Federal Register, Volume 78 Issue 23 (Monday, February 4, 2013)

[Federal Register Volume 78, Number 23 (Monday, February 4, 2013)]
[Rules and Regulations]
[Pages 7647-7650]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2013-01821]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2012-0639; Directorate Identifier 2012-NM-005-AD;
Amendment 39-17329; AD 2013-02-08]
RIN 2120-AA64

Airworthiness Directives; Bombardier, Inc. Airplanes

AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).

ACTION: Final rule.

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SUMMARY: We are adopting a new airworthiness directive (AD) for all
Bombardier, Inc. Model CL-600-2B19 (Regional Jet Series 100 & 440)
airplanes. This AD was prompted by a report that the safe life limit
and inspection requirements for the horizontal stabilizer trim actuator
(HSTA) attachment pins and trunnions were not listed in the
Airworthiness Limitations Section of the maintenance program. This AD
requires inspecting the trunnions and upper and lower pins for gouges,
scratches, and corrosion, and replacing the trunnions if necessary; and
adding serial numbers and new part numbers to certain trunnions, and
upper and lower pins. This AD also requires revising the maintenance
program to incorporate the information specified in certain temporary
revisions of the limitations section. We are issuing this AD to detect
and correct cracking, gouges, scratches, and corrosion of the HSTA
attachment pins and trunnions, which could result in failure of these
pins and trunnions and consequent disconnection of the horizontal
stabilizer and subsequent loss of controllability of the airplane.

DATES: This AD becomes effective March 11, 2013.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of March 11,
2013.

ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov or in person at the U.S. Department of
Transportation, Docket Operations, M-30, West Building Ground Floor,
Room W12-140, 1200 New Jersey Avenue SE., Washington, DC.

FOR FURTHER INFORMATION CONTACT: Cesar Gomez, Aerospace Engineer,
Airframe and Mechanical Systems Branch, ANE-171, FAA, New York Aircraft
Certification Office, 1600 Stewart Avenue, Suite 410, Westbury, New
York 11590; telephone (516) 228-7318; fax (516) 794-5531.

SUPPLEMENTARY INFORMATION:

Discussion

We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 to include an AD that would apply to the specified products.
That NPRM was published in the Federal Register on June 20, 2012 (77 FR
36948). That NPRM proposed to correct an unsafe condition for the
specified products. The Mandatory Continuing Airworthiness Information
(MCAI) states:

During a review of the Horizontal Stabilizer Trim Actuator
(HSTA) system, it was discovered that the safe life limits and the
inspection requirements for the HSTA attachment pins and trunnions
were not listed in the Airworthiness Limitations Section of the
Instructions for Continued Airworthiness. Also, the HSTA attachment
pins and trunnions were not serialized making it impossible to keep
accurate records of the life of these parts. Failure of these pins
and trunnions will lead to a disconnect of the horizontal stabilizer
and subsequent loss of the aeroplane.

[[Page 7648]]

This [Canadian] Airworthiness Directive (AD) mandates the
serialization of the HSTA attachment pins and trunnions.

The required actions include a detailed inspection of the trunnions and
upper and lower pins for gouges, scratches, and corrosion, and
replacing if necessary; and adding serial numbers and new part numbers
to certain trunnions, and upper and lower pins. The required actions
also include revising the maintenance program to incorporate the
information specified in certain temporary revisions of the limitations
section. You may obtain further information by examining the MCAI in
the AD docket.

Comments

We gave the public the opportunity to participate in developing
this AD. We considered the comments received.

Request To Allow Alternative Method of Identifying Parts

Air Wisconsin Airlines Corporation (Air Wisconsin) requested that
we allow the use of indelible ink and clear coat to mark the identified
HSTA. The commenter stated that the tolerances identified in Bombardier
Service Bulletin 601R-27-160, dated September 29, 2011, are too strict
to hand vibro-peen these individual parts. The commenter also noted
that Bombardier, Inc. is working on a revision to that service bulletin
to authorize marking all of these parts with indelible ink and clear
coat.
We agree that an alternative method of marking the HSTA would be
beneficial to operators. Since the issuance of the NPRM (77 FR 36948,
June 20, 2012), Bombardier, Inc. has issued Service Bulletin 601R-27-
160, Revision A, dated October 3, 2012, which describes an alternative
method for marking the HSTA. We have revised paragraphs (g), (h), (i),
and (n) of this AD to reference Bombardier Service Bulletin 601R-27-
160, Revision A, dated October 3, 2012. We have also added a new
paragraph (j) to this AD to allow credit for actions done before the
effective date of this AD in accordance with Bombardier Service
Bulletin 601R-27-160, dated September 29, 2011. We have re-identified
the subsequent paragraphs accordingly.

