Airworthiness Directives; B-N Group Ltd. BN-2, BN-2A, BN-2B, BN-2T, and BN-2T-4R Series (All Individual Models Included in Type Certificate Data Sheet (TCDS) A17EU, Revision 16, Dated December 9, 2002) Airplanes, 32492-32494 [E6-8713]
Download as PDF
32492
Federal Register / Vol. 71, No. 108 / Tuesday, June 6, 2006 / Proposed Rules
The Withdrawal
Accordingly, the notice of proposed
rulemaking, Docket 2001–NM–110–AD,
published in the Federal Register on
August 17, 2001 (66 FR 43128), is
withdrawn.
Issued in Renton, Washington, on May 26,
2006.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. E6–8710 Filed 6–5–06; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
SUPPLEMENTARY INFORMATION:
Federal Aviation Administration
Streamlined Issuance of AD
14 CFR Part 39
[Docket No. FAA–2005–22420; Directorate
Identifier 2005–CE–47–AD]
RIN 2120–AA64
Airworthiness Directives; B–N Group
Ltd. BN–2, BN–2A, BN–2B, BN–2T, and
BN–2T–4R Series (All Individual
Models Included in Type Certificate
Data Sheet (TCDS) A17EU, Revision
16, Dated December 9, 2002) Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Notice of proposed rulemaking
(NPRM).
AGENCY:
We propose to adopt a new
airworthiness directive (AD) for the
products listed above. This proposed
AD results from mandatory continuing
airworthiness information (MCAI)
issued by an airworthiness authority of
another country. The proposed AD
would require actions that are intended
to address an unsafe condition
described in the MCAI.
DATES: We must receive comments on
this proposed AD by June 21, 2006.
ADDRESSES: Use one of the following
addresses to comment on this proposed
AD:
• DOT Docket Web site: Go to
https://dms.dot.gov and follow the
instructions for sending your comments
electronically.
• Government-wide rulemaking Web
site: Go to https://www.regulations.gov
and follow the instructions for sending
your comments electronically.
• Mail: Docket Management Facility;
U.S. Department of Transportation, 400
Seventh Street, SW., Nassif Building,
Room PL–401, Washington, DC 20590.
• Fax: (202) 493–2251.
• Hand delivery: Room PL–401 on the
plaza level of the Nassif Building, 400
rwilkins on PROD1PC63 with PROPOSAL
SUMMARY:
VerDate Aug<31>2005
16:48 Jun 05, 2006
Seventh Street, SW., Washington, DC,
between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
For service information identified in
the proposed AD, contact the B–N
Group Ltd, Bembridge Airport, Isle of
Wright, United Kingdom, PO35 5PR;
telephone: 0870 881 5064; facsimile:
0870 881 5065; e-mail:
structural@britten-norman.com.
FOR FURTHER INFORMATION CONTACT:
Taylor Martin, Aerospace Safety
Engineer, FAA, Small Airplane
Directorate, 901 Locust, Room 301,
Kansas City, Missouri 64106; telephone:
(816) 329–4138; facsimile: (816) 329–
4090.
Jkt 208001
The FAA is implementing a new
process for streamlining the issuance of
ADs related to MCAI. We are
prototyping this process and specifically
request your comments on its use. This
streamlined process will allow us to
adopt MCAI safety requirements in a
more efficient manner and will reduce
safety risks to the public.
This process continues to follow all
existing AD issuance processes to meet
legal, economic, Administrative
Procedure Act, and Federal Register
requirements. We also continue to
follow our technical decision-making
processes in all aspects to meet our
responsibilities to determine and correct
unsafe conditions on U.S.-certificated
products.
This proposed AD references the
MCAI and related service information
that we considered in forming the
engineering basis to correct the unsafe
condition. The proposed AD contains
text copied from the MCAI and for this
reason might not follow our plain
language principles.
