CORN for the left
side and 2XA71A4AWHT / 2XA72A4BBLU / 2XA73A4CORN for the right
side.
Refer to Figure 1 .
(1) Between FS559.00+80.00 and FS559.00+96.00, and between stringers 2 and
3, do a visual inspection of the generator power cables for a damaged
insulation sleeve.
(2) Between FS559.00+112.00 and FS574.00, and between stringers 2 and 3, do
a visual inspection of the generator power cables for a damaged insulation
sleeve.
(3) If the insulation sleeve of the generator power cables is damaged and the wire
strands are not damaged, do a repair of the generator power cables as
follows:
(a) Between FS574.00 and FS621.00, remove the applicable ceiling panels
and sidewall lining panels to get access to the generator power cables
(Refer to AMM 25- - - 52- - - 01- - - 000- - - 801 and AMM 25- - - 52- - - 01- - - 000- - - 802).
CAUTION: DO NOT PULL TOO HARD ON THE GENERATOR POWER
CABLES. THIS CAN CAUSE DAMAGE TO THE INSULATION
SLEEVE.
(b) Between FS559.00+80.00 and FS621.00, remove the generator power
cables from the attachment points (standoffs, cable supports, cable ties)
as necessary to loosen the generator power cables near the damaged
area.
(c) Repair the damaged generator power cables with insulating tape (Refer
to REO 601R- - - 24- - - 21- - - 004).
(d) Between FS559.00+80.00 and FS621.00, attach the generator power
cables on the attachment points (standoffs, cable supports, cable ties)
that were removed.

### Page 10

SERVICE BULLETIN 601R- - -24- - -131
SB 601R- - - 24- - - 131
Page 10 of 17
Jun 28/2012
CAUTION: DO NOT DO A PERMANENT REPAIR TO THE GENERATOR POWER
CABLES IF THE WIRE STRANDS OF THE GENERATOR POWER
CABLES ARE DAMAGED. IF YOU DO, DAMAGE CAN OCCUR TO THE
ELECTRICAL GENERATION SYSTEM.
(4) If the wire strands of the generator power cables are damaged, speak with a
representative of Bombardier at the Bombardier Business Aircraft Customer
Response Center (CRC) at phone number 514-855-2999 or
1- - - 866- - - 538- - - 1247 or via email at ac.yul@aero.bombardier.com for a
disposition.
(5) If a support bracket is installed on the fuel tank support-brackets to hold the
generator power cables, speak with a representative of Bombardier at the
Bombardier Business Aircraft Customer Response Center (CRC) at phone
number 514-855-2999 or 1- - - 866- - - 538- - - 1247 or via email at
ac.yul@aero.bombardier .com for a disposition.
Refer to Figure 2 .
(6) Between FS559.00+80.00 and FS559.00+96.00, and between stringers 2 and
3, install the T eflon conduit (1) on the generator power cables as follows
(Refer to ESPM 20- - - 13- - - 00):
NOTE: If an equivalent type of Teflon conduit was installed on the generator
power cables before this service bulletin, it is not necessary to do this
step.
(a) Cut the T eflon conduit (1) along its length.
(b) Wrap the T eflon conduit (1) around the generator power cables.
(c) Make sure that the T eflon conduit (1) has an overlap of 0.5 in. (1.3 cm)
on the lower surface of the generator power cables.
(d) Attach the T eflon conduit (1) with two cable ties (2) to each end and two
cable ties (2) approximately at an equal distance from each other .
(7) Between FS559.00+112.00 and FS574.00 and between stringers 2 and 3,
install the T eflon conduit (1) on the generator power cables as follows (Refer
to ESPM 20- - - 13- - - 00):
NOTE: If an equivalent type of the Teflon conduit was installed on the generator
power cables before this service bulletin, it is not necessary to do this
step.

