(a) EFFECTIVE DATE
This AD becomes effective September 25, 2014.
(b) AFFECTED ADS
This AD replaces AD 2005-15-04, Amendment 39-14193 (70 FR 43032, July
26, 2005).
(c) APPLICABILITY
This AD applies to Bombardier, Inc. airplanes, certificated in any
category, as identified in paragraphs (c)(1) through (c)(4) of this
AD.
(1) Model CL-600-1A11 (CL-600) airplanes, serial numbers 1004 through 1085
inclusive.
(2) Model CL-600-2A12 (CL-601) airplanes, serial numbers 3001 through 3066
inclusive;
(3) Model CL-600-2B16 (CL-601-3A and CL-601-3R Variants) airplanes, serial
numbers 5001 through 5194 inclusive.
(4) Model CL-600-2B16 (CL-604 Variant) airplanes, serial numbers 5301
through 5573 inclusive, 5579, and 5595.
(5) This AD requires revisions to certain operator maintenance documents
to include new actions (e.g., inspections). Compliance with these
actions is required by 14 CFR 91.403(c). For airplanes that have been
previously modified, altered, or repaired in the areas addressed by
this AD, the operator may not be able to accomplish the actions
described in the revisions. In this situation, to comply with 14 CFR
91.403(c), the operator must request approval for an alternative
method of compliance according to paragraph (r) of this AD. The
request should include a description of changes to the required
actions that will ensure the continued damage tolerance of the
affected structure.
(d) SUBJECT
Air Transport Association (ATA) of America Code 32, Landing Gear.
(e) REASON
This AD was prompted by reports that landing gear parts that have
safe-life limits but do not have serial numbers (S/Ns) or part numbers
(P/Ns) can be removed from one landing gear and re-installed on
another, making tracking difficult. We are issuing this AD to prevent
life-limited landing gear parts from being used beyond their safe-life
limits, which could lead to collapse of the landing gear.
(f) COMPLIANCE
Comply with this AD within the compliance times specified, unless
already done.
(g) RETAINED REQUIREMENT TO ADD S/NS OR P/NS
This paragraph restates the actions required by paragraph (f) of AD
2005-15-04, Amendment 39-14193 (70 FR 43032, July 26, 2005), with
revised affected airplanes. Except for Model CL-600-2B16 airplanes
having S/Ns 5514 through 5595 inclusive: At the applicable compliance
time specified in paragraph (g)(1), (g)(2), or (g)(3) of this AD, add
serial numbers and part numbers, as applicable, to the parts
identified in the applicable service bulletin specified in paragraph
(g)(1), (g)(2), or (g)(3) of this AD. Do all actions in accordance
with the applicable service bulletin specified in paragraph (g)(1),
(g)(2), or (g)(3) of this AD.
(1) For parts identified in Bombardier Service Bulletin 600-0710, Revision
01, dated December 15, 2003; and Bombardier Service Bulletin 601-0546,
Revision 01, dated December 15, 2003; as having a compliance time of
"five years for the parts listed in Part A": Within 60 months after
August 30, 2005 (the effective date of AD 2005-15-04, Amendment 39
-14193 (70 FR 43032, July 26, 2005)).
(2) For parts identified in Bombardier Service Bulletin 600-0710, Revision
01, dated December 15, 2003; and Bombardier Service Bulletin 601-0546,
Revision 01, dated December 15, 2003; as having a compliance time of
"ten years for the parts listed in Part B": Within 120 months after
August 30, 2005 (the effective date of AD 2005-15-04, Amendment 39
-14193 (70 FR 43032, July 26, 2005)).
(3) For parts identified in Bombardier Service Bulletin 604-32-014, dated
May 31, 2002, as having a compliance time of "no later than a calendar
time of 8 years": Within 96 months after August 30, 2005 (the
effective date of AD 2005-15-04, Amendment 39-14193 (70 FR 43032, July
26, 2005)).
