FR Doc E9-26399

[Federal Register: November 6, 2009 (Volume 74, Number 214)]
[Rules and Regulations]
[Page 57408-57411]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr06no09-4]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2007-27747; Directorate Identifier 2007-CE-030-AD;
Amendment 39-16074; AD 2009-10-09 R1]
RIN 2120-AA64

Airworthiness Directives; Cessna Aircraft Company 150 and 152
Series 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) to revise
AD 2009-10-09, which applies to Cessna Aircraft Company (Cessna) 150
and 152 series airplanes. AD 2009-10-09 requires either installing a
placard prohibiting spins and other acrobatic maneuvers in the airplane
or replacing the rudder stop, the rudder stop bumper, and the
attachment hardware with a new rudder stop modification kit and
replacing the safety wire with jamnuts. Since we issued AD 2009-10-09,
we became aware of a need to clarify certain model and serial number
designations, remove the duplicate requirement of replacing the safety
wire with jamnuts, and clarify the conditional acceptability of using
modification kit part number (P/N) SK152-25 as a terminating action to
this AD. Consequently, this AD retains the actions currently required
in AD 2009-10-09, corrects model designation for certain serial
numbers, removes the duplicate requirement of replacing safety wire
with jamnuts, and clarifies the conditional acceptability of using
modification kit P/N SK152-25 as a terminating action to this AD. We
are issuing this AD to prevent the rudder from traveling past the
normal travel limit. Operation in this non-certificated control
position is unacceptable and could cause undesirable consequences, such
as contact between the rudder and the elevator.

DATES: This AD becomes effective on December 11, 2009.
As of June 17, 2009 (74 FR 22429, May 13, 2009), the Director of
the Federal Register approved the incorporation by reference of Cessna
Aircraft Company Service Bulletin SEB01-1, dated January 22, 2001;
Cessna Aircraft Company Service Kit SK152-25A, Revision A, dated
February 9, 2001; and Cessna Aircraft Company Service Kit SK152-24A,
Revision A, dated March 9, 2001, listed in this AD.

ADDRESSES: For service information identified in this AD, contact
Cessna Aircraft Company, Product Support, P.O. Box 7706, Wichita, KS
67277; telephone: (316) 517-5800; fax: (316) 517-7271; Internet: http:/
/www.cessna.com.
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-2007-27747;
Directorate Identifier 2007-CE-030-AD.

FOR FURTHER INFORMATION CONTACT: Ann Johnson, Aerospace Engineer, FAA,
Wichita Aircraft Certification Office, 1801 Airport Road, Room 100,
Wichita, Kansas 67209; telephone: (316) 946-4105; fax: (316) 946-4107;
e-mail: ann.johnson@faa.gov.

SUPPLEMENTARY INFORMATION:

Discussion

On August 7, 2009, 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 150 and 152 series airplanes. This
proposal was published in the Federal Register as a notice of proposed
rulemaking (NPRM) on August 14, 2009 (74 FR 41096). The NPRM proposed
to revise AD 2009-10-09 with a new AD that would retain the actions
currently required in AD 2009-10-09, correct model designation for
certain serial numbers, remove the duplicate requirement to replace the
safety wire with jamnuts, and clarify the conditional acceptability of
using the P/N SK152-25 kit as a terminating action to the proposed AD.

Comments

We provided the public the opportunity to participate in developing
this AD. We received no comments on the proposal or on the
determination of the cost to the public.

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:
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.

[[Page 57409]]

Costs of Compliance

We estimate that this AD affects 17,090 airplanes in the U.S.
registry.
We estimate the following costs to do the insertion of the
operational limitation:

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Total cost per Total cost on
Labor cost Parts cost airplane U.S. operators
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1 work-hour x $80 per hour = $80............. Not applicable................. $80 $1,367,200
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We estimate the following costs to do the modification:

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Total cost per Total cost on
Labor cost Parts cost airplane U.S. operators
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4 work-hours x $80 per hour = $320........................... $90 $410 $7,006,900
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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-2007-27747; Directorate Identifier 2007-CE-030-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. The FAA amends Sec. 39.13 by removing Airworthiness Directive (AD)
2009-10-09, Amendment 39-15904 (74 FR 22429, May 13, 2009), and adding
the following new AD:

2009-10-09 R1 Cessna Aircraft Company: Amendment 39-16074; Docket
No. FAA-2007-27747; Directorate Identifier 2007-CE-030-AD.

Effective Date

(a) This AD becomes effective on December 11, 2009.

Affected ADs

(b) This AD revises AD 2009-10-09, Amendment 39-15904.

