81 FR 44207 - Airworthiness Directives; Textron Aviation Inc. Airplanes

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration

Federal Register Volume 81, Issue 130 (July 7, 2016)

Page Range		44207-44209
FR Document		2016-15866

We are superseding Airworthiness Directive (AD) 2008-15-06 for certain Textron Aviation Inc. Models 175 and 175A airplanes (type certificate previously held by Cessna Aircraft Company). AD 2008-15-06 required checking the airplane logbook to determine if the original engine mounting brackets had been replaced. If the original engine mounting brackets were still installed, the AD required repetitively inspecting those brackets for cracks and replacing any cracked engine mounting bracket until all four original engine mounting brackets were replaced. Replacing all four original engine mounting brackets terminated the actions required in AD 2008-15-06. Since we issued AD 2008-15-06, we have determined that the applicability needs to be changed to add one serial number and remove another. This new AD retains the actions required in AD 2008-15-06 and changes the Applicability section. We are issuing this AD to correct the unsafe condition on these products.

Federal Register, Volume 81 Issue 130 (Thursday, July 7, 2016)

[Federal Register Volume 81, Number 130 (Thursday, July 7, 2016)]
[Rules and Regulations]
[Pages 44207-44209]
From the Federal Register Online  [www.thefederalregister.org]
[FR Doc No: 2016-15866]



========================================================================
Rules and Regulations
                                                Federal Register
________________________________________________________________________

This section of the FEDERAL REGISTER contains regulatory documents 
having general applicability and legal effect, most of which are keyed 
to and codified in the Code of Federal Regulations, which is published 
under 50 titles pursuant to 44 U.S.C. 1510.

The Code of Federal Regulations is sold by the Superintendent of Documents. 
Prices of new books are listed in the first FEDERAL REGISTER issue of each 
week.

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Federal Register / Vol. 81, No. 130 / Thursday, July 7, 2016 / Rules 
and Regulations

[[Page 44207]]



DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2016-5579; Directorate Identifier 2016-CE-010-AD; 
Amendment 39-18586; AD 2016-14-05]
RIN 2120-AA64


Airworthiness Directives; Textron Aviation Inc. Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

-----------------------------------------------------------------------

SUMMARY: We are superseding Airworthiness Directive (AD) 2008-15-06 for 
certain Textron Aviation Inc. Models 175 and 175A airplanes (type 
certificate previously held by Cessna Aircraft Company). AD 2008-15-06 
required checking the airplane logbook to determine if the original 
engine mounting brackets had been replaced. If the original engine 
mounting brackets were still installed, the AD required repetitively 
inspecting those brackets for cracks and replacing any cracked engine 
mounting bracket until all four original engine mounting brackets were 
replaced. Replacing all four original engine mounting brackets 
terminated the actions required in AD 2008-15-06. Since we issued AD 
2008-15-06, we have determined that the applicability needs to be 
changed to add one serial number and remove another. This new AD 
retains the actions required in AD 2008-15-06 and changes the 
Applicability section. We are issuing this AD to correct the unsafe 
condition on these products.

DATES: This AD is effective August 11, 2016.
    The Director of the Federal Register approved the incorporation by 
reference of a certain other publication listed in this AD as of 
September 2, 2008 (73 FR 43845, July 29, 2008).

ADDRESSES: For service information identified in this final rule, 
contact Cessna Aircraft Company, Product Support, P.O. Box 7706, 
Wichita, Kansas 67277; telephone: (316) 517-5800; fax: (316) 942-9006; 
Internet: www.cessna.txtav.com. You may view this referenced service 
information at the FAA, Small Airplane Directorate, 901 Locust, Kansas 
City, Missouri 64106. For information on the availability of this 
material at the FAA, call (816) 329-4148. It is also available on the 
Internet at http://www.regulations.gov by searching for and locating 
Docket No. FAA-2016-5579.

Examining the AD Docket

    You may examine the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016-
5579; 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 AD, the regulatory evaluation, any comments received, and 
other information. The address for the Docket Office (phone: 800-647-
5527) is Document Management Facility, U.S. Department of 
Transportation, Docket Operations, M-30, West Building Ground Floor, 
Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590.