Note 1 to paragraph (g) of this AD: The Bombardier service bulletins
identified in paragraphs (g)(1), (g)(2), and (g)(3) of this AD refer to
the Messier-Dowty service bulletins identified in table 1 to paragraph (g)
of this AD as additional sources of guidance for adding part numbers or
serial numbers by vibro-peening the numbers on main landing gear (MLG) and
nose landing gear (NLG) components that do not have them; and for
determining the number of landings for parts without a part number or
serial number on which the time since new (TSN) and cycles since new (CSN)
have not been tracked.
TABLE 1 TO PARAGRAPH (G) OF THIS AD - MESSIER-DOWTY SERVICE BULLETINS
__________________________________________________________________________
CORRESPONDING
BOMBARDIER MESSIER-DOWTY
LANDING GEAR SERVICE SERVICE
MODEL COMPONENT BULLETIN(S) BULLETIN
__________________________________________________________________________
CL-600-1A11 MLG side strut 600-0710 and M-DT SB104467009/
(CL-600), retraction 601-0546. 010-32-1, dated
CL-600-2A12 actuator eye March 19, 2001.
(CL-601) and bolt.
CL-600-2B16
(CL-601-3A and
CL-601-3R)
airplanes.
CL-600-2B16 MLG shock strut 604-32-014 M-DT SB19090-32-4
(CL-604) dated March 19,
airplanes 2001.
CL-600-2B16 NLG shock strut 604-32-014 M-DT SB20020-32-5
(CL-604) dated July 12,
airplanes 2001.
CL-600-1A11 NLG drag brace 600-0710 M-DT SB200814001-
(CL-600), hinge pin. and 601-0546. 32-3, dated March
CL-600-2A12 19, 2001.
(CL-601) and
CL-600-2B16
(CL-601-3A and
CL-601-3R)
airplanes.
CL-600-1A11 MLG shock strut 600-0710 M-DT SB200922001/
(CL-600) 2-32-6, dated
airplanes March 19, 2001.
CL-600-1A11 NLG shock strut 600-0710 M-DT SB200924003/
(CL-600) 004-32-16, dated
airplanes July 12, 2001.
CL-600-2A12 MLG shock strut 601-0546 M-DT SB6100-32-10
(CL-601) and pin dated March 19,
CL-600-2B16 2001.
(CL-601-3A
and CL-601-3R)
airplanes.
CL-600-1A11 MLG side strut 600-0710 M-DT SB6500-32-1,
(CL-600), retraction and 601-0546. dated March 19,
CL-600-2A12 actuator. 2001.
(CL-601) and
CL-600-2B16
(CL-601-3A and
CL-601-3R)
airplanes.
CL-600-1A11 NLG drag brace 600-0710 M-DT SB7200-32-6,
(CL-600), hinge pin. and 601-0546. dated March 19,
CL-600-2A12 2001.
(CL-601) and
CL-600-2B16
(CL-601-3A and
CL-601-3R)
airplanes.
CL-600-2A12 NLG shock strut 601-0546 M-DT SB7300-32-16
(CL-601) and dated July 12,
CL-600-2B16 2001.
(CL-601-3A and
CL-601-3R)
airplanes.
__________________________________________________________________________
(h) RETAINED REQUIREMENT - ESTABLISHMENT OF THE NUMBER OF LANDINGS
This paragraph restates the actions required by paragraph (g) of AD
2005-15-04, Amendment 39-14193 (70 FR 43032, July 26, 2005), with
revised affected airplanes. Except for Model CL-600-2B16 airplanes
having S/Ns 5314 through 5595 inclusive: At the applicable time
specified in paragraph (g) of this AD, if a component does not have a
serial number and the CSN or TSN were not tracked, use the formula in
the applicable Messier-Dowty service bulletin specified in table 1 to
paragraph (g) of this AD to establish the TSN or CSN, and record the
newly calculated TSN or CSN in the airplane log books.