The comment period for this
proposed AD is open for 15 days. The
comment period is reduced because the
airworthiness authority and
manufacturer have already published
the documents on which we based our
decision, making a longer comment
period unnecessary.
Comments Invited
We invite you to send any written
data, views, or arguments regarding this
proposed AD. Send your comments to
an address listed under the ADDRESSES
section. Include the docket number,
Docket No. FAA–2005–22420;
Directorate Identifier 2005–CE–47–AD
at the beginning of your comments. We
specifically invite comments on the
overall regulatory, economic,
environmental, and energy aspects of
PO 00000
Frm 00014
Fmt 4702
Sfmt 4702
the proposed AD. We are also inviting
comments, views, or arguments on the
new MCAI process. We will consider all
comments received by the closing date
and may amend the proposed AD in
light of those comments.
We will post all comments we
receive, without change, to https://
dms.dot.gov, including any personal
information you provide. We will also
post a report summarizing each
substantive verbal contact we receive
concerning this proposed AD.
Discussion
The Civil Aviation Authority (CAA),
which is the airworthiness authority for
the United Kingdom, has issued British
Airworthiness Directive No. G–2004–
0011, dated May 25, 2004 (referred to
after this as ‘‘the MCAI’’), to correct an
unsafe condition for the specified
products. The MCAI states that that the
aircraft manufacturer has identified
several cases of corroded elevator final
drive control rods. If not corrected
corrosion of the interior surface could
result in failure or collapse of the rod,
resulting in loss of control or jamming
of the elevator system. The MCAI
requires an inspection of the internal
surface of the elevator system final drive
control rod and replacement if found
corroded. You may obtain further
information by examining the MCAI in
the docket.
Relevant Service Information
BN-Group Ltd. has issued BrittenNorman Service Bulletin SB number
303, Issue 1, dated May 14, 2004. The
actions described in this service
information are intended to correct the
unsafe condition identified in the
MCAI.
FAA’s Determination and Requirements
of the Proposed AD
This product is manufactured outside
the United States and is type certificated
for operation in the United States under
the provisions of section 21.29 of the
Federal Aviation Regulations (14 CFR
21.29) and the applicable bilateral
agreement. Pursuant to this bilateral
airworthiness agreement, the State of
Design’s airworthiness authority has
notified us of the unsafe condition
described in the MCAI and service
information referenced above. We have
examined the airworthiness authority’s
findings, evaluated all pertinent
information, and determined an unsafe
condition exists and is likely to exist or
develop on all products of this type
design. We are issuing this proposed AD
to correct the unsafe condition.
E:\FR\FM\06JNP1.SGM
06JNP1
Federal Register / Vol. 71, No. 108 / Tuesday, June 6, 2006 / Proposed Rules
Differences Between the Proposed AD
and the MCAI or Service Information
We have reviewed the MCAI and
related service information and, in
general, agree with their substance. But
we might have found it necessary to use
different words from those in the MCAI
to ensure the AD is clear for U.S.
operators and is enforceable in a U.S.
court of law. In making these changes,
we do not intend to differ substantively
from the information provided in the
MCAI and related service information.
We might also have proposed
different actions in this AD from those
in the MCAI in order to follow FAA
policies. Any such differences are
described in a separate paragraph of the
proposed AD. These proposed
requirements, if ultimately adopted, will
take precedence over the actions copied
from the MCAI.
Costs of Compliance
Based on the service information, we
estimate that this proposed AD would
affect about 91 products of U.S. registry.
We also estimate that it would take
about 5 workhours per product to do the
action and that the average labor rate is
$80 per workhour. Required parts
would cost about $1,000 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 costs.
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 the proposed AD on U.S.
operators to be $127,400, or $1,400 per
product.
rwilkins on PROD1PC63 with PROPOSAL
Authority for This Rulemaking
Title 49 of the United States Code
specifies 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 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.
VerDate Aug<31>2005
16:48 Jun 05, 2006
Jkt 208001
Regulatory Findings
We have determined that this
proposed AD would not have federalism
implications under Executive Order
13132. This proposed AD would 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 the proposed regulation:
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); and
3. 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 proposed AD and placed it in the
AD docket.
