Airworthiness Directives; EADS SOCATA Model TBM 700 Airplanes, 56414-56416 [06-8277]
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56414
Federal Register / Vol. 71, No. 187 / Wednesday, September 27, 2006 / Proposed Rules
110 Stat. 1321, 1321–349 (42 U.S.C. 2243);
sec. 1704, 112 Stat. 2750 (44 U.S.C. 3504
note).
[Docket No. FAA–2006–25637; Directorate
Identifier 2006–CE–43–AD]
mandatory continuing airworthiness
information (MCAI) issued by the
airworthiness authority for France. We
are proposing this AD to detect and
replace incorrect length pilot door
locking stop-fittings. This condition, if
not corrected, could result in
depressurization of the airplane.
DATES: We must receive comments on
this proposed AD by October 27, 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–
0001.
• 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
this proposed AD, contact EADS
SOCATA, Direction des Services, 65921
Tarbes Cedex 9, France; telephone: 33
(0)5 62 41 73 00; fax: 33 (0)5 62 41 76
54; or SOCATA AIRCRAFT, INC., North
Perry Airport, 7501 South Airport Rd.,
Pembroke Pines, FL 33023; telephone:
(954) 893–1400; fax: (954) 964–4141.
FOR FURTHER INFORMATION CONTACT:
Gunnar Berg, Aerospace Safety
Engineer, FAA, Small Airplane
Directorate, 901 Locust, Room 301,
Kansas City, Missouri 64106; telephone:
(816) 329–4141; fax: (816) 329–4090.
SUPPLEMENTARY INFORMATION:
RIN 2120–AA64
Comments Invited
Sections 70.1(c) and 70.20a(b) also issued
under secs. 135, 141, Pub. L. 97–425, 96 Stat.
2232, 2241 (42 U.S.C. 10155, 10161). Section
70.7 also issued under Pub. L. 95–601, sec.
10, 92 Stat. 2951 (42 U.S.C. 5851). Section
70.21(g) also issued under sec. 122, 68 Stat.
939 (42 U.S.C. 2152). Section 70.31 also
issued under sec. 57d, Pub. L. 93–377, 88
Stat. 475 (42 U.S.C. 2077). Sections 70.36 and
70.44 also issued under sec. 184, 68 Stat. 954,
as amended (42 U.S.C. 2234). Section 70.81
also issued under secs. 186, 187, 68 Stat. 955
(42 U.S.C. 2236, 2237). Section 70.82 also
issued under sec. 108, 68 Stat. 939, as
amended (42 U.S.C. 2138).
2. In § 70.72, paragraph (c)(2) is
revised to read as follows:
§ 70.72 Facility changes and change
process.
*
*
*
*
*
(c) * * *
(2) Does not remove, without at least
an equivalent replacement of the safety
function, an item relied on for safety
that is listed in the integrated safety
analysis summary and is necessary for
compliance with the performance
requirements of § 70.61;
*
*
*
*
*
Dated at Rockville, Maryland, this 13th day
of September, 2006.
For the Nuclear Regulatory Commission.
Luis A. Reyes,
Executive Director for Operations.
[FR Doc. 06–8271 Filed 9–26–06; 8:45 am]
BILLING CODE 7590–01–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
Airworthiness Directives; EADS
SOCATA Model TBM 700 Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Notice of proposed rulemaking
(NPRM).
rwilkins on PROD1PC63 with PROPOSAL
AGENCY:
SUMMARY: We propose to adopt a new
airworthiness directive (AD) for certain
EADS SOCATA Model TBM 700
airplanes. This proposed AD would
require you to inspect the pilot door
locking stop-fittings for correct length
and, if any incorrect length pilot door
locking stop-fittings are found, replace
them. This proposed AD results from
VerDate Aug<31>2005
16:43 Sep 26, 2006
Jkt 208001
We invite you to send any written
relevant data, views, or arguments
regarding this proposed AD. Send your
comments to an address listed under the
ADDRESSES section. Include the docket
number, ‘‘FAA–2006–25637; Directorate
Identifier 2006–CE–43–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 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
PO 00000
Frm 00002
Fmt 4702
Sfmt 4702
information you provide. We will also
post a report summarizing each
substantive verbal contact we receive
concerning this proposed AD.
Discussion
´ ´
The Direction generale de l’aviation
civile (DGAC), which is the aviation
authority for France, notified FAA that
an unsafe condition may exist on certain
EADS SOCATA Model TBM 700
airplanes. The DGAC reports that the
pilot door adjustment procedure was
improperly done, and the pilot door
locking stop-fittings may be of incorrect
length. This condition, if not corrected,
could result in depressurization of the
airplane.