### Page 11

SERVICE BULLETIN 601R- - -24- - -131
SB 601R- - - 24- - - 131
Page 11 of 17
Jun 28/2012
(a) Cut the T eflon conduit (1) along its length.
(b) Wrap the T eflon conduit (1) around the generator power cables.
(c) Make sure that the T eflon conduit (1) has an overlap of 0.5 in. (1.3 cm)
on the lower surface of the generator power cables.
(d) Attach the T eflon conduit (1) with two cable ties (2) to each end and two
cable ties (2) approximately at an equal distance from each other .
(8) Between FS559.00+80.00 and FS559.00+96.00, and between stringers 2 and
3, install the edging grommets (3) on the fuel tank support-brackets as
follows:
(a) Clean the edges of the fuel tank support-brackets (Refer to SRM
51- - - 26- - - 00).
(b) Apply sealing compound on the edging grommets (3) and on the edges
of the fuel tank support-brackets (Refer to SRM 51- - - 23- - - 00).
(c) Install the edging grommets (3) on the edges of the fuel tank
support-brackets (Refer to SRM 51- - -22- - -38).
(9) Make sure that the overlap of the T eflon conduit (1) points in the direction of
the edging grommets (3) on the fuel tank support-brackets.
(10) Between FS559.00+112.00 and FS574.00, and between stringers 2 and 3,
install the edging grommets (3) on the fuel tank support-brackets as follows:
(a) Clean the edges of the fuel tank support-brackets (Refer to SRM
51- - - 26- - - 00).
(b) Apply sealing compound on the edging grommets (3) and on the edges
of the fuel tank support-brackets (Refer to SRM 51- - - 23- - - 00).
(c) Install the edging grommets (3) on the edges of the fuel tank
support-brackets (Refer to SRM 51- - -22- - -38).
(11) Make sure that the overlap of the conduit (1) points in the direction of the
edging grommets (3) on the fuel tank support-brackets.

### Page 12

SERVICE BULLETIN 601R- - -24- - -131
SB 601R- - - 24- - - 131
Page 12 of 17
Jun 28/2012
C. Job Close-Out
(1) Remove all tools, equipment, and unwanted materials from the work area.
(2) Remove the tags and close the circuit breakers that follow:
For Aircraft 7075, 7136, 7140, 7152, 7176, 7180, 7351, 7730, 7755, and 7763
CB PANEL CB NO. NAME ZONE
C B P --- 1 M2 ENG IGN A 221
C B P --- 1 M3 ENG IGN B 221
C B P --- 1 M4 ENG START R 221
C B P --- 1 M5 ENG START L 221
C B P --- 3 B7 ENG IGN A 221
C B P --- 4 B5 THRUST REV AUTO STOW 1 222
C B P --- 4 B6 THRUST REV AUTO STOW 2 222
C B P --- 4 B7 THRUST REV 1 222
C B P --- 4 B8 THRUST REV 2 222
C B P --- 5 B1 ENG IGN B 311
For Aircraft 8043, 8046 thru 8049, 8051 thru 8057, 8060, 8063, 8065 thru 8069, 8071 thru
8094, 8096 thru 8100, 8102, and 8104
CB PANEL CB NO. NAME ZONE
C B P --- 1 M3 ENG IGN B 221
C B P --- 1 M4 ENG START R 221
C B P --- 1 M5 ENG START L 221
C B P --- 3 B7 ENG IGN A 221
C B P --- 4 B5 THRUST REV AUTO STOW 1 222
C B P --- 4 B6 THRUST REV AUTO STOW 2 222
C B P --- 4 B7 THRUST REV 1 222
C B P --- 4 B8 THRUST REV 2 222

### Page 13

SERVICE BULLETIN 601R- - -24- - -131
SB 601R- - - 24- - - 131
Page 13 of 17
Jun 28/2012
CB PANEL ZONE NAMECB NO.
C B P --- 4 C6 ENG IGN A 222
C B P --- 5 B1 ENG IGN B 311
For all Aircraft
(3) If removed, install the applicable ceiling panels and/or sidewall lining panels
(Refer to AMM 25- - - 52- - - 01- - - 400- - - 801 and AMM 25- - - 52- - - 01- - - 400- - - 802).
(4) Close the cargo compartment door.
(5) If the insulation sleeve of the generator power cables that are installed on the
left side was repaired during the installation of this service bulletin, do the
operational test of the left IDG (Refer to AMM 24- - - 11- - - 01- - - 710- - - 801).
(6) If the insulation sleeve of the generator power cables that are installed on the
right side was repaired during the installation of this service bulletin, do the
operational test of the right IDG (Refer to AMM 24- - - 11- - - 01- - - 710- - - 802).
(7) When this service bulletin is completed, add the weight and balance data
shown in paragraph 1.I. of this service bulletin to the Weight and Balance
Manual. Under ‘Description of Change’ enter “Service Bulletin 601R- - - 24- - - 131,
incorporated.”
(8) When this service bulletin is completed, make this entry in the applicable
l o g b o o k s : “ E l e c t r i c a l P o w e r --- P r i m a r y A C --- G e n e r a t i o n S y s t e m --- I n s p e c t i o n
for Chafing and Installation of Protective Conduit on the Generator Power
Cables, incorporated.”