Examining the AD Docket
You may examine the AD docket that
contains the proposed AD, the
regulatory evaluation, any comments
received, and other information on the
Internet at https://dms.dot.gov; or in
person at the Docket Management
Facility between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal
holidays. The Docket Office (telephone
(800) 647–5227) is located at the street
address stated 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, Safety.
The Proposed Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the Federal Aviation Administration
proposes to amend 14 CFR part 39 as
follows:
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new AD:
B–N Group Ltd: Docket No. FAA–2005–
22420; Directorate Identifier 2005–CE–
47–AD.
PO 00000
Frm 00015
Fmt 4702
Sfmt 4702
32493
Comments Due Date
(a) We must receive comments on this
proposed airworthiness directive (AD) by
June 21, 2006.
Affected ADs
(b) None.
Applicability
(c) This AD applies to all BN–2, BN–2A,
BN–2B, BN–2T, and BN–2T–4R Series (all
individual models included in Type
Certificate Data Sheet (TCDS) A17EU,
Revision 16, dated December 9, 2002)
airplanes; certificated in any U.S. category.
Reason
(d) The aircraft manufacturer has identified
several cases of corroded elevator final drive
control rods. If not corrected corrosion of the
interior surface could result in failure or
collapse of the rod, resulting in loss of
control or jamming of the elevator system.
The mandatory continuing airworthiness
information (MCAI) requires an inspection of
the internal surface of the elevator system
final drive control rod and replacement if
found corroded.
Actions and Compliance
(e) Unless already done, do the following
except as stated in paragraph (f) below.
(1) Within the next 50 hours time-inservice or one month after the effective date
of this AD, whichever occurs first, inspect
the internal surface of the elevator system
final drive control rod, in accordance with BN Group Ltd. Britten-Norman Service
Bulletin SB number 303, Issue 1, dated May
14, 2004.
(2) If corrosion is found, the elevator
control rod must be replaced before further
flight.
FAA AD Differences
(f) When complying with this AD, repeat
the actions in paragraphs (e)(1) and (e)(2) of
this AD at intervals not to exceed 12 months.
Other FAA AD Provisions
(g) The following provisions also apply to
this AD:
(1) Alternative Methods of Compliance
(AMOCs): The Manager, Standards Staff,
FAA, ATTN: Taylor Martin, Aerospace Safety
Engineer, FAA, Small Airplane Directorate,
901 Locust, Room 301, Kansas City, Missouri
64106; telephone: (816) 329–4138; fax: (816)
329–4090, has the authority to approve
AMOCs for this AD, if requested using the
procedures found in 14 CFR 39.19.
(2) Return to Airworthiness: When
complying with this AD, perform FAAapproved corrective actions before returning
the product to an airworthy condition.
(3) Reporting Requirements: For any
reporting requirement in this AD, under the
provisions of the Paperwork Reduction Act,
the Office of Management and Budget (OMB)
has approved the information collection
requirements and has assigned OMB Control
Number 2120–0056.
Related Information
(h) This AD is related to MCAI United
Kingdom Airworthiness Directive No: G–
2004–0011, Issued Date: May 25, 2004, which
E:\FR\FM\06JNP1.SGM
06JNP1
32494
Federal Register / Vol. 71, No. 108 / Tuesday, June 6, 2006 / Proposed Rules
references B-N Group Ltd. Britten-Norman
Service Bulletin SB number 303, Issue 1,
dated May 14, 2004, for information on
required actions.
Issued in Kansas City, Missouri, on May
30, 2006.
David R. Showers,
Acting Manager, Small Airplane Directorate,
Aircraft Certification Service.
[FR Doc. E6–8713 Filed 6–5–06; 8:45 am]
BILLING CODE 4910–13–P
SOCIAL SECURITY ADMINISTRATION
20 CFR Parts 401 and 402
RIN 0960–AG14
Privacy and Disclosure of Official
Records and Information
Social Security Administration.