(i) RETAINED REQUIREMENT TO REVISE THE AIRWORTHINESS LIMITATIONS SECTION
(ALS)
This paragraph restates the revision required by paragraph (h) of AD
2005-15-04, Amendment 39-14193 (70 FR 43032, July 26, 2005), with
revised affected airplanes. Except for Model CL-600-2B16 airplanes
having S/Ns 5514 through 5595 inclusive: Within 30 days after August
30, 2005 (the effective date of AD 2005-15-04), revise the ALS of the
applicable Instructions for Continued Airworthiness to reflect the new
life limits of the landing gear parts by inserting copies of the
Canadair temporary revisions (TR) specified in table 2 to paragraph
(i) of this AD into the ALS of the applicable Canadair Time
-Limits/Maintenance Check Manual. When the contents of the TRs are
included in the general revisions of the ALS, these TRs may be removed
provided the relevant information in the ALS is identical to that in
the TRs.
TABLE 2 TO PARAGRAPH (I) OF THIS AD - CANADAIR TEMPORARY REVISIONS
__________________________________________________________________________
APPLICABLE
CANADAIR CANADAIR TIME-
TEMPORARY MANUAL LIMITS/MAINTENANCE
MODEL REVISION SECTION CHECK MANUAL
__________________________________________________________________________
CL-600-1A11 (CL-600) 5-116, dated 5-10-10 PSP 605.
airplanes April 11, 2002.
CL-600-2A12 (CL-601) 5-190, dated 5-10-10 PSP 601-5.
and CL-600-2B16 (CL- April 11, 2002.
601-3A and CL-601-3R)
airplanes.
CL-600-2A12 (CL-601) 5-191, dated 5-10-11 PSP 601-5.
and CL-600-2B16 (CL- April 11, 2002.
601-3A and CL-601-3R)
airplanes.
CL-600-2A12 (CL-601) 5-192, dated 5-10-12 PSP 601-5.
and CL-600-2B16 (CL- April 11, 2002.
601-3A and CL-601-3R)
airplanes.
CL-600-2B16 (CL-604) 5-2-6, dated 5-10-10 CL-604.
airplanes April 11, 2002.
CL-600-2A12 (CL-601) 5-204, dated 5-10-10 PSP 601A-5.
and CL-600-2B16 (CL- April 11, 2002.
601-3A and CL-601-3R)
airplanes.
CL-600-2A12 (CL-601) 5-205, dated 5-10-11 PSP 601A-5.
and CL-600-2B16 (CL- April 11, 2002.
601-3A and CL-601-3R)
airplanes.
CL-600-2A12 (CL-601) 5-206, dated 5-10-12 PSP 601A-5.
and CL-600-2B16 (CL- April 11, 2002.
601-3A and CL-601-3R)
airplanes.
__________________________________________________________________________
(j) RETAINED PARTS INSTALLATION LIMITATION
This paragraph restates the limitations specified in paragraph (i) of
AD 2005-15-04, Amendment 39-14193 (70 FR 43032, July 26, 2005), with
revised affected airplanes. Except for Model CL-600-2B16 airplanes
having serial numbers 5514 through 5595 inclusive: As of August 30,
2005 (the effective date of AD 2005-15-04), no person may install on
any airplane a landing gear part, unless it has had the applicable
part number or serial number added in accordance with paragraph (g) of
this AD; and has had the number of landings established in accordance
with paragraph (h) of this AD.
(k) RETAINED STIPULATION OF INFORMATION OF NO REPORTING
This paragraph restates the stipulation specified in paragraph (j) of
AD 2005-15-04, Amendment 39-14193 (70 FR 43032, July 26, 2005).
Although the service bulletins identified in paragraph (g) of this AD
specify that operators should submit incorporation notices to
Bombardier after each new part number or serial number and landings
assigned to these parts is added, this AD does not include that
action.