Relevant Service Information
We have reviewed EADS SOCATA
Service Bulletin SB 70–131, ATA No.
53, dated July 2005.
The service information describes
procedures for:
• Inspecting the pilot door locking
stop-fittings for correct length and
• Replacing any incorrect length pilot
door locking stop-fittings.
Foreign Airworthiness Authority
Information
The DGAC classified this service
bulletin as mandatory and issued
French AD Number F–2005–134, dated
August 03, 2005, to ensure the
continued airworthiness of these
airplanes in France. These EADS
SOCATA Model TBM 700 airplanes are
manufactured in France and are typecertificated 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 airworthiness
agreement.
Under this bilateral airworthiness
agreement, the DGAC has kept us
informed of the situation described
above.
FAA’s Determination and Requirements
of the Proposed AD
We are proposing this AD because we
have examined the DGAC’s findings,
evaluated all information and
determined the unsafe condition
described previously is likely to exist or
develop on other products of the same
type design that are certificated for
operation in the United States.
This proposed AD would require you
to inspect the pilot door locking stopfittings for correct length and, if any
incorrect length pilot door locking stopfittings are found, replace them.
E:\FR\FM\27SEP1.SGM
27SEP1
56415
Federal Register / Vol. 71, No. 187 / Wednesday, September 27, 2006 / Proposed Rules
Differences Between This Proposed AD
and the Service Information
The service information allows for
unpressurized flight if any incorrect
length pilot door locking-stop fittings
are found. If parts have been ordered but
are not available, the proposed AD
would permit unpressurized flight for
90 days after the required inspection or
until parts become available, whichever
occurs first. In addition, a placard in
view of the pilot would be installed
prohibiting pressurized flight until the
repairs are done. The service
information does not have a compliance
time for the repairs or a placard
requirement if incorrect length pilot
door locking stop-fittings are found. The
requirements of this proposed AD, if
adopted as a final rule, would take
precedence over the provisions in the
service information.
Costs of Compliance
We estimate that this proposed AD
would affect 157 airplanes in the U.S.
registry.
We estimate the following costs to do
the proposed inspection and repair:
Labor cost
Parts cost
Total cost per
airplane
Total cost on
U.S. operators
4.5 work-hours × $80 per hour = $360 .......................................................................................
$15
$375
$58,875
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 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.
PART 39—AIRWORTHINESS
DIRECTIVES
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.
Comments Due Date
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new AD:
EADS SOCATA: Docket No. FAA–2006–
25637; Directorate Identifier 2006–CE–
43–AD.
(a) We must receive comments on this
airworthiness directive (AD) action by
October 27, 2006.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Model TBM 700
airplanes, serial numbers 126 through 322,
that are certificated in any category.
Unsafe Condition
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 FAA proposes to amend 14 CFR part
39 as follows:
(d) This AD results from a pilot door
adjustment procedure not being done
properly. We are issuing this AD to detect
and correct incorrect length pilot door
locking stop-fittings. This condition, if not
corrected, could result in depressurization of
the airplane.
Compliance
Actions
Within 30 days after the effective date of
this AD, unless already done
Before further flight after the inspection
by paragraph (e)(1) of this AD
(e) To address this problem, you must do
the following:
Compliance
(1) Inspect the pilot door locking stop-fittings for
correct length
(2) If any incorrect length pilot door locking stopfittings are found, replace them
rwilkins on PROD1PC63 with PROPOSAL
1. The authority citation for part 39
continues to read as follows:
(f) If you have ordered parts and they are
not available, then you may fly
unpressurized until parts become available or
for a period not to exceed 90 days after the
inspection required in paragraph (e)(1) of this
VerDate Aug<31>2005
16:43 Sep 26, 2006
Jkt 208001
Procedures
AD, whichever occurs first. You must also
fabricate and install a placard as described
below. Completing the action of paragraph
(e)(2) of this AD terminates the placard
requirement.
PO 00000
Frm 00003
Fmt 4702
Sfmt 4702
Follow
131,
Follow
131,
EADS SOCATA Service Bulletin SB 70–
ATA No. 53, dated July 2005.
EADS SOCATA Service Bulletin SB 70–
ATA No. 53, dated July 2005.
(1) Fabricate (using letters at least 1⁄8 inch
in height) a warning placard which states
‘‘This airplane is prohibited from pressurized
flight.’’