FOR FURTHER INFORMATION CONTACT: Gary Park, Aerospace Engineer, Wichita 
Aircraft Certification Office, 1801 Airport Road, Room 100, Wichita, 
Kansas 67209; telephone: (316) 946-4123; fax: (316) 946-4107, email: 
[email protected].

SUPPLEMENTARY INFORMATION:

Discussion

    We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR 
part 39 to supersede AD 2008-15-06, Amendment 39-15618 (73 FR 43845, 
July 29, 2008), (``AD 2008-15-06''). AD 2008-15-06 applied to certain 
Textron Aviation Inc. Models 175 and 175A airplanes (type certificate 
previously held by Cessna Aircraft Company). The NPRM published in the 
Federal Register on April 12, 2016 (81 FR 21501). The NPRM was prompted 
by our determination that a serial number had been inadvertently 
included in the applicability and a serial number had been 
inadvertently omitted from the applicability. The NPRM proposed to 
retain the requirements of AD 2008-15-06, add one serial number to the 
applicability and remove another. We are issuing this AD to correct the 
unsafe condition on these products.

Comments

    We gave the public the opportunity to participate in developing 
this AD. We received no comments on the NPRM (81 FR 21501, April 12, 
2016) or on the determination of the cost to the public.

Conclusion

    We reviewed the relevant data and determined that air safety and 
the public interest require adopting this AD as proposed except for 
minor editorial changes. We have determined that these minor changes:
     Are consistent with the intent that was proposed in the 
NPRM (81 FR 21501, April 12, 2016) for correcting the unsafe condition; 
and
     Do not add any additional burden upon the public than was 
already proposed in the NPRM (81 FR 21501, April 12, 2016).

Related Service Information Under 1 CFR Part 51

    We reviewed Cessna Single Engine Service Bulletin SEB07-2, Revision 
2, dated June 18, 2007. The service information describes procedures 
for inspecting the upper and lower engine mounting brackets on both the 
left and right sides for cracks and replacing cracked engine mounting 
brackets. This service information is reasonably available because the 
interested parties have access to it through their normal course of 
business or by the means identified in the ADDRESSES section.

Costs of Compliance

    We estimate that this AD will affect 1,218 airplanes in the U.S. 
registry.
    We estimate the following costs to do each inspection:

[[Page 44208]]



----------------------------------------------------------------------------------------------------------------
                                                                                 Total cost per   Total cost on
                  Labor cost                              Parts cost                airplane      U.S. operators
----------------------------------------------------------------------------------------------------------------
7.5 work-hours x $80 per hour = $600.........  Not applicable.................            $600         $730,800
----------------------------------------------------------------------------------------------------------------

    We estimate the following costs to do any necessary replacements:

------------------------------------------------------------------------
                                                        Total cost per
           Labor cost                 Parts cost           airplane
------------------------------------------------------------------------
3 work-hours per bracket x $80    $200 per bracket.   $440 per bracket.
 per hour = $240 per bracket. 4    4 x $200 = $800     $1,760 to replace
 brackets per airplane x $240      for all 4           all 4 brackets.
 per bracket = $960.               brackets.
------------------------------------------------------------------------

    There is no estimated cost of compliance difference between this AD 
and AD 2008-15-06 since there is no change in the number of affected 
airplanes or in the required actions. The cost impact on the public 
will be in the removal of serial number 691 and the addition of serial 
number 619.

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 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 DOT Regulatory Policies and 
Procedures (44 FR 11034, February 26, 1979),
    (3) Will not affect intrastate aviation in Alaska, and
    (4) Will not have a significant economic impact, positive or 
negative, on a substantial number of small entities under the criteria 
of the Regulatory Flexibility Act.