(l) NEW REQUIREMENT OF THIS AD: ADD SERIAL NUMBERS AND PART NUMBERS
(1) For Model CL-600-2B16 (CL-604 Variant) airplanes: Within 96 months
after the effective date of this AD, add serial numbers and part
numbers, as applicable, to the parts identified in paragraphs
(l)(1)(i) and (l)(1)(ii) of this AD, as applicable, in accordance with
the Accomplishment Instructions of Bombardier Service Bulletin 604-32
-014, Revision 02, dated May 9, 2011, including Appendix 1, dated May
9, 2011, and Service Bulletin Information Sheet, dated July 6, 2010.
(i) For airplanes having S/Ns 5301 through 5513 inclusive: Main fitting/
drag stay pin of the NLG having P/N 200811721.
(ii) For airplanes having S/Ns 5301 through 5573 inclusive, 5579 and 5595:
NLG crossbeam pins having P/N 200814601 and NLG center hinge pins
having P/N 200814624.
(2) For Bombardier Model CL-600-2A12 (CL-601) airplanes and Model CL-600-
2B16 (CL-601-3A and CL-601-3R Variants) airplanes: Within 60 months
after the effective date of this AD, add serial numbers and part
numbers, as applicable, to left and right MLG side strut pins having
P/N 6318-1 or 6318-3; and to left and right MLG hinge pins having P/N
6329-3; in accordance with the Accomplishment Instructions of
Bombardier Service Bulletin 601-0546, Revision 03, dated May 9, 2011,
including Appendix 1, dated May 9, 2011, and Service Bulletin
Information Sheet, dated July 6, 2010.
(3) For Bombardier Model CL-600-2A12 (CL-601) airplanes and Model CL-600-
2B16 (CL-601-3A and CL-601-3R Variants) airplanes: Within 120 months
after the effective date of this AD, add serial numbers and part
numbers, as applicable, to NLG main fitting/drag stay pins having P/N
200811721; NLG drag brace pivot pins having P/N 200814601; and left
and right MLG pintle pins having P/N 6324-1; in accordance with the
Accomplishment Instructions of Bombardier Service Bulletin 601-0546,
Revision 03, dated May 9, 2011, including Appendix 1, dated May 9,
2011, and Service Bulletin Information Sheet, dated July 6, 2010.
(4) For Bombardier Model CL-600-1A11 (CL-600) airplanes: Within 120 months
after the effective date of this AD, add serial numbers and part
numbers, as applicable, to NLG main fitting/drag stay pins having P/N
200811721 and NLG drag brace pivot pins having P/N 200814601, in
accordance with the Accomplishment Instructions of Bombardier Service
Bulletin 600-0710, Revision 03, dated May 9, 2011, including Appendix
1, dated May 9, 2011, and Service Bulletin Information Sheet, dated
July 6, 2010.
(m) NEW REQUIREMENT OF THIS AD: ESTABLISH THE NUMBER OF LANDINGS (CSN)
At the applicable times specified in paragraph (l) of this AD: If a
component does not have a serial number and the CSN were not tracked,
use Appendix 1, dated May 9, 2011, of the applicable service bulletin
specified in paragraph (m)(1), (m)(2), or (m)(3) of this AD to
establish the number of landings (CSN).
(1) Bombardier Service Bulletin 604-32-014, Revision 02, dated May 9, 2011
including Service Bulletin Information Sheet, dated July 6, 2010 (for
Bombardier Model CL-600-2B16 (CL-604 Variant) airplanes).
(2) Bombardier Service Bulletin 601-0546, Revision 03, dated May 9, 2011,
including Service Bulletin Information Sheet, dated July 6, 2010 (for
Model CL-600-2A12 (CL-601) airplanes and Model CL-600-2B16 (CL-601-3A
and CL-601-3R Variants) airplanes).
