[Federal Register: March 4, 2008 (Volume 73, Number 43)]
[Rules and Regulations]
[Page 11536-11538]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr04mr08-7]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2007-28433; Directorate Identifier 2007-CE-052-AD;
Amendment 39-15403; AD 2008-05-09]
RIN 2120-AA64
Airworthiness Directives; Cessna Aircraft Company 172, 182, and
206 Series Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
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SUMMARY: The FAA adopts a new airworthiness directive (AD) for certain
Cessna Aircraft Company (Cessna) 172, 182, and 206 series airplanes.
This AD requires you to remove the crew seats, modify the seat base/
back attach brackets, and reinstall the seats of the affected
airplanes. This AD results from reports of the seat base/back attach
bracket failing where it is welded to the seat base. We are issuing
this AD to prevent failure of the seat base/back attach brackets, which
could result in the seats collapsing backwards during flight with
consequent loss of control.
DATES: This AD becomes effective on April 8, 2008.
On April 8, 2008, the Director of the Federal Register approved the
incorporation by reference of certain publications listed in this AD.
ADDRESSES: To get the service information identified in this AD,
contact Cessna Aircraft Company, Product Support, P.O. Box 7706,
Wichita, Kansas 67277; telephone: (316) 517-5800; fax: (316) 942-9006.
To view the AD docket, go to U.S. Department of Transportation,
Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200
New Jersey Avenue, SE., Washington, DC 20590, or on the Internet at
http://www.regulations.gov. The docket number is FAA-2007-28433;
Directorate Identifier 2007-CE-052-AD.
FOR FURTHER INFORMATION CONTACT: Gary Park, Aerospace Engineer, 1801
Airport Road, Room 100, Wichita, Kansas 67209; telephone: (316) 946-
4123; fax: (316) 946-4107.
SUPPLEMENTARY INFORMATION:
Discussion
On July 12, 2007, we issued a proposal to amend part 39 of the
Federal Aviation Regulations (14 CFR part 39) to include an AD that
would apply to certain Cessna Models 172, 182, and 206 airplanes. This
proposal was published in the Federal Register as a notice of proposed
rulemaking (NPRM) on July 19, 2007 (72 FR 39584). The NPRM proposed to
remove the crew seats, modify the seat base/back attach brackets, and
reinstall the seats of the affected airplanes and seats 3 and 4 on 206
series airplanes.
Comments
We provided the public the opportunity to participate in developing
this AD. The following presents the comments received on the proposal
and FAA's response to each comment:
Comment Issue No. 1: Number of Affected Airplanes
Jack Buster with the Modification and Replacement Part Association
(MARPA) noted that the airworthiness concern sheet stated the proposed
AD action affected 2,770 airplanes and the actual proposed AD stated
the action affected 1,556 airplanes. He requests we clarify the number
of the affected airplanes.
The FAA agrees that the numbers in the airworthiness concern sheet
and the proposed AD differ. There are 2,770 airplanes worldwide but
only 1,556 airplanes on the U.S. Registry. In the Cost of Compliance
section of the AD preamble we state how many airplanes are listed on
the U.S. Registry.
We will not change the final rule AD action as a result of this
comment.
Comment Issue No. 2: Availability of Incorporated by Reference (IBR)
Documents in the Docket Management System (DMS)
Jack Buster of MARPA requests IBR documents be available to the
public by publication in the DMS.
The FAA has transitioned from the DMS to the government-wide
Federal Docket Management System (FDMS). We are currently reviewing
issues surrounding the posting of service bulletins in the FDMS as part
of the AD docket. Once we have thoroughly examined all aspects of this
issue and have made a final determination, we will consider whether our
current practice needs to be revised.
Comment Issue No. 3: Exempting Non-crew Seats From This AD Action
The Aircraft Owners and Pilots Association requests that the FAA
exempt non-crew seats from the AD action. Modification of the third and
fourth seats on the Cessna Model 206 is estimated at just under $1,000
per aircraft and does not directly address the safety of flight issue
proposed for this AD. The third and fourth seats are not crew seats and
pose little to no risk that a seat collapse could cause the pilot to
lose control of the airplane.
The FAA agrees that the modification of the third and fourth seats
on the Cessna 206 does not directly address the safety of flight issue
proposed for this AD.
We will change the final rule AD action as a result of this comment
and not include seats 3 and 4 on 206 series airplanes.
Conclusion
We have carefully reviewed the available data and determined that
air safety and the public interest require adopting the AD as proposed
except for minor editorial corrections. We have determined that these
minor corrections:
[[Page 11537]]
Are consistent with the intent that was proposed in the
NPRM for correcting the unsafe condition; and
do not add any additional burden upon the public than was
already proposed in the NPRM.
Costs of Compliance
We estimate that this AD affects 1,556 airplanes in the U.S.
registry.
We estimate the following costs to do the modification:
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Total cost per Total cost on U.S.
Labor cost Parts cost airplane operators
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5 work-hours x $80 per hour = $400 (for $800 (for two crew seats)... $1,200 $1,867,200
two crew seats).