List of Subjects in 14 CFR Part 39

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

Adoption of the Amendment

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

PART 39--AIRWORTHINESS DIRECTIVES

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

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


Sec.  39.13  [Amended]

0
2. The FAA amends Sec.  39.13 by removing Airworthiness Directive (AD) 
2008-15-06, Amendment 39-15618 (73 FR 43845, July 29, 2008), and adding 
the following new AD:

2016-14-05 Textron Aviation Inc.: Amendment 39-18586; Docket No. 
FAA-2016-5579; Directorate Identifier 2016-CE-010.

(a) Effective Date

    This AD is effective August 11, 2016.

(b) Affected ADs

    This AD replaces AD 2008-15-06, Amendment 39-15618 (73 FR 43845, 
July 29, 2008) (``AD 2008-15-06'').

(c) Applicability

    This AD applies to the Textron Aviation Inc. airplane models and 
serial numbers (type certificate previously held by Cessna Aircraft 
Company) that are certificated in any category listed in Table 1 to 
paragraph (c) of this AD. The new airplane affected by this AD is 
model number 175A, serial number 619, manufactured in 1960.

         Table 1 to Paragraph (c) of This AD--Airplanes Affected
------------------------------------------------------------------------
             Model                  Serial Nos.       Year manufactured
------------------------------------------------------------------------
(1) 175........................  55001 through      1958.
                                  55703.
(2) 175........................  55704 through      1959.
                                  56238.
(3) 175........................  28700A, 626, and   1958 and 1959.
                                  640.
(4) 175 A......................  56239 through      1960.
                                  56777.
(5) 175 A......................  619..............  1960.
------------------------------------------------------------------------

(d) Subject

    Joint Aircraft System Component (JASC)/Air Transport Association 
(ATA) of America Code 71, Power Plant.

(e) Unsafe Condition

    This AD was prompted by the determination that one airplane 
needs to be added and another airplane needs to be removed from the 
Applicability section. We are issuing this AD to detect and correct 
cracks in the engine mounting brackets, which could result in 
failure of the engine mounting bracket. This failure could lead to 
the engine detaching from the firewall.

[[Page 44209]]

(f) Compliance

    Comply with this AD within the compliance times specified, 
unless already done.

(g) Airplane Logbook Check

    (1) Check the airplane logbook to determine if all four of the 
original engine mounting brackets have been replaced. Do the logbook 
check at the following compliance time, as applicable. The owner/
operator holding at least a private pilot certificate as authorized 
by section 43.7 may do this action.
    (i) For airplanes previously affected by AD 2008-15-06: Within 
the next 30 days after September 2, 2008 (the effective date 
retained from AD 2008-15-06).
    (ii) For the new airplane affected by this AD: Within the next 
30 days after August 11, 2016 (the effective date of this AD).
    (2) If you can positively determine that all four of the 
original engine mounting brackets have been replaced, no further 
action is required. Make an entry into the airplane logbook showing 
compliance with this portion of the AD in accordance with 14 CFR 
43.9. The owner/operator holding at least a private pilot 
certificate as authorized by section 43.7 may do this action.
    (3) If you cannot positively determine that all four of the 
original engine mounting brackets have been replaced, inspect each 
of the upper and lower engine mounting brackets on both the left and 
right sides for cracks following Cessna Single Engine Service 
Bulletin SEB07-2, Revision 2, dated June 18, 2007. Do the 
inspections at the following compliance times, as applicable.
    (i) For airplanes previous affected by AD 2008-15-06: Initially 
inspect within the next 12 months after September 2, 2008 (the 
effective date retained from AD 2008-15-06). If no cracks are found, 
repetitively inspect thereafter at intervals not to exceed 500 hours 
time-in-service (TIS) until all four of the original engine mounting 
brackets are replaced.
    (ii) For the new airplane affected by this AD: Initially inspect 
within the next 12 months after August 11, 2016 (the effective date 
of this AD). If no cracks are found, repetitively inspect thereafter 
at intervals not to exceed 500 hours TIS until all four of the 
original engine mounting brackets are replaced.