Notice of Proposed Rulemaking.
AGENCY:
rwilkins on PROD1PC63 with PROPOSAL
ACTION:
SUMMARY: We propose to amend our
privacy and disclosure rules to help
preserve the anonymity of, and help
protect the physical well-being of, SSA
employees who reasonably believe that
they are at risk of injury or other harm
if certain employment information
about them is disclosed. These changes
in the regulations would ensure uniform
application of the policy for at-risk
employees.
DATES: To be sure that your comments
are considered, we must receive them
no later than August 7, 2006.
ADDRESSES: You may give us your
comments by: using our Internet facility
(i.e., Social Security Online) at https://
policy.ssa.gov/erm/rules.nsf/
Rules+Open+To+Comment or the
Federal eRulemaking Portal at https://
www.regulations.gov; e-mail to
regulations@ssa.gov; by telefax to (410)
966–2830, or letter to the Commissioner
of Social Security, P.O. Box 17703,
Baltimore, MD 21235–7703. You may
also deliver them to the Office of
Regulations, Social Security
Administration, 100 Altmeyer Building,
6401 Security Boulevard, Baltimore,
MD. 21235–6401, between 8 a.m. and
4:30 p.m. on regular business days.
Comments are posted on our Internet
site, or you may inspect them on regular
business days by making arrangements
with the contact person shown in this
preamble.
FOR FURTHER INFORMATION CONTACT: Edie
McCracken, Social Insurance Specialist,
Office of Public Disclosure, 3–A–6
Operations Building, 6401 Security
Boulevard, Baltimore, MD 21235–6401,
(410) 965–6117 or TTY (410) 965–5609.
For information on eligibility or filing
for benefits, call our national toll-free
VerDate Aug<31>2005
16:48 Jun 05, 2006
Jkt 208001
number, 1–800–772–1213 or TTY 1–
800–325–0778, or visit our Internet
Website, Social Security Online, at
https://www.socialsecurity.gov.
SUPPLEMENTARY INFORMATION:
Electronic Version
The electronic file of this document is
available on the date of publication in
the Federal Register at https://
www.gpoaccess.gov/fr/.
Background
Former Commissioner Kenneth S.
Apfel approved a recommendation of
the National Health and Safety
Partnership Committee for Security
(NHSPCS) to implement a nationwide
program to enhance the safety and
security of SSA employees who are
victims, or potential victims, of
domestic violence. The NHSPCS’
proposed program was developed,
during the era of ‘‘partnership’’, by a
joint union/management workgroup. It
was intended to safeguard the
anonymity of at-risk employees when
requests for their work location and/or
phone number were received, by
delaying the disclosure of the
information when certain conditions
were met. This would have entailed a
change in SSA policy that now permits
such information requests to be
honored. No action was ever taken on
the recommendation when the
‘‘partnership’’ was dissolved by
Executive Order 13203 on February 17,
2001. We are now proposing a modified
approach to strengthening our privacy
and disclosure rules to better safeguard
at-risk employees.
Explanation of Changes
We propose to amend subsection
(b)(3)(c)(4) of Appendix A to Part 401
and add a new subsection (e) to § 402.45
to permit SSA to exercise its discretion,
consistent with the Freedom of
Information Act and the rules of the
Office of Personnel Management (5 CFR
part 293), to withhold the work location
and telephone number of employees
who reasonably believe that they are at
risk of injury or other harm by the
disclosure of such information. These
proposed changes would clarify our
procedures for access to, and disclosure
of, personally identifiable information
regarding employees and enhance our
ability to maintain adequate safeguards
against disclosures in situations in
which an employee may be at risk or
fear for his/her physical safety.