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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 AD.
Regulatory Findings
We have 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); 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 summary of the costs to comply with this AD (and
other information as included in the Regulatory Evaluation) and placed
it in the AD Docket. You may get a copy of this summary by sending a
request to us at the address listed under ADDRESSES. Include ``Docket
No. FAA-2007-28433; Directorate Identifier 2007-CE-052-AD'' in your
request.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
0
Accordingly, under the authority delegated to me by the Administrator,
the Federal Aviation Administration amends part 39 of the Federal
Aviation Regulations (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. FAA amends Sec. 39.13 by adding a new AD to read as follows:
2008-05-09 Cessna Aircraft Company: Amendment 39-15403; Docket No.
FAA-2007-28433; Directorate Identifier 2007-CE-052-AD.
Effective Date
(a) This AD becomes effective on April 8, 2008.
Affected ADs
(b) None.
Applicability
(c) This AD applies to the following airplane models and serial
numbers that are certificated in any category:
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Models Serial Nos.
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(1) 172R................... 17281211 through 17281356.
(2) 172S................... 172S9621 through 172S10310, 172S10312
through 172S10324, 172S10327 through
172S10332, 172S10334 through 172S10349,
172S10351 through 172S10374, 172S10376
through 172S10386, 172S10388 through
172S10408, 172S10410 through 172S10412,
172S10414 through 172S10417, and 172S10421
through 172S10423.
(3) 182T................... 18281328 through 18281867, 18281869 through
18281871, 18281873 through 18281875, and
18281877.
(4) T182T.................. T18208240 through T18208651, T18208654,
T18208656 through T18208659, T18208663,
T18208664, and T18208667 through
T18208668.
(5) 206H................... 20608216 through 20608283.
(6) T206H.................. T20608445 through T20608662, T20608664
through T20608671, T20608673, T20608674,
T20608676 through T20608681, T20608683
through T20608689, T20608691, T20608692,
T20608694 through T20608696, T20608699
through T20608701, T20608703, and
T20608704.
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Unsafe Condition
(d) This AD results from reports of the seat base/back attach
bracket failing where it is welded to the seat base. We are issuing
this AD to prevent failure of the seat base/back attach brackets,
which could result in the seats collapsing backwards during flight
with consequent loss of control.
Compliance
(e) To address this problem, you must do the following, unless
already done:
[[Page 11538]]
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Actions Compliance Procedures
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Remove, modify, and Within the next 50 Follow Cessna
reinstall the crew seats. hours time-in- Aircraft Company
service after April Single Engine
8, 2008 (the Modification Kit
effective date of No. MK206-25-10,
this AD) or within dated April 23,
the next 6 months 2007, as specified
after April 8, 2008 in Cessna Aircraft
(the effective date Company Service
of this AD), Bulletin SB07-25-
whichever occurs 04, dated April 23,
first. 2007.
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Alternative Methods of Compliance (AMOCs)
(f) The Manager, Wichita Aircraft Certification Office, FAA, has
the authority to approve AMOCs for this AD, if requested using the
procedures found in 14 CFR 39.19. Send information to ATTN: Gary
Park, Aerospace Engineer, 1801 Airport Road, Room 100, Wichita,
Kansas 67209; telephone: (316) 946-4123; fax: (316) 946-4107. Before
using any approved AMOC on any airplane to which the AMOC applies,
notify your appropriate principal inspector (PI) in the FAA Flight
Standards District Office (FSDO), or lacking a PI, your local FSDO.
Related Information
(g) To get copies of the service information referenced in this
AD, contact Cessna Aircraft Company, Product Support, P.O. Box 7706,
Wichita, Kansas 67277; telephone: (316) 517-5800; fax: (316) 942-
9006. To view the AD docket, go to U.S. Department of
Transportation, Docket Operations, M-30, West Building Ground Floor,
Room W12-140, 1200 New Jersey Avenue, SE., Washington, DC 20590, or
on the Internet at http://dms.dot.gov. The docket number is Docket
No. FAA-2007-28433; Directorate Identifier 2007-CE-052-AD.
Material Incorporated by Reference
(h) You must use Cessna Aircraft Company Single Engine
Modification Kit No. MK206-25-10, dated April 23, 2007, as specified
in Cessna Aircraft Company Service Bulletin SB07-25-04, dated April
23, 2007, to do the actions required by this AD, unless the AD
specifies otherwise.
(1) The Director of the Federal Register approved the
incorporation by reference of this service information under 5
U.S.C. 552(a) and 1 CFR part 51.
(2) For service information identified in this AD, contact
Cessna Aircraft Company, Product Support, P.O. Box 7706, Wichita,
Kansas 67277; telephone: (316) 517-5800; fax: (316) 942-9006.
(3) You may review copies at the FAA, Central Region, Office of
the Regional Counsel, 901 Locust, Kansas City, Missouri 64106; or 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/code_
of_federal_regulations/ibr_locations.html.
Issued in Kansas City, Missouri, on February 22, 2008.
Patrick R. Mullen,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E8-3771 Filed 3-3-08; 8:45 am]
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