Applicability

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Models Serial Nos.
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(1) 150F............................... 15061533 through 15064532.
(2) 150G............................... 15064533 through 15064969 and
15064971 through 15067198.
(3) 150H............................... 15067199 through 15069308 and
649.
(4) 150J............................... 15069309 through 15071128.
(5) 150K............................... 15071129 through 15072003.
(6) 150L............................... 15072004 through 15075781.
(7) 150M............................... 15075782 through 15079405.
(8) A150K.............................. A1500001 through A1500226.
(9) A150L.............................. A1500227 through A1500432 and
A1500434 through A1500523.
(10) A150M............................. A1500524 through A1500734 and
15064970.
(11) F150F............................. F150-0001 through F150-0067.
(12) F150G............................. F150-0068 through F150-0219.
(13) F150H............................. F150-0220 through F150-0389.
(14) F150J............................. F150-0390 through F150-0529.
(15) F150K............................. F15000530 through F15000658.
(16) F150L............................. F15000659 through F15001143.

[[Page 57410]]

(17) F150M............................. F15001144 through F15001428.
(18) FA150K............................ FA1500001 through FA1500081.
(19) FA150L............................ FA1500082 through FA1500120.
(20) FA150L or FRA150L................. FA1500121 through FA1500261
that are equipped with FKA150-
2311 and FKA150-2316, or
FRA1500121 through FRA1500261.
(21) FA150M or FRA150M................. FA1500262 through FA1500336
that are equipped with FKA150-
2311 and FKA150-2316, or
FRA1500262 through FRA1500336.
(22) 152............................... 15279406 through 15286033.
(23) A152.............................. A1520735 through A1521049,
A1500433, and 681.
(24) F152.............................. F15201429 through F15201980.
(25) FA152............................. FA1520337 through FA1520425.
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Note: This AD revision clarifies the applicability of AD 2009-
10-09, eliminates a duplicate requirement for replacement of safety
wire with jamnuts, and clarifies the intent of the conditional
acceptability of using modification kit P/N SK152-25 as a
terminating requirement to the AD. No further action is required for
those already in compliance with AD 2009-10-09.

Unsafe Condition

(d) Aircraft in full conformity with type design can exceed the
travel limits set by the rudder stops. We are issuing this AD to
prevent the rudder from traveling past the normal travel limit.
Operation in this non-certificated control position is unacceptable
and could cause undesirable consequences, such as contact between
the rudder and the elevator.

Compliance

(e) To address this problem, you must do either the actions in
option 1 or option 2 of this AD, unless already done:

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Actions Compliance Procedures
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(1) Option 1: For all airplanes that Within the next 100 hours time-in- A person authorized to perform
do not have modification kits part service (TIS) after June 17, 2009 maintenance as specified in 14 CFR
number (P/N) SK152-25A or P/N SK152- (the effective date retained from section 43.3 of the Federal
24A installed, do the following: AD 2009-10-09), or within the next Aviation Administration Regulations
(i) Insert the following text into 12 months after June 17, 2009 (the (14 CFR 43.3) is required to make
the Limitations section of the FAA- effective date retained from AD the AFM and POH changes, fabricate
approved airplane flight manual 2009-10-09), whichever occurs first. the placard required in paragraph
(AFM), and pilots operating (e)(1)(i) of this AD, and make an
handbook (POH): ``INTENTIONAL SPINS entry into the aircraft logbook
AND OTHER ACROBATIC/AEROBATIC showing compliance with the portion
MANEUVERS PROHIBITED PER AD 2009-10- of the AD per compliance with 14
09. NOTE: THIS AD DOES NOT PROHIBIT CFR 43.9.
PERFORMING INTENTIONAL STALLS.''
(ii) Fabricate a placard (using
at least \1/8\-inch letters)
with the following words and
install the placard on the
instrument panel within the
pilot's clear view:
``INTENTIONAL SPINS AND OTHER
ACROBATIC/AEROBATIC MANEUVERS
PROHIBITED PER AD 2009-10-09.''.
(iii) The AFM and POH
limitations in paragraph
(e)(1)(i) of the AD and the
placard in paragraph (e)(1)(ii)
of this AD may be removed after
either paragraph (e)(2)(i) or
paragraph (e)(2)(ii) of this AD
is done.
(2) Option 2: Install a rudder stop Within the next 100 hours TIS after Follow Cessna Aircraft Company
modification kit: June 17, 2009 (the effective date Service Bulletin SEB01-1, dated
(i) For airplanes with a forged retained from AD 2009-10-09), or January 22, 2001; and, as
bulkhead, replace the rudder stops, within the next 12 months after applicable, either Cessna Aircraft
rudder stop bumpers, and attachment June 17, 2009 (the effective date Company Service Kit SK152-25A,
hardware with the new rudder stop retained from AD 2009-10-09), Revision A, dated February 9, 2001,
modification kit P/N SK152-25A, whichever occurs first. or Cessna Aircraft Company Service
which includes replacing the safety Kit SK152-24A, Revision A, dated
wire with jamnuts March 9, 2001.
(ii) For airplanes with a sheet
metal bulkhead, replace the
rudder stops, rudder stop
bumpers, and attachment
hardware with the new rudder
stop modification kit P/N SK152-
24A, which includes replacing
the safety wire with jamnuts.
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(f) Kit P/Ns SK152-24 and SK152-25, which are listed in SEB01-1,
were superseded by kit P/Ns SK152-24A and SK152-25A. Cessna has not
revised the service bulletin to reflect the new P/Ns. The kits P/Ns
SK152-24 and SK152-25 will automatically be filled with P/Ns SK152-
24A and SK152-25A, respectively.
(1) The P/N SK152-24 kit does not address the unsafe condition
because the nutplate in the kit can not be used due to rivet spacing
on the aft bulkhead. In addition, a note was added to kit P/N SK152-
24A stating ``some airplanes in this serial range may have a forged
bulkhead installed after leaving the factory. Service Kit SK152-25A
or later revision must be used to modify these airplanes.''
Therefore, kit P/N SK152-24 is not allowed for installation for this
AD.