(h) Engine Mounting Bracket Replacement

    If cracks are found in any of the engine mounting brackets 
during any inspection required in paragraph (g)(3) of this AD, 
including all subparagraphs, before further flight after the 
inspection in which cracks are found, replace the cracked engine 
mounting bracket(s) following Cessna Single Engine Service Bulletin 
SEB07-2, Revision 2, dated June 18, 2007. Replacing the cracked 
engine mounting bracket terminates the repetitive inspections 
required in paragraphs (g)(3)(i) and (ii) of this AD only for the 
replaced engine mounting bracket.

(i) Terminating Action

    To terminate the repetitive inspections required in paragraphs 
(g)(3)(i) and (ii) of this AD, you may replace all four original 
engine mounting brackets following Cessna Single Engine Service 
Bulletin SEB07-2, Revision 2, dated June 18, 2007.

(j) Engine Mounting Bracket Disposal

    For all airplanes affected by this AD: Before further flight 
after the engine mounting bracket is removed for replacement, 
dispose of every replaced bracket following 14 CFR 43.10, paragraph 
(c)(6), which states the following: ``Mutilation. The part may be 
mutilated to deter its installation in a type certificated product. 
The mutilation must render the part beyond repair and incapable of 
being reworked to appear to be airworthy.''

(k) Alternative Methods of Compliance (AMOCs)

    (1) The Manager, Wichita Aircraft Certification Office (ACO), 
FAA, has the authority to approve AMOCs for this AD, if requested 
using the procedures found in 14 CFR 39.19. In accordance with 14 
CFR 39.19, send your request to your principal inspector or local 
Flight Standards District Office, as appropriate. If sending 
information directly to the manager of the ACO, send it to the 
attention of the person identified in paragraph (l) of this AD.
    (2) Before using any approved AMOC, notify your appropriate 
principal inspector, or lacking a principal inspector, the manager 
of the local flight standards district office/certificate holding 
district office.
    (3) AMOCs approved for AD 2008-15-06 are approved as AMOCs for 
the corresponding provisions of this AD.

(l) Related Information

    For more information about this AD, contact Gary Park, Aerospace 
Engineer, Wichita ACO, 1801 Airport Road, Room 100, Wichita, Kansas 
67209; telephone: (316) 946-4123; fax: (316) 946-4107, email: 
[email protected]

(m) Material Incorporated by Reference

    (1) The Director of the Federal Register approved the 
incorporation by reference (IBR) of the service information listed 
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
    (2) You must use this service information as applicable to do 
the actions required by this AD, unless the AD specifies otherwise.
    (3) The following service information was approved for IBR on 
September 2, 2008 (73 FR 43845, July 29, 2008).
    (i) Cessna Single Engine Service Bulletin SEB07-2, Revision 2, 
dated June 18, 2007.
    (ii) Reserved.
    (4) For Cessna Aircraft Company 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; Internet: www.cessna.txtav.com.
    (5) You may view this service information at FAA, Small Airplane 
Directorate, 901 Locust, Kansas City, Missouri 64106. For 
information on the availability of this material at the FAA, call 
(816) 329-4148. In addition, you can access this service information 
on the Internet at http://www.regulations.gov by searching for and 
locating Docket No. FAA-2016-5579.
    (6) You may view this service information that is incorporated 
by reference at the National Archives and Records Administration 
(NARA). For information on the availability of this material at 
NARA, call 202-741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued in Kansas City, Missouri, on June 28, 2016.
Pat Mullen,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2016-15866 Filed 7-6-16; 8:45 am]
 BILLING CODE 4910-13-P