(3) Bombardier Service Bulletin 600-0710, Revision 03, dated May 9, 2011,
including Service Bulletin Information Sheet, dated July 6, 2010 (for
Bombardier Model CL-600-1A11 (CL-600) airplanes).
(n) NEW REQUIREMENT OF THIS AD: RECORDS UPDATE
Concurrently with the actions specified in paragraphs (l) and (m) of
this AD: Record any newly calculated CSN, new part numbers, and new
serial numbers in the airplane technical records and manuals.
(o) NEW REQUIREMENT OF THIS AD: PARTS INSTALLATION LIMITATION
As of the effective date of this AD, no person may install on any
airplane a landing gear part identified in paragraph (l) of this AD,
unless it has had the applicable part number or serial number added as
required by paragraph (l) of this AD, and had the CSN established as
required by paragraph (m) of this AD.
(p) NEW ACTION OF THIS AD: OPTIONAL METHOD OF COMPLIANCE
Accomplishing the action required by paragraph (g) of this AD, in
accordance with the Accomplishment Instructions of the applicable
service bulletin specified in paragraph (p)(1), (p)(2), or (p)(3) of
this AD, is acceptable for compliance with the requirements of
paragraph (g) of this AD.
(1) Bombardier Service Bulletin 601-0546, Revision 03, dated May 9, 2011,
including Appendix 1, dated May 9, 2011, and Service Bulletin
Information Sheet, dated July 6, 2010 (for Model CL-600-2A12 (CL-601)
airplanes and Model CL-600-2B16 (CL-601-3A and CL-601-3R Variants)
airplanes).
(2) Bombardier Service Bulletin 604-32-014, Revision 02, dated May 9, 2011
including Appendix 1, dated May 9, 2011, and Service Bulletin
Information Sheet, dated July 6, 2010 (for Model CL-600-2B16 (CL-604
Variant) airplanes).
(3) Bombardier Service Bulletin 600-0710, Revision 03, dated May 9, 2011,
including Appendix 1, dated May 9, 2011, and Service Bulletin
Information Sheet, dated July 6, 2010 (for Model CL-600-1A11 (CL-600)
airplanes).
(q) CREDIT FOR PREVIOUS ACTIONS
(1) This paragraph provides credit for the actions required by paragraph
(g) of this AD, if those actions were performed before August 30, 2005
(the effective date of AD 2005-15-04, Amendment 39-14193 (70 FR 43032,
July 26, 2005)), using the applicable service bulletin specified in
paragraph (q)(1)(i), (q)(1)(ii), or (q)(1)(iii) of this AD, which are
not incorporated by reference in this AD.
(i) Bombardier Service Bulletin 601-0546, dated May 31, 2002 (for Model
CL-600-2A12 (CL-601) airplanes and Model CL-600-2B16 (CL-601-3A and
CL-601-3R Variants) airplanes).
(ii) Bombardier Service Bulletin 600-0710, dated May 31, 2002 (for Model
CL-600-1A11 (CL-600) airplanes).
(iii) Bombardier Service Bulletin 604-32-014, dated May 31, 2002 (for
Model CL-600-2B16 (CL-604 Variant) airplanes).
(2) This paragraph provides credit for the addition of serial numbers and
part numbers required by paragraph (l) of this AD, if those actions
were performed before the effective date of this AD using the
applicable service bulletin specified in paragraph (q)(2)(i),
(q)(2)(ii), or (q)(2)(iii) of this AD, which are not incorporated by
reference in this AD.
(i) Bombardier Service Bulletin 604-32-014, Revision 01, dated October 29,
2007 (for Bombardier Model CL-600-2B16 (CL-604 Variant) airplanes).
(ii) Bombardier Service Bulletin 601-0546, Revision 02, dated October 29,
2007 (for Model CL-600-2A12 (CL-601) airplanes and Model CL-600-2B16
(CL-601-3A and CL-601-3R Variants) airplanes).