E:\FR\FM\27SEP1.SGM
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56416
Federal Register / Vol. 71, No. 187 / Wednesday, September 27, 2006 / Proposed Rules
(2) Install the placard in full view of the
pilot. The owner/operator holding at least a
private pilot certificate as authorized by
section 43.7 of the Federal Aviation
Regulations (14 CFR 43.7) may install the
placard as required in paragraph (f) of this
AD.
Alternative Methods of Compliance
(AMOCs)
(g) The Manager, Standards Office, Small
Airplane Directorate, FAA, ATTN: Gunnar
Berg, Aerospace Safety Engineer, FAA, Small
Airplane Directorate, 901 Locust, Room 301,
Kansas City, Missouri 64106; telephone:
(816) 329–4141; fax: (816) 329–4090, has the
authority to approve AMOCs for this AD, if
requested using the procedures found in 14
CFR 39.19.
Related Information
(h) This AD is related to French AD
Number F–2005–134, dated August 3, 2005.
To get copies of the service information
referenced in this AD, contact EADS
SOCATA, Direction des Services, 65921
Tarbes Cedex 9, France; telephone: 33 (0)5 62
41 73 00; fax: 33 (0)5 62 41 76 54; or
SOCATA AIRCRAFT, INC., North Perry
Airport, 7501 South Airport Rd., Pembroke
Pines, FL 33023; telephone: (954) 893–1400;
fax: (954) 964–4141. To view the AD docket,
go to the Docket Management Facility; U.S.
Department of Transportation, 400 Seventh
Street, SW., Nassif Building, Room PL–401,
Washington, DC, or on the Internet at https://
dms.dot.gov. The docket number is Docket
No. FAA–2006–25637; Directorate Identifier
2006–CE–43–AD.
another country to identify and correct
an unsafe condition on an aviation
product. The proposed AD would
require actions that are intended to
address the unsafe condition described
in the MCAI.
We must receive comments on
this proposed AD by October 27, 2006.
ADDRESSES: You may send comments by
any of the following methods:
• DOT Docket Web Site: Go to
https://dms.dot.gov and follow the
instructions for sending your comments
electronically.
• Fax: (202) 493–2251.
• Mail: Docket Management Facility,
U.S. Department of Transportation, 400
Seventh Street, SW., Nassif Building,
Room PL–401, Washington, DC 20590–
0001.
• 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.
• Federal eRulemaking Portal: https://
www.regulations.gov. Follow the
instructions for submitting comments.
DATES:
Examining the AD Docket
[Docket No. FAA–2006–25810; Directorate
Identifier 2006–CE–49–AD]
You may examine the AD docket 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 AD docket contains this
proposed AD, the regulatory evaluation,
any comments received, and other
information. The street address for the
Docket Office (telephone (800) 647–
5227) is in the ADDRESSES section.
Comments will be available in the AD
docket shortly after receipt.
FOR FURTHER INFORMATION CONTACT:
Gregory Davison, Glider Program
Manager, 901 Locust, Room 301, Kansas
City, Missouri, 64106; telephone: (816)
329–4130; fax: (816) 329–4090.
SUPPLEMENTARY INFORMATION:
RIN 2120–AA64
Streamlined Issuance of AD
Airworthiness Directives; PZL-Bielsko
Model SZD–50–3 ‘‘Puchacz’’ Gliders
The FAA is implementing a new
process for streamlining the issuance of
ADs related to MCAI. The 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 FAA AD issuance processes to
meet legal, economic, Administrative
Procedure Act, and Federal Register
requirements. We also continue to meet
our technical decision-making
responsibilities to identify and correct
unsafe conditions on U.S.-certificated
products.
Issued in Kansas City, Missouri, on
September 20, 2006.
David R. Showers,
Acting Manager, Small Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 06–8277 Filed 9–26–06; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Notice of proposed rulemaking
(NPRM).
rwilkins on PROD1PC63 with PROPOSAL
AGENCY:
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 aviation authority of
VerDate Aug<31>2005
16:43 Sep 26, 2006
Jkt 208001
PO 00000
Frm 00004
Fmt 4702
Sfmt 4702
Comments Invited
We invite you to send any written
relevant data, views, or arguments about
this proposed AD. Send your comments
to an address listed under the
ADDRESSES section. Include ‘‘Docket No.
FAA–2006–25810; Directorate Identifier
2006-CE–49-AD’’ at the beginning of
your comments. We specifically invite
comments on the overall regulatory,
economic, environmental, and energy
aspects of this proposed AD. We will
consider all comments received by the
closing date and may amend this
proposed AD because 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
about this proposed AD.