### Page 14

SERVICE BULLETIN 601R- - -24- - -131
SB 601R- - - 24- - - 131
Page 14 of 17
Jun 28/2012
Inspection Area on the Generator Power Cable
Figure 1
rsb601r24131_001.cgm
B
POWER
CABLE
(REF) FUEL TANK
SUPPORT- -
BRACKET (REF)
A
NOTE
Shaded area is
to be inspected.
LEFT SIDE SHOWN
RIGHT SIDE OPPOSITE
A
FS574.00
FS559.00
+112.00
FS567.00
FS559.00
+96.00
FS559.00
+80.00
FS559.00
+89.34
B
B
B
B
STGR 2
STGR 3

### Page 15

SERVICE BULLETIN 601R- - -24- - -131
SB 601R- - - 24- - - 131
Page 15 of 17
Jun 28/2012
Installation of the T eflon Conduit on the Generator Power Cable
Figure 2
rsb601r24131_002.cgm
D
POWER
CABLE
(REF) 2 2
23 3 1
1
1
1
A
C B
C
B C C--
FS574.00
FS559.00
+112.00
FS567.00
FS559.00
+96.00
FS559.00
+80.00
FS559.00
+89.34
STGR 2
STGR 3
D
D
D
D
LEFT SIDE SHOWN
RIGHT SIDE OPPOSITE
A
NOTE
O n ec a b l et i e( 2 )i s
installed on each end
of the teflon conduit (1)
and two cable ties (2) are
installed approximately
at an equal distance
from each other.
1
FUEL TANK
SUPPORT- -
BRACKET
(REF)3
4.00 in.
(10.2 cm)
REF 3
1
0.50 in.
(1.3 cm)
POWER
CABLE
(REF)
FUEL TANK
SUPPORT- -
BRACKET
(REF)
LEGEND
1. Conduit, teflon
S10155M3- -1600.
2. Cable tie
B0816019- -003.
3. Grommet, edging
MS21266- -4T .

### Page 16

SERVICE BULLETIN 601R- - -24- - -131
SB 601R- - - 24- - - 131
Page 16 of 17
Jun 28/2012
3. MATERIAL INFORMATION
A. Kit Information
Kit Contents:
KIT 601R24 - - -131K1¡
PART NUMBER QUANTITY NAME ALTERNATEPARTS NOTES
B0816019- - - 003 16 Cable tie
MS21266- - - 4T 8 Grommet, edging Length: 4.0 in.
(10.2 cm)
S10155M3- - - 1600 4 Conduit, T eflon
¡ Refer to paragraph 1.G. for special terms and conditions.
B. Consumable Information
The materials that follow are necessary to do this service bulletin. Y ou can order
them from Bombardier or purchased directly from industry sources. If the material
is ordered from Bombardier , there can be some lead time because of the shelf life
of the material.
CONSUMABLES
SPECIFICATION QUANTITY NAME REFERENCE
MIL- - - PRF- - - 81733,
Type I- - - 1/2,
Ty p e I I --- 1 / 2 , o r --- 2
As
necessary
Compound, sealing
and coating,
corrosion inhibitive
09- - - 009¡
MIL- - - I- - - 19166
or
A- - - A- - - 59163
or
S10155 Type C
As
necessary
Insulation tape
or
Insulation tape
or
Conduit, T eflon
05- - - 094¡
05- - - 089¡
05- - - 117¡

### Page 17

SERVICE BULLETIN 601R- - -24- - -131
SB 601R- - - 24- - - 131
Page 17 of 17
Jun 28/2012
SPECIFICATION REFERENCE NAMEQUANTITY
B0816019- - - 003 As
necessary
Cable tie 05- - - 147¡
¡ R e f e r t o A M M 5 1 --- 3 1 --- 0 0 --- 9 9 0 --- 8 0 1
NOTE: T o complete this list of consumables, refer to the different tasks that are
given as references in this service bulletin
C. Special T ools and Equipment
For a list of special tools and equipment, refer to the different tasks that are given
as references in this service bulletin.
D. Disposition of Parts
Not applicable.
1

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