Request To Clarify the Term ``Horizontal Stabilizer Trim Actuator
(HSTA) Trunnion Support''

Air Wisconsin requested that we clarify what is meant by ``HSTA
trunnion support,'' as referenced in paragraph (j) of the NPRM (77 FR
36948, June 20, 2012) and Bombardier Temporary Revision 2B-2180, dated
August 8, 2011, to Appendix B--Airworthiness Limitations, of Part 2,
Airworthiness Requirements, of the Bombardier CL-600-2B19 Maintenance
Requirements Manual.
We agree to clarify the definition of HSTA trunnion support. The
HSTA trunnion support includes the upper and lower attachments of the
HSTA to the airframe mounting structure. No change has been made to the
AD in this regard.

Request To Make Documents Available to Public

Air Wisconsin requested that the documents ``Aerospace Standard
478'' and ``ATA Report 51-93-01 `Structural Maintenance Program
Guidelines for Continuing Airworthiness' '' be made available to the
public. The commenter stated that these documents are referenced in
Bombardier Service Bulletin 601R-27-160, dated September 29, 2011.
We disagree with the request to make these documents available to
the public. At the final rule stage, we post on www.regulations.gov
only the service information that is approved for incorporation by
reference in the final rule by the Office of the Federal Register.
Since Aerospace Standard 478 is not a document that is incorporated by
reference, we do not make it available on that Web site. However, if
the document is not currently in an operator's possession, it can be
obtained from the airplane manufacturer at the address specified in
paragraph (n)(2) of this AD. We have added an option to paragraph (i)
of this AD to allow operators to do the actions using a method approved
by the FAA. ATA Report 51-93-01 ``Structural Maintenance Program
Guidelines for Continuing Airworthiness'' is not necessary to
accomplish the AD actions. It is not necessary for compliance with the
AD, and is cited as reference material only.

Conclusion

We reviewed the available data, including the comments received,
and determined that air safety and the public interest require adopting
the AD with the changes described previously and minor editorial
changes. We have determined that these changes:
Are consistent with the intent that was proposed in the
NPRM (77 FR 36948, June 20, 2012) for correcting the unsafe condition;
and
Do not add any additional burden upon the public than was
already proposed in the NPRM (77 FR 36948, June 20, 2012).

Costs of Compliance

We estimate that this AD will affect 586 products of U.S. registry.
We also estimate that it will take about 20 work-hours per product to
comply with the basic requirements of this AD. The average labor rate
is $85 per work-hour. Required parts will cost about $162 per product.
Where the service information lists required parts costs that are
covered under warranty, we have assumed that there will be no charge
for these parts. As we do not control warranty coverage for affected
parties, some parties may incur costs higher than estimated here. Based
on these figures, we estimate the cost of this AD to the U.S. operators
to be $1,091,132, or $1,862 per product.
In addition, we estimate that any necessary follow-on actions would
take about 20 work-hours and require parts costing $4,391, for a cost
of $6,091 per product. We have no way of determining the number of
products that may need these actions.

Authority for This Rulemaking

Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. ``Subtitle VII: Aviation
Programs,'' describes in more detail the scope of the Agency's
authority.
We are issuing this rulemaking under the authority described in
``Subtitle VII, Part A, Subpart III, Section 44701: General
requirements.'' Under that section, Congress charges the FAA with
promoting safe flight of civil aircraft in air commerce by prescribing
regulations for practices, methods, and procedures the Administrator
finds necessary for safety in air commerce. This regulation is within
the scope of that authority because it addresses an unsafe condition
that is likely to exist or develop on products identified in this
rulemaking action.

Regulatory Findings

We determined that this AD will not have federalism implications
under Executive Order 13132. This AD will not have a substantial direct
effect on the States, on the relationship between the national
government and the States, or on the distribution of power and
responsibilities among the various levels of government.
For the reasons discussed above, I certify that this AD:
1. Is not a ``significant regulatory action'' under Executive Order
12866;
2. Is not a ``significant rule'' under the DOT Regulatory Policies
and Procedures (44 FR 11034, February 26, 1979);

[[Page 7649]]

3. Will not affect intrastate aviation in Alaska; and
4. Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
We prepared a regulatory evaluation of the estimated costs to
comply with this AD and placed it in the AD docket.