44207

Rules and Regulations Federal Register
Vol. 81, No. 130

Thursday, July 7, 2016

This section of the FEDERAL REGISTER of a certain other publication listed in NPRM published in the Federal
contains regulatory documents having general this AD as of September 2, 2008 (73 FR Register on April 12, 2016 (81 FR
applicability and legal effect, most of which 43845, July 29, 2008). 21501). The NPRM was prompted by
are keyed to and codified in the Code of our determination that a serial number
ADDRESSES: For service information
Federal Regulations, which is published under had been inadvertently included in the
50 titles pursuant to 44 U.S.C. 1510. identified in this final rule, contact
Cessna Aircraft Company, Product applicability and a serial number had
The Code of Federal Regulations is sold by Support, P.O. Box 7706, Wichita, been inadvertently omitted from the
the Superintendent of Documents. Prices of Kansas 67277; telephone: (316) 517– applicability. The NPRM proposed to
new books are listed in the first FEDERAL 5800; fax: (316) 942–9006; Internet: retain the requirements of AD 2008–15–
REGISTER issue of each week. www.cessna.txtav.com. You may view 06, add one serial number to the
this referenced service information at applicability and remove another. We
the FAA, Small Airplane Directorate, are issuing this AD to correct the unsafe
DEPARTMENT OF TRANSPORTATION 901 Locust, Kansas City, Missouri condition on these products.
64106. For information on the Comments
Federal Aviation Administration
availability of this material at the FAA,
call (816) 329–4148. It is also available We gave the public the opportunity to
14 CFR Part 39
on the Internet at http:// participate in developing this AD. We
[Docket No. FAA–2016–5579; Directorate www.regulations.gov by searching for received no comments on the NPRM (81
Identifier 2016–CE–010–AD; Amendment and locating Docket No. FAA–2016– FR 21501, April 12, 2016) or on the
39–18586; AD 2016–14–05] 5579. determination of the cost to the public.
RIN 2120–AA64
Examining the AD Docket Conclusion
Airworthiness Directives; Textron You may examine the AD docket on We reviewed the relevant data and
Aviation Inc. Airplanes the Internet at http:// determined that air safety and the
www.regulations.gov by searching for public interest require adopting this AD
AGENCY: Federal Aviation
and locating Docket No. FAA–2016– as proposed except for minor editorial
Administration (FAA), DOT.
5579; or in person at the Docket changes. We have determined that these
ACTION: Final rule. Management Facility between 9 a.m. minor changes:
and 5 p.m., Monday through Friday,
SUMMARY: We are superseding • Are consistent with the intent that
Airworthiness Directive (AD) 2008–15– except Federal holidays. The AD docket
was proposed in the NPRM (81 FR
06 for certain Textron Aviation Inc. contains this AD, the regulatory
21501, April 12, 2016) for correcting the
Models 175 and 175A airplanes (type evaluation, any comments received, and
unsafe condition; and
certificate previously held by Cessna other information. The address for the
Docket Office (phone: 800–647–5527) is • Do not add any additional burden
Aircraft Company). AD 2008–15–06
Document Management Facility, U.S. upon the public than was already
required checking the airplane logbook
Department of Transportation, Docket proposed in the NPRM (81 FR 21501,
to determine if the original engine
Operations, M–30, West Building April 12, 2016).
mounting brackets had been replaced. If
the original engine mounting brackets Ground Floor, Room W12–140, 1200 Related Service Information Under 1
were still installed, the AD required New Jersey Avenue SE., Washington, CFR Part 51
repetitively inspecting those brackets for DC 20590.
cracks and replacing any cracked engine FOR FURTHER INFORMATION CONTACT: Gary We reviewed Cessna Single Engine
mounting bracket until all four original Park, Aerospace Engineer, Wichita Service Bulletin SEB07–2, Revision 2,
engine mounting brackets were Aircraft Certification Office, 1801 dated June 18, 2007. The service
replaced. Replacing all four original Airport Road, Room 100, Wichita, information describes procedures for
engine mounting brackets terminated Kansas 67209; telephone: (316) 946– inspecting the upper and lower engine
the actions required in AD 2008–15–06. 4123; fax: (316) 946–4107, email: mounting brackets on both the left and
Since we issued AD 2008–15–06, we gary.park@faa.gov. right sides for cracks and replacing
have determined that the applicability cracked engine mounting brackets. This
SUPPLEMENTARY INFORMATION:
needs to be changed to add one serial service information is reasonably
number and remove another. This new Discussion available because the interested parties
AD retains the actions required in AD We issued a notice of proposed have access to it through their normal
2008–15–06 and changes the rulemaking (NPRM) to amend 14 CFR course of business or by the means
Applicability section. We are issuing part 39 to supersede AD 2008–15–06, identified in the ADDRESSES section.
this AD to correct the unsafe condition Amendment 39–15618 (73 FR 43845, Costs of Compliance
on these products. July 29, 2008), (‘‘AD 2008–15–06’’). AD
DATES: This AD is effective August 11, 2008–15–06 applied to certain Textron We estimate that this AD will affect
Lhorne on DSK30JT082PROD with RULES