(iii) Bombardier Service Bulletin 600-0710, Revision 02, dated October 29,
2007 (for Bombardier Model CL-600-1A11 (CL-600) airplanes).
(3) This paragraph provides credit for the establishment of the CSN re-
quired by paragraph (m) of this AD, if those actions were performed
before the effective date of this AD using the applicable service
bulletin information sheet specified in paragraph (q)(3)(i),
(q)(3)(ii), or (q)(3)(iii) of this AD.
(i) Service Bulletin Information Sheet, dated July 6, 2010, of Bombardier
Service Bulletin 604-32-014, Revision 01, dated October 29, 2007 (for
Bombardier Model CL-600-2B16 (CL-604 Variant) airplanes).
(ii) Service Bulletin Information Sheet, dated July 6, 2010, of Bombardier
Service Bulletin 601-0546, Revision 02, dated October 29, 2007 (for
Bombardier Model CL-600-2A12 (CL-601) and Model CL-600-2B16 (CL-601
-3A and CL-601-3R Variants) airplanes).
(iii) Service Bulletin Information Sheet dated July 6, 2010, of Bombardier
Service Bulletin 600-0710, Revision 02, dated October 29, 2007 (for
Bombardier Model CL-600-1A11 (CL-600) airplanes).
(r) OTHER FAA AD PROVISIONS
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager, New York
Aircraft Certification Office (ACO), ANE-170, FAA, has the authority
to approve AMOCs for this AD, if requested using the procedures found
in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to
your principal inspector or local Flight Standards District Office, as
appropriate. If sending information directly to the ACO, send it to
ATTN: Program Manager, Continuing Operational Safety, FAA, New York
ACO, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone
516-228-7300; fax 516-794-5531. Before using any approved AMOC, notify
your appropriate principal inspector, or lacking a principal
inspector, the manager of the local flight standards district
office/certificate holding district office. The AMOC approval letter
must specifically reference this AD. AMOCs approved previously in
accordance with AD 2005-15-04, Amendment 39-14193 (70 FR 43032, July
26, 2005), are approved as AMOCs for the corresponding provisions of
this AD.
(2) Contacting the Manufacturer: For any requirement in this AD to obtain
corrective actions from a manufacturer, the action must be
accomplished using a method approved by the Manager, New York ACO,
ANE-170, Engine and Propeller Directorate, FAA; or Transport Canada
Civil Aviation (TCCA); or Bombardier, Inc.'s TCCA Design Approval
Organization (DAO). If approved by the DAO, the approval must include
the DAO-authorized signature.
(s) RELATED INFORMATION
(1) Refer to Mandatory Continuing Airworthiness Information (MCAI)
Canadian Airworthiness Directives specified in paragraphs (s)(1)(i),
(s)(1)(ii), and (s)(1)(iii) of this AD for related information. You
may examine the MCAI in the AD docket on the Internet at
http://www.regulations.gov/#!documentDetail;D=FAA-2013-1065-0002.
(i) Canadian Airworthiness Directive CF-2003-18R2, dated September 28,
2011.
(ii) Canadian Airworthiness Directive CF-2003-20R1, dated September 28,
2011.
(iii) Canadian Airworthiness Directive CF-2003-21R2, dated September 28,
2011.
(2) Service information identified in this AD that is not incorporated by
reference in this AD may be obtained at the addresses specified in
paragraphs (t)(5) and (t)(6) of this AD.
(t) MATERIAL INCORPORATED BY REFERENCE
(1) The Director of the Federal Register approved the incorporation by
reference (IBR) of the service information listed in this paragraph
under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do the actions
required by this AD, unless this AD specifies otherwise.
(3) The following service information was approved for IBR on September
25, 2014.
(i) Bombardier Service Bulletin 600-0710, Revision 03, dated May 9, 2011,
including Appendix 1, dated May 9, 2011, and Service Bulletin
Information Sheet, dated July 6, 2010.