We propose to amend Part 401,
Appendix A, (b)(3)(c)(4) by removing
the first sentence, ‘‘Location of duty
station, including room number and
telephone number.’’ We also propose to
PO 00000
Frm 00016
Fmt 4702
Sfmt 4702
revise § 402.45 by adding a new
subsection (e). New subsection
§ 402.45(e) will fully describe the rules
governing the release of personally
identifiable information as it pertains to
employees’ telephone numbers and duty
stations (including room numbers, bay
designations, or other identifying
information regarding buildings or
places of employment).
Clarity of These Proposed Rules
Executive Order 12866, as amended
by Executive Order 13258, requires each
agency to write all rules in plain
language. In addition to your
substantive comments on these
proposed rules, we invite your
comments on how to make these
proposed rules easier to understand. For
example:
• Have we organized the material to
suit your needs?
• Are the requirements in the rules
clearly stated?
• Do the rules contain technical
language or jargon that is not clear?
• Would a different format (grouping
and order of sections, use of headings,
paragraphing) make the rules easier to
understand?
• Would more (but shorter) sections
be better?
• Could we improve clarity by adding
tables, lists, or diagrams?
• What else could we do to make the
rules easier to understand?
Regulatory Procedures
Executive Order 12866
We have consulted with the Office of
Management and Budget (OMB) and
determined that these proposed rules
would meet the criteria for a significant
regulatory action under Executive Order
12866, as amended by Executive Order
13258. Thus, they were subject to OMB
review.
Regulatory Flexibility Act
We certify that these proposed rules
would not have a significant economic
impact on a substantial number of small
entities because they affect only
individuals or entities acting on their
behalf. Thus, a regulatory flexibility
analysis as provided in the Regulatory
Flexibility Act, as amended, is not
required.
Paperwork Reduction Act
These proposed rules impose no
reporting or record keeping
requirements subject to OMB clearance.
(Catalog of Federal Domestic Assistance
Program Nos. 96.001, Social SecurityDisability Insurance; 96.002, Social SecurityRetirement Insurance; 96.004, Social
E:\FR\FM\06JNP1.SGM
06JNP1
Agencies
[Federal Register Volume 71, Number 108 (Tuesday, June 6, 2006)]
[Proposed Rules]
[Pages 32492-32494]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E6-8713]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2005-22420; Directorate Identifier 2005-CE-47-AD]
RIN 2120-AA64
Airworthiness Directives; B-N Group Ltd. BN-2, BN-2A, BN-2B, BN-
2T, and BN-2T-4R Series (All Individual Models Included in Type
Certificate Data Sheet (TCDS) A17EU, Revision 16, Dated December 9,
2002) Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Notice of proposed rulemaking (NPRM).
-----------------------------------------------------------------------
SUMMARY: We propose to adopt a new airworthiness directive (AD) for the
products listed above. This proposed AD results from mandatory
continuing airworthiness information (MCAI) issued by an airworthiness
authority of another country. The proposed AD would require actions
that are intended to address an unsafe condition described in the MCAI.
DATES: We must receive comments on this proposed AD by June 21, 2006.
ADDRESSES: Use one of the following addresses to comment on this
proposed AD:
DOT Docket Web site: Go to https://dms.dot.gov and follow
the instructions for sending your comments electronically.
Government-wide rulemaking Web site: Go to https://
www.regulations.gov and follow the instructions for sending your
comments electronically.
Mail: Docket Management Facility; U.S. Department of
Transportation, 400 Seventh Street, SW., Nassif Building, Room PL-401,
Washington, DC 20590.
Fax: (202) 493-2251.
Hand delivery: Room PL-401 on the plaza level of the
Nassif Building, 400 Seventh Street, SW., Washington, DC, between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
For service information identified in the proposed AD, contact the
B-N Group Ltd, Bembridge Airport, Isle of Wright, United Kingdom, PO35
5PR; telephone: 0870 881 5064; facsimile: 0870 881 5065; e-mail:
structural@britten-norman.com.