2016. Aviation Inc. Models 175 and 175A 1,218 airplanes in the U.S. registry.
The Director of the Federal Register airplanes (type certificate previously We estimate the following costs to do
approved the incorporation by reference held by Cessna Aircraft Company). The each inspection:

VerDate Sep<11>2014 13:01 Jul 06, 2016 Jkt 238001 PO 00000 Frm 00001 Fmt 4700 Sfmt 4700 E:\FR\FM\07JYR1.SGM 07JYR1

44208 Federal Register / Vol. 81, No. 130 / Thursday, July 7, 2016 / Rules and Regulations

Total cost per Total cost on
Labor cost Parts cost airplane U.S. operators

7.5 work-hours × $80 per hour = $600 ..................................................... Not applicable .................................. $600 $730,800

We estimate the following costs to do
any necessary replacements:

Labor cost Parts cost Total cost per airplane

3 work-hours per bracket × $80 per hour = $240 per bracket. 4 brack- $200 per bracket. 4 × $200 = $800 $440 per bracket. $1,760 to re-
ets per airplane × $240 per bracket = $960. for all 4 brackets. place all 4 brackets.

There is no estimated cost of Regulatory Findings PART 39—AIRWORTHINESS
compliance difference between this AD We have determined that this AD will DIRECTIVES
and AD 2008–15–06 since there is no not have federalism implications under
change in the number of affected Executive Order 13132. This AD will ■ 1. The authority citation for part 39
airplanes or in the required actions. The not have a substantial direct effect on continues to read as follows:
cost impact on the public will be in the the States, on the relationship between Authority: 49 U.S.C. 106(g), 40113, 44701.
removal of serial number 691 and the the national government and the States,
addition of serial number 619. or on the distribution of power and § 39.13 [Amended]
responsibilities among the various
Authority for This Rulemaking levels of government. ■ 2. The FAA amends § 39.13 by
For the reasons discussed above, I removing Airworthiness Directive (AD)
Title 49 of the United States Code 2008–15–06, Amendment 39–15618 (73
specifies the FAA’s authority to issue certify that this AD:
(1) Is not a ‘‘significant regulatory FR 43845, July 29, 2008), and adding the
rules on aviation safety. Subtitle I, following new AD:
action’’ under Executive Order 12866,
Section 106, describes the authority of (2) Is not a ‘‘significant rule’’ under
the FAA Administrator. Subtitle VII, 2016–14–05 Textron Aviation Inc.:
DOT Regulatory Policies and Procedures Amendment 39–18586; Docket No.
Aviation Programs, describes in more (44 FR 11034, February 26, 1979), FAA–2016–5579; Directorate Identifier
detail the scope of the Agency’s (3) Will not affect intrastate aviation 2016–CE–010.
authority. in Alaska, and
(4) Will not have a significant (a) Effective Date
We are issuing this rulemaking under
the authority described in Subtitle VII, economic impact, positive or negative, This AD is effective August 11, 2016.
Part A, Subpart III, section 44701, on a substantial number of small entities (b) Affected ADs
‘‘General requirements.’’ Under that under the criteria of the Regulatory
This AD replaces AD 2008–15–06,
section, Congress charges the FAA with Flexibility Act.
Amendment 39–15618 (73 FR 43845, July 29,
promoting safe flight of civil aircraft in List of Subjects in 14 CFR Part 39 2008) (‘‘AD 2008–15–06’’).
air commerce by prescribing regulations Air transportation, Aircraft, Aviation (c) Applicability
for practices, methods, and procedures safety, Incorporation by reference,
the Administrator finds necessary for This AD applies to the Textron Aviation
Safety. Inc. airplane models and serial numbers
safety in air commerce. This regulation
Adoption of the Amendment (type certificate previously held by Cessna
is within the scope of that authority Aircraft Company) that are certificated in any
because it addresses an unsafe condition Accordingly, under the authority category listed in Table 1 to paragraph (c) of
that is likely to exist or develop on delegated to me by the Administrator, this AD. The new airplane affected by this
products identified in this rulemaking the FAA amends 14 CFR part 39 as AD is model number 175A, serial number
action. follows: 619, manufactured in 1960.

