BAS67050012 Rev NC
BAS67050012 Rev NC
Cover
http://www.cic.bombardier.com
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It is understood that this documentation, comprising technical data and other information in any media
shall not be reproduced or disclosed in whole or in part without Bombardier’s written authorization, is
proprietary and confidential to Bombardier and that all rights to patent, copyright, trademark, trade
secret and other intellectual property rights therein belong to Bombardier. Such documentation,
technical data and other information shall not be modified, translated, reverse assembled, reverse
engineered or de-compiled and shall be used solely to maintain, operate or repair the aircraft.
REVISION LOG
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REVISION RECORD
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BD-700 SUPPLEMENTAL MAINTENANCE INFORMATION
STC NUMBER: SA07-19, Water Proofing and Spill Management Interior Modifications
“Modification of an aircraft and issuance of a new or amended Type Certificate (TC) Data Sheet or a
Supplemental Type Certificate (STC) obligates the aircraft operator to include the following maintenance
information in the operator’s Aircraft Maintenance Manual and the operator’s Scheduled Aircraft Maintenance
Program as specified.”
It is not the intention of this document to supersede any information in the aircraft manuals, except in those areas
listed herein. The information in this document is presented in ATA-100 format; however, minor deviations may
be encountered.
For Canadian registered aircraft, “The Airworthiness Limitations section is approved by the Minister and
specifies maintenance required by any applicable airworthiness or operating rule, unless an alternative program
has been approved by the Minister.”
For US registered aircraft, “The Airworthiness Limitations section is FAA-approved and specifies maintenance
required under Sec. 43.16 and 91.403 of the Federal Aviation Regulations, unless an alternative program has
been FAA approved.”
This cover sheet and the documents listed in numbered paragraphs 1. through 4. below constitute the ICA.
1. Maintenance manual information (system description, operation, location, removal, installation, testing, etc.)
is contained in the Supplemental Maintenance Manual number BAS67050012-SMM Revision NC.
2. Line Replaceable Unit (LRU) part numbers and other necessary part numbers are contained in the
Supplemental IPC number BAS67050012-IPC Revision NC.
3. Scheduled Maintenance program tasks are contained in the Supplemental Time Limits/Maintenance
Checks - Scheduled Maintenance manual number BAS67050012-TLMC Revision NC. The existing
maintenance program tasks, as defined in the production Aircraft Maintenance Manual, remain in effect for
the applicable aspects of this STC.
4. This ICA does not generate any additional Airworthiness Limitations. The existing Airworthiness Limitations,
as defined in the production Aircraft Maintenance Manual, remain in effect for the applicable aspects of this
STC.
Bombardier, Inc.
Mar 6/2009
BD-700 SUPPLEMENTAL MAINTENANCE INFORMATION
Mar 6/2009
BAS67050012-TLMC
Cover
http://www.cic.bombardier.com
Distribution
FAX 514-855-2535
Ordering
E-mail bbad.user.comments@aero.bombardier.com
It is understood that this documentation, comprising technical data and other information in any media
shall not be reproduced or disclosed in whole or in part without Bombardier’s written authorization, is
proprietary and confidential to Bombardier and that all rights to patent, copyright, trademark, trade
secret and other intellectual property rights therein belong to Bombardier. Such documentation,
technical data and other information shall not be modified, translated, reverse assembled, reverse
engineered or de-compiled and shall be used solely to maintain, operate or repair the aircraft.
INTRODUCTION
General
This document contains the manufacturers’ recommended time limits for inspections and scheduled
maintenance checks for the components installed during the modification of this aircraft. This document is
supplementary to the BD-700 Time Limits/Maintenance Checks manual.
Scheduled maintenance, time limits, and inspections are presented in a columnar format. This information
cross-references detailed procedures in the associated Supplemental Maintenance Manual (SMM).
Organization
• The first column identifies the location of the instructions required to perform the task. The applicable
task number in the SMM published for the aircraft is identified.
• The second column of this section contains the Bombardier assigned chapter 5 task number.
• The third column of this section contains the task title. For task title definitions refer to BD-700 Time
Limits/Maintenance Checks, INTRODUCTION, Part 1, 5-00-05, Program Glossary and Definitions.
• The fourth column of this section contains the inspection interval for each maintenance task.
The maintenance program is based on tasks prescribed at specific intervals and identified as “A”
Checks or “C” Checks. The task intervals consist of basic intervals and multiple intervals (in flight
hours for “A” Checks and in months for the “C” Checks). Each task is to be performed at the interval
indicated (A, 2A, etc. or C, 2C, etc.) for the task, so that both the applicable basic as well as the
multiple interval tasks are performed, as required. The check intervals are identified as follows:
• These columns may include a note in the heading or in the column. These notes are explained in the
notes section appearing at the end of the section.