Examining the AD Docket

You may examine the AD docket on the Internet at http://www.regulations.gov; or in person at the Docket Operations office
between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The AD docket contains the NPRM (77 FR 36948, June 20, 2012),
the regulatory evaluation, any comments received, and other
information. The street address for the Docket Operations office
(telephone (800) 647-5527) is in the ADDRESSES section. Comments will
be available in the AD docket shortly after receipt.

List of Subjects in 14 CFR Part 39

Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.

Adoption of the Amendment

Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 14 CFR part 39 as follows:

PART 39--AIRWORTHINESS DIRECTIVES

0
1. The authority citation for part 39 continues to read as follows:

Authority: 49 U.S.C. 106(g), 40113, 44701.

Sec. 39.13 [Amended]

0
2. The FAA amends Sec. 39.13 by adding the following new AD:

2013-02-08 Bombardier, Inc.: Amendment 39-17329. Docket No. FAA-
2012-0639; Directorate Identifier 2012-NM-005-AD.

(a) Effective Date

This airworthiness directive (AD) becomes effective March 11,
2013.

(b) Affected ADs

None.

(1) This AD applies to Bombardier, Inc. Model CL-600-2B19
(Regional Jet Series 100 & 440) airplanes, certificated in any
category, all serial numbers.
(2) This AD requires revisions to certain operator maintenance
documents to include new actions (e.g., inspections) and/or Critical
Design Configuration Control Limitations (CDCCLs). Compliance with
these actions and/or CDCCLs 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 (m)(1) of this AD. The request should include a
description of changes to the required actions that will ensure the
continued operational safety of the airplane.

(d) Subject

Air Transport Association (ATA) of America Code 27: Flight
controls.

(e) Reason

This AD was prompted by a report that the safe life limit and
inspection requirements for the horizontal stabilizer trim actuator
(HSTA) attachment pins and trunnions were not listed in the
Airworthiness Limitations Section of the maintenance program. We are
issuing this AD to detect and correct cracking, gouges, scratches,
and corrosion of the HSTA attachment pins and trunnions, which could
result in failure of these pins and trunnions and consequent
disconnection of the horizontal stabilizer and subsequent loss of
controllability of the airplane.

(f) Compliance

You are responsible for having the actions required by this AD
performed within the compliance times specified, unless the actions
have already been done.

(g) Inspection

At the earliest of the times specified in paragraphs (g)(1),
(g)(2), and (g)(3) of this AD: Do a detailed inspection of the
trunnions, upper pins, and lower pins identified in table 1 to
paragraphs (g) and (h) of this AD, for gouges, scratches, and
corrosion, in accordance with the Accomplishment Instructions of
Bombardier Service Bulletin 601R-27-160, Revision A, dated October
3, 2012.
(1) Within 5,000 flight hours after the effective date of this
AD.
(2) Within 60 months after the effective date of this AD.
(3) Before the accumulation of 40,000 total flight cycles, or
within 60 days after the effective date of this AD, whichever occurs
later.

Table 1 to Paragraphs (g) and (h) of This AD--Affected Parts
------------------------------------------------------------------------
Part name Part No.
------------------------------------------------------------------------
Upper Pin............................................... 600-92384-5
Upper Pin............................................... 600-92384-7
Upper Pin............................................... 601R92310-1
Lower Pin............................................... 600-92383-5
Lower Pin............................................... 600-92383-7
Lower Pin............................................... 601R92309-1
Trunnion................................................ 601R92386-1
------------------------------------------------------------------------

(h) Replacement

If, during any inspection required by paragraph (g) of this AD,
any gouges, scratches, or corrosion are found: Before further
flight, replace the affected part with a part other than one
identified in table 1 to paragraphs (g) and (h) of this AD, in
accordance with the Accomplishment Instructions of Bombardier
Service Bulletin 601R-27-160, Revision A, dated October 3, 2012.

(i) Re-Identification

If, during any inspection required by paragraph (g) of this AD,
no gouges, scratches or corrosion are found: Before further flight,
add serial numbers and new part numbers to the trunnions, upper
pins, and lower pins, in accordance with the Accomplishment
Instructions of Bombardier Service Bulletin 601R-27-160, Revision A,
dated October 3, 2012; or using a method approved by the Manager,
International Branch, ANM-116, Transport Airplane Directorate, FAA.