TABLE 1 TO PARAGRAPH (c) OF THIS AD—AIRPLANES AFFECTED
Year
Model Serial Nos. manufactured

(1) 175 ........................................................................................ 55001 through 55703 ................................................................ 1958.
(2) 175 ........................................................................................ 55704 through 56238 ................................................................ 1959.
(3) 175 ........................................................................................ 28700A, 626, and 640 ............................................................... 1958 and 1959.
(4) 175 A .................................................................................... 56239 through 56777 ................................................................ 1960.
(5) 175 A .................................................................................... 619 ............................................................................................. 1960.

(d) Subject (e) Unsafe Condition which could result in failure of the engine
Lhorne on DSK30JT082PROD with RULES

Joint Aircraft System Component (JASC)/ This AD was prompted by the mounting bracket. This failure could lead to
Air Transport Association (ATA) of America determination that one airplane needs to be the engine detaching from the firewall.
Code 71, Power Plant. added and another airplane needs to be
removed from the Applicability section. We
are issuing this AD to detect and correct
cracks in the engine mounting brackets,

VerDate Sep<11>2014 13:01 Jul 06, 2016 Jkt 238001 PO 00000 Frm 00002 Fmt 4700 Sfmt 4700 E:\FR\FM\07JYR1.SGM 07JYR1

Federal Register / Vol. 81, No. 130 / Thursday, July 7, 2016 / Rules and Regulations 44209