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TABLE OF CONTENTS
25-30-90-210-801 25-30-90-601 General Visual Inspection of Galley Floor Attachment Point Covers C
TIME LIMITS/MAINTENANCE CHECKS
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TIME LIMITS/MAINTENANCE CHECKS
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NOTE: This list is effective at the date of publishing, no update will be provided.
Note Description
1 Intervals given are either Flight Hours (H), Months (M), Landings (L), or sequential checks (A, C) per BD-700 TLMC
section 5-20-05.
Extension tolerances for intervals shall be in accordance with the BD-700 Maintenance Planning Document (MPD).
The application of rules established for the Flexible Maintenance Program is acceptable where local regulatory
authorities permit.
2 Refer to Supplemental Maintenance Manual document number BAS67050012-SMM for task procedures.
BD-700 SUPPLEMENTAL TIME LIMITS/MAINTENANCE CHECKS
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BAS67050012-SMM
Cover
Supplemental
Maintenance Manual
http://www.cic.bombardier.com
Distribution
FAX 514-855-2535
Ordering
E-mail bbad.user.comments@aero.bombardier.com
It is understood that this documentation, comprising technical data and other information in any media
shall not be reproduced or disclosed in whole or in part without Bombardier’s written authorization, is
proprietary and confidential to Bombardier and that all rights to patent, copyright, trademark, trade
secret and other intellectual property rights therein belong to Bombardier. Such documentation,
technical data and other information shall not be modified, translated, reverse assembled, reverse
engineered or de-compiled and shall be used solely to maintain, operate or repair the aircraft.
INTRODUCTION
General
This Supplemental Maintenance Manual (SMM) contains information describing custom installation(s) and
modification(s) to this aircraft, and may include procedures for periodic maintenance. The SMM should be
used concurrently with the Aircraft Maintenance Manual (AMM) for maintenance activities. This manual does
not supersede the AMM, except in those instances where a custom installation or modification has completely
replaced a production-installed system. This manual was published and released in accordance with the latest
technical data available at the time of publication.
Organization
Content and format of the SMM is based on the ATA-100 Specification and standard conventions. This
maintenance information is organized according to ATA chapter designation. A separate table of contents is
provided for each chapter. The information within each chapter may be organized under one or more of the
following subject categories and page number identifiers. These categories need not all be included in every
chapter.
System Descriptions - - - - - - - - - - - - Pages 1 - 99
Maintenance Practices - - - - - - - - - - - Pages 201 - 299
Servicing - - - - - - - - - - - - - - - - - - Pages 301 - 399
Removal/Installation - - - - - - - - - - - - Pages 401 - 499
Adjustment/Test - - - - - - - - - - - - - - Pages 501 - 599
Inspection/Check - - - - - - - - - - - - - - Pages 601 - 699
This supplemental maintenance manual may reference a manufacturer’s maintenance document or the AMM
for additional maintenance procedures. Unless identified in the manufacturer’s maintenance document(s),
specific parts identified for maintenance and/or replacement in the SMM are also identified in the Supplemental
Illustrated Parts Catalog.
Figures such as tables, diagrams, illustrations, or photographs may be provided to assist with system or
component identification or location. Figures in pages 1 through 99 are identified by title; other figures are
numbered consecutively within each page block.
Warnings, cautions, or notes may be included in various sections of the text. It is important to understand the
significance of each:
WARNING: WARNING STATEMENTS IDENTIFY METHODS, PROCEDURES, OR LIMITS THAT MUST
BE PRECISELY FOLLOWED TO AVOID INJURY TO PERSONS.
CAUTION: CAUTION STATEMENTS IDENTIFY PROCESSES THAT MUST BE FOLLOWED TO AVOID
DAMAGE TO EQUIPMENT.
NOTE: Notes call attention to details which may make the job easier.
• The configuration necessary for your task does not cause an unsafe condition for the other tasks.
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CHAPTER 11 - PLACARDS
AND MARKINGS
List of Effective Pages BD-700 SUPPLEMENTAL MAINTENANCE MANUAL
TABLE OF CONTENTS
1. General
This chapter shows the additional internal placards, labels, and markings that are necessary for safety
and instructions for persons.
2. Component Location
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A C
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B
(VIEW LOOKING OUTBOARD)
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B. Procedure
(1) Do a general visual inspection of the interior cabin and make sure that the added placards
are installed and that the placards can be read. Refer to the DESCRIPTION/OPERATION
section for location of the placards.
C. Close Out
(1) Remove all tools, equipment, and unwanted materials from the work area.
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CHAPTER 25 - EQUIP-
MENT/FURNISHINGS
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CHAPTER 25 - EQUIPMENT/FURNISHINGS
CHAPTER 25 - EQUIPMENT/FURNISHINGS
TABLE OF CONTENTS
1. General
This section provides general information about sealing of the galley and galley annex attachment points
to prevent water damage to aircraft components.