FOR FURTHER INFORMATION CONTACT: Taylor Martin, Aerospace Safety
Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas
City, Missouri 64106; telephone: (816) 329-4138; facsimile: (816) 329-
4090.
SUPPLEMENTARY INFORMATION:
Streamlined Issuance of AD
The FAA is implementing a new process for streamlining the issuance
of ADs related to MCAI. We are prototyping this process and
specifically request your comments on its use. This streamlined process
will allow us to adopt MCAI safety requirements in a more efficient
manner and will reduce safety risks to the public.
This process continues to follow all existing AD issuance processes
to meet legal, economic, Administrative Procedure Act, and Federal
Register requirements. We also continue to follow our technical
decision-making processes in all aspects to meet our responsibilities
to determine and correct unsafe conditions on U.S.-certificated
products.
This proposed AD references the MCAI and related service
information that we considered in forming the engineering basis to
correct the unsafe condition. The proposed AD contains text copied from
the MCAI and for this reason might not follow our plain language
principles.
The comment period for this proposed AD is open for 15 days. The
comment period is reduced because the airworthiness authority and
manufacturer have already published the documents on which we based our
decision, making a longer comment period unnecessary.
Comments Invited
We invite you to send any written data, views, or arguments
regarding this proposed AD. Send your comments to an address listed
under the ADDRESSES section. Include the docket number, Docket No. FAA-
2005-22420; Directorate Identifier 2005-CE-47-AD at the beginning of
your comments. We specifically invite comments on the overall
regulatory, economic, environmental, and energy aspects of the proposed
AD. We are also inviting comments, views, or arguments on the new MCAI
process. We will consider all comments received by the closing date and
may amend the proposed AD in light of those comments.
We will post all comments we receive, without change, to https://
dms.dot.gov, including any personal information you provide. We will
also post a report summarizing each substantive verbal contact we
receive concerning this proposed AD.
Discussion
The Civil Aviation Authority (CAA), which is the airworthiness
authority for the United Kingdom, has issued British Airworthiness
Directive No. G-2004-0011, dated May 25, 2004 (referred to after this
as ``the MCAI''), to correct an unsafe condition for the specified
products. The MCAI states that that the aircraft manufacturer has
identified several cases of corroded elevator final drive control rods.
If not corrected corrosion of the interior surface could result in
failure or collapse of the rod, resulting in loss of control or jamming
of the elevator system. The MCAI requires an inspection of the internal
surface of the elevator system final drive control rod and replacement
if found corroded. You may obtain further information by examining the
MCAI in the docket.
Relevant Service Information
BN-Group Ltd. has issued Britten-Norman Service Bulletin SB number
303, Issue 1, dated May 14, 2004. The actions described in this service
information are intended to correct the unsafe condition identified in
the MCAI.
FAA's Determination and Requirements of the Proposed AD
This product is manufactured outside the United States and is type
certificated for operation in the United States under the provisions of
section 21.29 of the Federal Aviation Regulations (14 CFR 21.29) and
the applicable bilateral agreement. Pursuant to this bilateral
airworthiness agreement, the State of Design's airworthiness authority
has notified us of the unsafe condition described in the MCAI and
service information referenced above. We have examined the
airworthiness authority's findings, evaluated all pertinent
information, and determined an unsafe condition exists and is likely to
exist or develop on all products of this type design. We are issuing
this proposed AD to correct the unsafe condition.
[[Page 32493]]
Differences Between the Proposed AD and the MCAI or Service Information
We have reviewed the MCAI and related service information and, in
general, agree with their substance. But we might have found it
necessary to use different words from those in the MCAI to ensure the
AD is clear for U.S. operators and is enforceable in a U.S. court of
law. In making these changes, we do not intend to differ substantively
from the information provided in the MCAI and related service
information.
We might also have proposed different actions in this AD from those
in the MCAI in order to follow FAA policies. Any such differences are
described in a separate paragraph of the proposed AD. These proposed
requirements, if ultimately adopted, will take precedence over the
actions copied from the MCAI.