(ii) Bombardier Service Bulletin 601-0546, Revision 03, dated May 9, 2011,
including Appendix 1, dated May 9, 2011, and Service Bulletin
Information Sheet, dated July 6, 2010.
(iii) Bombardier Service Bulletin 604-32-014, Revision 02, dated May 9,
2011, including Appendix 1, dated May 9, 2011, and Service Bulletin
Information Sheet, dated July 6, 2010.
(4) The following service information was approved for IBR on August 30,
2005 (70 FR 43032, July 26, 2005).
(i) Bombardier Service Bulletin 600-0710, Revision 01, dated December 15,
2003.
(ii) Bombardier Service Bulletin 601-0546, Revision 01, dated December 15,
2003.
(iii) Bombardier Service Bulletin 604-32-014, dated May 31, 2002.
(iv) Canadair Temporary Revision 5-116, dated April 11, 2002.
(v) Canadair Temporary Revision 5-190, dated April 11, 2002.
(vi) Canadair Temporary Revision 5-191, dated April 11, 2002.
(vii) Canadair Temporary Revision 5-192, dated April 11, 2002.
(viii) Canadair Temporary Revision 5-2-6, dated April 11, 2002.
(ix) Canadair Temporary Revision 5-204, dated April 11, 2002.
(x) Canadair Temporary Revision 5-205, dated April 11, 2002.
(xi) Canadair Temporary Revision 5-206, dated April 11, 2002.
(xii) Messier-Dowty Service Bulletin M-DT SB104467009/010-32-1 dated March
19, 2001.
(xiii) Messier-Dowty Service Bulletin M-DT SB19090-32-4, dated March 19,
2001.
(xiv) Messier-Dowty Service Bulletin M-DT SB20020-32-5, dated July 12,
2001.
(xv) Messier-Dowty Service Bulletin M-DT SB200814001-32-3, dated March 19,
2001.
(xvi) Messier-Dowty Service Bulletin M-DT SB200922001/2-32-6, dated March
19, 2001.
(xvii) Messier-Dowty Service Bulletin M-DT SB200924003/004-32-16, dated
July 12, 2001.
(xviii) Messier-Dowty Service Bulletin M-DT SB6100-32-10, dated March 19,
2001.
(xix) Messier-Dowty Service Bulletin M-DT SB6500-32-1, dated March 19,
2001.
(xx) Messier-Dowty Service Bulletin M-DT SB7200-32-6 dated March 19, 2001.
(xxi) Messier-Dowty Service Bulletin M-DT SB7300-32-16, dated July 12,
2001.
(5) For Bombardier, Inc./Canadair service information identified in this
AD, contact Bombardier, Inc., 400 Cote-Vertu Road West, Dorval, Quebec
H4S 1Y9, Canada; telephone 514-855-5000; fax 514-855-7401; email thd.
crj@aero.bombardier.com; Internet http://www.bombardier.com. For
Messier-Dowty service information identified in this AD, contact
Messier Services Americas, Customer Support Center, 45360 Severn Way,
Sterling, VA 20166-8910.
(6) You may view this service information at the FAA, Transport Airplane
Directorate, 1601 Lind Avenue SW., Renton, WA. For information on the
availability of this material at the FAA, call 425-227-1221.
(7) You may view this service information that is incorporated by
reference at the National Archives and Records Administration (NARA).
For information on the availability of this material at NARA, call
202-741-6030, or go to: http://www.archives.gov/federal-register/cfr/
ibr-locations.html.
Issued in Renton, Washington, on July 17, 2014. John P. Piccola, Acting
Manager, Transport Airplane Directorate, Aircraft Certification Service.
FOR FURTHER INFORMATION CONTACT: Andreas Rambalakos, Aerospace Engineer,
Airframe and Mechanical Systems Branch, ANE-171, FAA, New York Aircraft
Certification Office, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
telephone (516) 228-7345; fax (516) 794-5531.