2. Component Location
Refer to Figure 1.
3. Component Description
The floor attachment point cover is a one-piece Lexan assembly that is bonded over each galley
floor attachment point. The cover prevents water from seeping through the attachment point.
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FLOOR ATTACHMENT
POINT COVER
A
(TYPICAL AT EACH ATTACHMENT POINT)
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A. Reference Information
REFERENCE DESIGNATION
B. Consumable Materials
MANUFACTURERS’ REFERENCE
REFERENCE DESIGNATION
AND/OR SPECIFICATION
C. Job Set-Up
NOTE: The galley attachment points must be resealed whenever the covers are disturbed during
maintenance.
(1) Remove all loose items from the galley lower storage areas.
(2) Remove all lower drawers from the galley and galley annex (if installed).
D. Procedure
CAUTION: DO NOT TRY TO PULL THE POLYURETHANE TAPE FROM THE GALLEY FLOOR
PANEL. THE ADHESIVE BOND IS STRONG ENOUGH TO DELAMINATE THE
GALLEY FLOOR PANEL IF FORCED.
(a) Cut the polyurethane tape around the attachment point cover.
(b) Carefully pry the attachment point cover to break the adhesive sealant.
(d) Remove the adhesive sealant from the attachment point cover and the galley floor
panel (AMM TASK 51-23-00-100-801).
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(b) Make sure all mating surfaces are clean and free of old sealant.
1 If the cover interferes with galley structure, trim to provide proper fit.
(d) Use RTV108 sealant and do faying surface sealing of the cover to the galley floor
panel.
NOTE: RTV108 becomes tack free in 20 minutes but will require 7 days to fully cure.
(e) Use RTV108 sealant and do fillet sealing around the edges of the cover.
(f) Install the polyurethane protective tape over the galley attachment point.
1 Make sure that there is a minimum run-out of 1.12 inches (28.4mm) around the
cover edge.
E. Close Out
(1) Remove all tools, equipment, and unwanted materials from the galley cabinet area.
(3) Install all lower drawers in the galley and galley annex (if installed).
(4) Check the lower galley and galley annex (if installed) drawers for proper operation and
latching.
(5) Put all the loose items back in the galley lower storage areas.
(6) Remove all tools, equipment, and unwanted materials from the work area.
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B. Job Set-Up
(1) Remove all loose items from the galley lower storage areas.
(2) Remove all lower drawers from the galley and galley annex (if installed).
C. Procedure
(1) Make sure each floor attachment point has a cover installed.
(2) Check each floor attachment point cover for security of installation. Cover should have no
evidence of looseness and sealant securing the cover should not be broken, have voids, or
be missing.
(3) Check each floor attachment point cover for damage or cracks.
D. Close Out
(1) Remove all tools, equipment, and unwanted materials from the work area.
(3) Install all lower drawers in the galley and galley annex (if installed).
(4) Check the lower galley and galley annex (if installed) drawers for proper operation and
latching.
(5) Put all the loose items back in the galley lower storage areas.
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BAS67050012-IPC
Cover
Supplemental
Illustrated Parts Catalog
http://www.cic.bombardier.com
Distribution
FAX 514-855-2535
Ordering
E-mail bbad.user.comments@aero.bombardier.com
It is understood that this documentation, comprising technical data and other information in any media
shall not be reproduced or disclosed in whole or in part without Bombardier’s written authorization, is
proprietary and confidential to Bombardier and that all rights to patent, copyright, trademark, trade
secret and other intellectual property rights therein belong to Bombardier. Such documentation,
technical data and other information shall not be modified, translated, reverse assembled, reverse
engineered or de-compiled and shall be used solely to maintain, operate or repair the aircraft.
INTRODUCTION
General
The Supplemental Illustrated Parts Catalog (IPC) is used to identify line replaceable parts installed during the
modification of the aircraft. This catalog is a companion document to the Supplemental Maintenance Manual
that describes the aircraft modification(s). For information regarding replacement part numbers of production-
installed equipment, please refer to the original production manuals.
Organization
The format and organizational structure of the Supplemental IPC is based on the ATA-100 specification. Each
chapter contains subsections that begin with a title page and are identified by a six-digit ATA number. Parts are
listed in their applicable ATA-100 chapters and sections.
Illustrations
Illustrations precede their corresponding parts list. The figure title corresponds to the associated parts list.
Illustrations may include a detail bubble which leads to an enlarged view on the same or the following page.
The enlarged view will be identified by the same detail bubble shown on the parent illustration. To enable a
parts list to start on an odd-numbered page per ATA-100 requirements, the associated illustration page may be
preceded by a blank page.