Discussion
The European Aviation Safety Agency
(EASA), which is the aviation authority
for the European Union (EU), has issued
Emergency Airworthiness Directive
EAD No: 2006–0243-E (referred to after
this as ‘‘the MCAI’’), to correct an unsafe
condition for the specified products.
The MCAI states that the aircraft
manufacturer has identified that a
discrepancy between the design
documentation and the Technical
Service Manual has been identified. In
1981, a castellated nut with cotter pin
was introduced to secure the rudder,
replacing the self locking nut, through
PZL Bielsko Bulletin No. BK 06/50 3/81.
This change has not been introduced to
the Technical Service Manual and use
of a self locking nut, in accordance with
the Manual, is still possible. This was
probably the reason of rudder
disconnection during flight which
occurred recently.
If not corrected, loss of the nut could
result and allow the rudder to slip out
of its hinges, separate from the glider,
and lead to loss of control.
The MCAI requires you to inspect
and, if necessary, replace the Rudder
Attachment parts in accordance with
the instruction contained in the Allstar
PZL Glider Sp. z o.o. Mandatory
Bulletin No. BE 058/SZD 50 3/2006
‘‘PUCHACZ’’, dated August 10, 2006.
Concurrently, changes in the Technical
Service Manual must be introduced in
accordance with the referenced bulletin.
You may obtain further information by
examining the MCAI in the AD docket.
Relevant Service Information
PZL-Bielsko has issued Allstar PZL
Glider Sp. z o.o. Mandatory Bulletin No.
E:\FR\FM\27SEP1.SGM
27SEP1
Agencies
[Federal Register Volume 71, Number 187 (Wednesday, September 27, 2006)]
[Proposed Rules]
[Pages 56414-56416]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 06-8277]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2006-25637; Directorate Identifier 2006-CE-43-AD]
RIN 2120-AA64
Airworthiness Directives; EADS SOCATA Model TBM 700 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
certain EADS SOCATA Model TBM 700 airplanes. This proposed AD would
require you to inspect the pilot door locking stop-fittings for correct
length and, if any incorrect length pilot door locking stop-fittings
are found, replace them. This proposed AD results from mandatory
continuing airworthiness information (MCAI) issued by the airworthiness
authority for France. We are proposing this AD to detect and replace
incorrect length pilot door locking stop-fittings. This condition, if
not corrected, could result in depressurization of the airplane.
DATES: We must receive comments on this proposed AD by October 27,
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 20590-0001.
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 this proposed AD, contact
EADS SOCATA, Direction des Services, 65921 Tarbes Cedex 9, France;
telephone: 33 (0)5 62 41 73 00; fax: 33 (0)5 62 41 76 54; or SOCATA
AIRCRAFT, INC., North Perry Airport, 7501 South Airport Rd., Pembroke
Pines, FL 33023; telephone: (954) 893-1400; fax: (954) 964-4141.
FOR FURTHER INFORMATION CONTACT: Gunnar Berg, Aerospace Safety
Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas
City, Missouri 64106; telephone: (816) 329-4141; fax: (816) 329-4090.
SUPPLEMENTARY INFORMATION:
Comments Invited
We invite you to send any written relevant data, views, or
arguments regarding this proposed AD. Send your comments to an address
listed under the ADDRESSES section. Include the docket number, ``FAA-
2006-25637; Directorate Identifier 2006-CE-43-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 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 Direction g[eacute]n[eacute]rale de l'aviation civile (DGAC),
which is the aviation authority for France, notified FAA that an unsafe
condition may exist on certain EADS SOCATA Model TBM 700 airplanes. The
DGAC reports that the pilot door adjustment procedure was improperly
done, and the pilot door locking stop-fittings may be of incorrect
length. This condition, if not corrected, could result in
depressurization of the airplane.
Relevant Service Information
We have reviewed EADS SOCATA Service Bulletin SB 70-131, ATA No.
53, dated July 2005.
The service information describes procedures for:
Inspecting the pilot door locking stop-fittings for
correct length and
Replacing any incorrect length pilot door locking stop-
fittings.
Foreign Airworthiness Authority Information
The DGAC classified this service bulletin as mandatory and issued
French AD Number F-2005-134, dated August 03, 2005, to ensure the
continued airworthiness of these airplanes in France. These EADS SOCATA
Model TBM 700 airplanes are manufactured in France and are 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 airworthiness agreement.
Under this bilateral airworthiness agreement, the DGAC has kept us
informed of the situation described above.
FAA's Determination and Requirements of the Proposed AD
We are proposing this AD because we have examined the DGAC's
findings, evaluated all information and determined the unsafe condition
described previously is likely to exist or develop on other products of
the same type design that are certificated for operation in the United
States.