(j) Credit for Previous Actions

This paragraph provides credit for the actions specified in
paragraphs (g), (h), and (i) of this AD, if those actions were
performed before the effective date of this AD using Bombardier
Service Bulletin 601R-27-160, dated September 29, 2011 (which is not
incorporated by reference by this AD).

(k) Revise Maintenance Program

Within 30 days after the effective date of this AD, revise the
maintenance program to incorporate the information specified in
Bombardier Temporary Revisions 2B-2180, dated August 8, 2011; and
2B-2186, dated August 8, 2011; to Appendix B--Airworthiness
Limitations, of Part 2, Airworthiness Requirements, of the
Bombardier CL-600-2B19 Maintenance Requirements Manual (MRM). The
compliance time for doing the initial replacement for the HSTA
trunnion support and attaching hardware is before the accumulation
of 80,000 landings or within 60 days after the effective date of
this AD, whichever occurs later. The compliance time for doing the
initial inspection of the upper and lower installation pins of the
horizontal stabilizer pitch trim actuator is before the accumulation
of 40,000 landings or within 60 days after the effective date of
this AD, whichever occurs later.

(l) No Alternative Actions or Intervals

After accomplishing the revision required by paragraph (k) of
this AD, no alternative actions (e.g., inspections) or intervals may
be used unless the actions or intervals are approved as an
alternative method of compliance (AMOC) in accordance with the
procedures specified in paragraph (m)(1) of this AD.

(m) 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, 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,

[[Page 7650]]

Suite 410, Westbury, New York 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.
(2) Airworthy Product: For any requirement in this AD to obtain
corrective actions from a manufacturer or other source, use these
actions if they are FAA-approved. Corrective actions are considered
FAA-approved if they are approved by the State of Design Authority
(or their delegated agent). You are required to assure the product
is airworthy before it is returned to service.

(n) Related Information

(1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) Canadian Airworthiness Directive CF-2011-45, dated December
19, 2011, and the service information specified in paragraphs
(n)(1)(i), (n)(1)(ii), and (n)(1)(iii) of this AD, for related
information.
(i) Bombardier Service Bulletin 601R-27-160, Revision A, dated
October 3, 2012.
(ii) Bombardier Temporary Revision 2B-2180, dated August 8,
2011, to Appendix B--Airworthiness Limitations, of Part 2,
Airworthiness Requirements, of the Bombardier CL-600-2B19
Maintenance Requirements Manual.
(iii) Bombardier Temporary Revision 2B-2186, dated August 8,
2011, to Appendix B--Airworthiness Limitations, of Part 2,
Airworthiness Requirements, of the Bombardier CL-600-2B19
Maintenance Requirements Manual.
(2) For service information identified in this AD, contact
Bombardier, Inc., 400 C[ocirc]te-Vertu Road West, Dorval,
Qu[eacute]bec H4S 1Y9, Canada; telephone 514-855-5000; fax 514-855-
7401; email thd.crj@aero.bombardier.com; Internet http://www.bombardier.com. You may review copies of the referenced service
information at the FAA, Transport Airplane Directorate, 1601 Lind
Avenue SW., Renton, Washington. For information on the availability
of this material at the FAA, call 425-227-1221.

(o) 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 the AD specifies otherwise.
(i) Bombardier Service Bulletin 601R-27-160, Revision A, dated
October 3, 2012.
(ii) Bombardier Temporary Revision 2B-2180, dated August 8,
2011, to Appendix B--Airworthiness Limitations, of Part 2,
Airworthiness Requirements, of the Bombardier CL-600-2B19
Maintenance Requirements Manual.
(iii) Bombardier Temporary Revision 2B-2186, dated August 8,
2011, to Appendix B--Airworthiness Limitations, of Part 2,
Airworthiness Requirements, of the Bombardier CL-600-2B19
Maintenance Requirements Manual.
(3) For service information identified in this AD, contact
Bombardier, Inc., 400 C[ocirc]te-Vertu Road West, Dorval,
Qu[eacute]bec H4S 1Y9, Canada; telephone 514-855-5000; fax 514-855-
7401; email thd.crj@aero.bombardier.com; Internet http://www.bombardier.com.
(4) You may review copies of the service information at the FAA,
Transport Airplane Directorate, 1601 Lind Avenue SW., Renton,
Washington. For information on the availability of this material at
the FAA, call 425-227-1221.
(5) 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 January 16, 2013.
Michael Kaszycki,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2013-01821 Filed 2-1-13; 8:45 am]
BILLING CODE 4910-13-P