Parts List
The parts in each chapter are listed under their associated assembly drawing number. The parts under the
primary assembly number are preceded by one period (.) and shown as indented one level. When an
assembly includes subassemblies, these parts are preceded by two periods (..) and shown as indented two
levels. If additional subassemblies are required, a third or fourth level of indenture may be used.
If two or more assemblies share a large number of identical parts, these parts may be grouped together under
the drawing/part number prefix in the “Part Number” column and be shown with an “-XX” suffix. Each part
number suffix appears after the assembly description in the “Nomenclature” column, e.g., (-97, -101, -105).
Items unique to only one assembly will be labeled accordingly, e.g., (-105 only). The “Units per Assy” column
represents only the number of parts required for one assembly.
Grouped
assemblies
} Parts common
to all assemblies
Parts unique to
one assembly
Indenture
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When an OEM part is assigned a different part number by the completion center, the original manufacturer’s
part number may be shown in brackets following the item description. If an alternate item can be used as a
substitute part, it will be shown with an “A” following the item number in the “Fig. Item” column, e.g., 203A. The
word “ALTERNATE” will be placed in parentheses following the item description at the next indenture level.
Vendor codes or vendor names are provided, when available. They are shown in parentheses following an
item description in the “Nomenclature” column. The vendor code can be used to locate the vendor name,
address, and telephone number in the vendor list included in this supplement. Part numbers starting with CL,
TM, or M are assigned by Bombardier, Inc., Learjet, or Canadair. Standard parts, starting with MS, AN, or
NAS, do not carry vendor codes since they are based upon Military Specifications, Army/Navy, or National
Aircraft Specifications, respectively.
Vendor
code
Alternate part
Interior Furnishings
Some items listed in this supplement may require a special finish, plating, color, or size that is not specified in
the part number or nomenclature. When ordering parts that may fall into these categories, please refer to your
Aircraft Interior Specification to determine the particular requirement(s). If the special ordering number is not
known when this IPC is published, it will be shown as “XX” in the part number.
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Vendor List
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CHAPTER 11 - PLACARDS
List of Effective Pages
BD-700 SUPPLEMENTAL ILLUSTRATED PARTS CATALOG
CHAPTER 11 - PLACARDS
CHAPTER 11 - PLACARDS
TABLE OF CONTENTS
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GALLEY (TYPICAL)
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NOMENCLATURE UNITS
FIG. ITEM PART NUMBER
1 2 3 4 5 6 7 PER ASSY
1 -1 BAS67038558-1 GALLEY SINK TAMBOR DOOR PLACARD INSTL NP
5 S40073-1 . PLACARD (BLACK LETTERING) (3AJ74) 1
-5A S40073-2 . . PLACARD (WHITE LETTERING) (ALTERNATE) (3AJ74)
A C
A
(VIEW LOOKING DOWN)
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B
(VIEW LOOKING OUTBOARD)
D
6
C
(VIEW LOOKING DOWN)
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NOMENCLATURE UNITS
FIG. ITEM PART NUMBER
1 2 3 4 5 6 7 PER ASSY
2 -1 BAS67038563-3 PLACARD INSTALLATION NP
5 BAS67038563-103 . PLACARD (3AJ74) 3
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NOMENCLATURE UNITS
FIG. ITEM PART NUMBER
1 2 3 4 5 6 7 PER ASSY
3 -1 BAS67038560-X GALLEY AND GALLEY ANNEX WATER SEALING NP
MODIFICATION (PLACARDS)
5 BAS67038560-115 . PLACARD (3AJ74) AR
10 BAS67038560-117 . PLACARD (3AJ74) AR
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CHAPTER 25 - EQUIPMENT/
FURNISHINGS
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CHAPTER 25 - EQUIPMENT/FURNISHINGS
CHAPTER 25 - EQUIPMENT/FURNISHINGS
TABLE OF CONTENTS
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5
15
10
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NOMENCLATURE UNITS
FIG. ITEM PART NUMBER
1 2 3 4 5 6 7 PER ASSY
1 -1 BAS67037560-3 SEALING MODIFICATION NP
5 BAS67037560-101 . COVER (3AJ74) AR
10 RTV108 . SEALANT ADHESIVE (24446) AR
15 8694 . POLYURETHANE PROTECTIVE TAPE (1A9T3) AR
5
15
10
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NOMENCLATURE UNITS
FIG. ITEM PART NUMBER
1 2 3 4 5 6 7 PER ASSY
2 -1 BAS67037560-7 SEALING MODIFICATION NP
5 700D016481-3 . COVER (3AJ74) AR
10 RTV108 . SEALANT ADHESIVE (24446) AR
15 8694 . POLYERETHANE PROTECTIVE TAPE (1A9T3) AR
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