This proposed AD would require you to inspect the pilot door
locking stop-fittings for correct length and, if any incorrect length
pilot door locking stop-fittings are found, replace them.
[[Page 56415]]
Differences Between This Proposed AD and the Service Information
The service information allows for unpressurized flight if any
incorrect length pilot door locking-stop fittings are found. If parts
have been ordered but are not available, the proposed AD would permit
unpressurized flight for 90 days after the required inspection or until
parts become available, whichever occurs first. In addition, a placard
in view of the pilot would be installed prohibiting pressurized flight
until the repairs are done. The service information does not have a
compliance time for the repairs or a placard requirement if incorrect
length pilot door locking stop-fittings are found. The requirements of
this proposed AD, if adopted as a final rule, would take precedence
over the provisions in the service information.
Costs of Compliance
We estimate that this proposed AD would affect 157 airplanes in the
U.S. registry.
We estimate the following costs to do the proposed inspection and
repair:
----------------------------------------------------------------------------------------------------------------
Total cost per Total cost on
Labor cost Parts cost airplane U.S. operators
----------------------------------------------------------------------------------------------------------------
4.5 work-hours x $80 per hour = $360......................... $15 $375 $58,875
----------------------------------------------------------------------------------------------------------------
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 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 FAA 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:
EADS SOCATA: Docket No. FAA-2006-25637; Directorate Identifier 2006-
CE-43-AD.
Comments Due Date
(a) We must receive comments on this airworthiness directive
(AD) action by October 27, 2006.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Model TBM 700 airplanes, serial numbers
126 through 322, that are certificated in any category.
Unsafe Condition
(d) This AD results from a pilot door adjustment procedure not
being done properly. We are issuing this AD to detect and correct
incorrect length pilot door locking stop-fittings. This condition,
if not corrected, could result in depressurization of the airplane.
Compliance
(e) To address this problem, you must do the following:
------------------------------------------------------------------------
Actions Compliance Procedures
------------------------------------------------------------------------
(1) Inspect the pilot door Within 30 days Follow EADS SOCATA
locking stop-fittings for after the Service Bulletin
correct length effective date of SB 70-131, ATA
this AD, unless No. 53, dated
already done July 2005.
(2) If any incorrect length Before further Follow EADS SOCATA
pilot door locking stop- flight after the Service Bulletin
fittings are found, replace inspection by SB 70-131, ATA
them paragraph (e)(1) No. 53, dated
of this AD July 2005.
------------------------------------------------------------------------
(f) If you have ordered parts and they are not available, then
you may fly unpressurized until parts become available or for a
period not to exceed 90 days after the inspection required in
paragraph (e)(1) of this AD, whichever occurs first. You must also
fabricate and install a placard as described below. Completing the
action of paragraph (e)(2) of this AD terminates the placard
requirement.
(1) Fabricate (using letters at least \1/8\ inch in height) a
warning placard which states ``This airplane is prohibited from
pressurized flight.''
[[Page 56416]]
(2) Install the placard in full view of the pilot. The owner/
operator holding at least a private pilot certificate as authorized
by section 43.7 of the Federal Aviation Regulations (14 CFR 43.7)
may install the placard as required in paragraph (f) of this AD.
Alternative Methods of Compliance (AMOCs)
(g) The Manager, Standards Office, Small Airplane Directorate,
FAA, ATTN: Gunnar Berg, Aerospace Safety Engineer, FAA, Small
Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri
64106; telephone: (816) 329-4141; fax: (816) 329-4090, has the
authority to approve AMOCs for this AD, if requested using the
procedures found in 14 CFR 39.19.
Related Information
(h) This AD is related to French AD Number F-2005-134, dated
August 3, 2005. To get copies of the service information referenced
in this AD, contact EADS SOCATA, Direction des Services, 65921
Tarbes Cedex 9, France; telephone: 33 (0)5 62 41 73 00; fax: 33 (0)5
62 41 76 54; or SOCATA AIRCRAFT, INC., North Perry Airport, 7501
South Airport Rd., Pembroke Pines, FL 33023; telephone: (954) 893-
1400; fax: (954) 964-4141. To view the AD docket, go to the Docket
Management Facility; U.S. Department of Transportation, 400 Seventh
Street, SW., Nassif Building, Room PL-401, Washington, DC, or on the
Internet at https://dms.dot.gov. The docket number is Docket No. FAA-
2006-25637; Directorate Identifier 2006-CE-43-AD.
Issued in Kansas City, Missouri, on September 20, 2006.
David R. Showers,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 06-8277 Filed 9-26-06; 8:45 am]
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