[[Page 57411]]

(2) The P/N SK152-25 kit did not address the unsafe condition
because a washer that was too small, P/N NAS1149FN832P, was included
in the kit. This error was corrected in the P/N SK152-25A kit. If a
P/N SK152-25 kit is installed using the correct washer P/N
NAS1149F0332P (and this information is recorded in the maintenance
log), credit will be given for installing P/N SK152-25A kit because
this was the only difference between the kits.
(3) If you previously installed a kit P/N SK152-24 or a kit P/N
SK152-25 with washer P/N NAS1149FN832P, and you choose the Option 2
kit installation to comply with this AD, then kit P/N SK152-24A or
either kit P/N SK152-25 with washer P/N NAS1149F0332P or kit P/N
SK152-25A, as applicable, must be installed.
(4) If a P/N SK152-25 kit was installed prior to this AD and the
washer P/N used in the installation is unknown (not recorded in the
maintenance log), and you wish to use Option 2 to comply with this
AD, the installed washer must be replaced with a P/N NAS1149F0332P
washer, and this work must be recorded in the maintenance log.

Alternative Methods of Compliance (AMOCs)

(g) The Manager, FAA, ATTN: Ann Johnson, Aerospace Engineer,
FAA, Wichita Aircraft Certification Office, 1801 Airport Road, Room
100, Wichita, Kansas 67209; telephone: (316) 946-4105; fax: (316)
946-4107; e-mail: ann.johnson@faa.gov, has the authority to approve
AMOCs for this AD, if requested using the procedures found in 14 CFR
39.19. 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.
(h) AMOCs approved for AD 2009-10-09 are approved for this AD.

Material Incorporated by Reference

(i) If you choose to comply with this AD using paragraph (e)(2)
of this AD, you must use Cessna Aircraft Company Service Bulletin
SEB01-1, dated January 22, 2001; and, as applicable, either Cessna
Aircraft Company Service Kit SK152-25A, Revision A, dated February
9, 2001; or Cessna Aircraft Company Service Kit SK152-24A, Revision
A, dated March 9, 2001, to do the actions required by this AD,
unless the AD specifies otherwise.
(1) On June 17, 2009 (74 FR 22429, May 13, 2009), the Director
of the Federal Register approved the incorporation by reference of
Cessna Aircraft Company Service Bulletin SEB01-1, dated January 22,
2001; Cessna Aircraft Company Service Kit SK152-25A, Revision A,
dated February 9, 2001; and Cessna Aircraft Company Service Kit
SK152-24A, Revision A, dated March 9, 2001 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, KS
67277.
(3) You may review copies of the service information
incorporated by reference for this AD at the FAA, Central Region,
Office of the Regional Counsel, 901 Locust, Kansas City, Missouri
64106. For information on the availability of this material at the
Central Region, call (816) 329-3768.
(4) You may also review copies of the service information
incorporated by reference for this AD 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 October 27, 2009.
Kim Smith,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. E9-26399 Filed 11-5-09; 8:45 am]

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