Costs of Compliance
Based on the service information, we estimate that this proposed AD
would affect about 91 products of U.S. registry. We also estimate that
it would take about 5 workhours per product to do the action and that
the average labor rate is $80 per workhour. Required parts would cost
about $1,000 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 costs. 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 the
proposed AD on U.S. operators to be $127,400, or $1,400 per product.
Authority for This Rulemaking
Title 49 of the United States Code specifies 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 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 have determined that this proposed AD would not have federalism
implications under Executive Order 13132. This proposed AD would 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 the proposed
regulation:
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); and
3. 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 proposed AD and placed it in the AD docket.
Examining the AD Docket
You may examine the AD docket that contains the proposed AD, the
regulatory evaluation, any comments received, and other information on
the Internet at https://dms.dot.gov; or in person at the Docket
Management Facility between 9 a.m. and 5 p.m., Monday through Friday,
except Federal holidays. The Docket Office (telephone (800) 647-5227)
is located at the street address stated 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, Safety.
The Proposed Amendment
Accordingly, under the authority delegated to me by the
Administrator, the Federal Aviation Administration proposes to amend 14
CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
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]
2. The FAA amends Sec. 39.13 by adding the following new AD:
B-N Group Ltd: Docket No. FAA-2005-22420; Directorate Identifier
2005-CE-47-AD.
Comments Due Date
(a) We must receive comments on this proposed airworthiness
directive (AD) by June 21, 2006.
Affected ADs
(b) None.
Applicability
(c) This AD applies to all BN-2, BN-2A, BN-2B, BN-2T, and BN-2T-
4R Series (all individual models included in Type Certificate Data
Sheet (TCDS) A17EU, Revision 16, dated December 9, 2002) airplanes;
certificated in any U.S. category.
Reason
(d) The aircraft manufacturer has identified several cases of
corroded elevator final drive control rods. If not corrected
corrosion of the interior surface could result in failure or
collapse of the rod, resulting in loss of control or jamming of the
elevator system. The mandatory continuing airworthiness information
(MCAI) requires an inspection of the internal surface of the
elevator system final drive control rod and replacement if found
corroded.
Actions and Compliance
(e) Unless already done, do the following except as stated in
paragraph (f) below.
(1) Within the next 50 hours time-in-service or one month after
the effective date of this AD, whichever occurs first, inspect the
internal surface of the elevator system final drive control rod, in
accordance with B-N Group Ltd. Britten-Norman Service Bulletin SB
number 303, Issue 1, dated May 14, 2004.
(2) If corrosion is found, the elevator control rod must be
replaced before further flight.
FAA AD Differences
(f) When complying with this AD, repeat the actions in
paragraphs (e)(1) and (e)(2) of this AD at intervals not to exceed
12 months.
Other FAA AD Provisions
(g) The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
Standards Staff, FAA, ATTN: Taylor Martin, Aerospace Safety
Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301,
Kansas City, Missouri 64106; telephone: (816) 329-4138; fax: (816)
329-4090, has the authority to approve AMOCs for this AD, if
requested using the procedures found in 14 CFR 39.19.
(2) Return to Airworthiness: When complying with this AD,
perform FAA-approved corrective actions before returning the product
to an airworthy condition.
(3) Reporting Requirements: For any reporting requirement in
this AD, under the provisions of the Paperwork Reduction Act, the
Office of Management and Budget (OMB) has approved the information
collection requirements and has assigned OMB Control Number 2120-
0056.
Related Information
(h) This AD is related to MCAI United Kingdom Airworthiness
Directive No: G-2004-0011, Issued Date: May 25, 2004, which
[[Page 32494]]
references B-N Group Ltd. Britten-Norman Service Bulletin SB number
303, Issue 1, dated May 14, 2004, for information on required
actions.
Issued in Kansas City, Missouri, on May 30, 2006.
David R. Showers,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E6-8713 Filed 6-5-06; 8:45 am]
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