(f) Compliance mounting brackets following Cessna Single (6) You may view this service information
Comply with this AD within the Engine Service Bulletin SEB07–2, Revision 2, that is incorporated by reference at the
compliance times specified, unless already dated June 18, 2007. National Archives and Records
done. Administration (NARA). For information on
(j) Engine Mounting Bracket Disposal the availability of this material at NARA, call
(g) Airplane Logbook Check For all airplanes affected by this AD: 202–741–6030, or go to: http://
(1) Check the airplane logbook to Before further flight after the engine www.archives.gov/federal-register/cfr/ibr-
determine if all four of the original engine mounting bracket is removed for locations.html.
mounting brackets have been replaced. Do replacement, dispose of every replaced
Issued in Kansas City, Missouri, on June
the logbook check at the following bracket following 14 CFR 43.10, paragraph
28, 2016.
compliance time, as applicable. The owner/ (c)(6), which states the following:
‘‘Mutilation. The part may be mutilated to Pat Mullen,
operator holding at least a private pilot
certificate as authorized by section 43.7 may deter its installation in a type certificated Acting Manager, Small Airplane Directorate,
do this action. product. The mutilation must render the part Aircraft Certification Service.
(i) For airplanes previously affected by AD beyond repair and incapable of being [FR Doc. 2016–15866 Filed 7–6–16; 8:45 am]
2008–15–06: Within the next 30 days after reworked to appear to be airworthy.’’
BILLING CODE 4910–13–P
September 2, 2008 (the effective date retained (k) Alternative Methods of Compliance
from AD 2008–15–06). (AMOCs)
(ii) For the new airplane affected by this
AD: Within the next 30 days after August 11, (1) The Manager, Wichita Aircraft DEPARTMENT OF HOMELAND
2016 (the effective date of this AD). Certification Office (ACO), FAA, has the SECURITY
(2) If you can positively determine that all authority to approve AMOCs for this AD, if
four of the original engine mounting brackets requested using the procedures found in 14 Coast Guard
CFR 39.19. In accordance with 14 CFR 39.19,
have been replaced, no further action is
send your request to your principal inspector 33 CFR Part 165
required. Make an entry into the airplane
or local Flight Standards District Office, as
logbook showing compliance with this
appropriate. If sending information directly [Docket No. USCG–2016–0493]
portion of the AD in accordance with 14 CFR
to the manager of the ACO, send it to the
43.9. The owner/operator holding at least a
private pilot certificate as authorized by
attention of the person identified in Safety Zone; Southern California
paragraph (l) of this AD. Annual Fireworks for the San Diego
section 43.7 may do this action.
(2) Before using any approved AMOC, Captain of the Port Zone
(3) If you cannot positively determine that
notify your appropriate principal inspector,
all four of the original engine mounting or lacking a principal inspector, the manager AGENCY: Coast Guard, DHS.
brackets have been replaced, inspect each of of the local flight standards district office/
the upper and lower engine mounting ACTION: Notice of enforcement of
certificate holding district office. regulation.
brackets on both the left and right sides for (3) AMOCs approved for AD 2008–15–06
cracks following Cessna Single Engine are approved as AMOCs for the
Service Bulletin SEB07–2, Revision 2, dated SUMMARY: The Coast Guard will enforce
corresponding provisions of this AD. a safety zone for the San Diego, CA
June 18, 2007. Do the inspections at the
following compliance times, as applicable. (l) Related Information POPS Fireworks Display on the waters
(i) For airplanes previous affected by AD For more information about this AD, of San Diego Bay, CA on specific
2008–15–06: Initially inspect within the next contact Gary Park, Aerospace Engineer, evenings from July 1, 2016 to September
12 months after September 2, 2008 (the Wichita ACO, 1801 Airport Road, Room 100, 4, 2016. This safety zone is necessary to
effective date retained from AD 2008–15–06). Wichita, Kansas 67209; telephone: (316) 946– provide for the safety of the
If no cracks are found, repetitively inspect 4123; fax: (316) 946–4107, email: gary.park@ participants, spectators, official vessels
thereafter at intervals not to exceed 500 hours faa.gov
time-in-service (TIS) until all four of the
of the events, and general users of the
original engine mounting brackets are (m) Material Incorporated by Reference waterway. Our regulation for the
replaced. (1) The Director of the Federal Register southern California annual fireworks for
(ii) For the new airplane affected by this approved the incorporation by reference the San Diego Captain of the Port Zone
AD: Initially inspect within the next 12 (IBR) of the service information listed in this identifies the regulated area for the
months after August 11, 2016 (the effective paragraph under 5 U.S.C. 552(a) and 1 CFR events. During the enforcement period,
date of this AD). If no cracks are found, part 51. no spectators shall anchor, block, loiter
repetitively inspect thereafter at intervals not (2) You must use this service information in, or impede the transit of official
to exceed 500 hours TIS until all four of the as applicable to do the actions required by patrol vessels in the regulated area
original engine mounting brackets are this AD, unless the AD specifies otherwise.
replaced. (3) The following service information was
without the approval of the Captain of
approved for IBR on September 2, 2008 (73 the Port, or designated representative.
(h) Engine Mounting Bracket Replacement FR 43845, July 29, 2008). DATES: The regulations in 33 CFR
If cracks are found in any of the engine (i) Cessna Single Engine Service Bulletin 165.1123 will be enforced from 9:00
mounting brackets during any inspection SEB07–2, Revision 2, dated June 18, 2007. p.m. through 10:00 p.m. on July 1
required in paragraph (g)(3) of this AD, (ii) Reserved. through July 3, July 8 and July 9, July
including all subparagraphs, before further (4) For Cessna Aircraft Company service 15 and July 16, July 29 and July 30,
flight after the inspection in which cracks are information identified in this AD, contact
found, replace the cracked engine mounting Cessna Aircraft Company, Product Support, August 5 and August 6, August 12 and
bracket(s) following Cessna Single Engine P.O. Box 7706, Wichita, Kansas 67277; August 13, August 20, August 26 and
Service Bulletin SEB07–2, Revision 2, dated telephone: (316) 517–5800; fax: (316) 942– August 27 and September 1 through
June 18, 2007. Replacing the cracked engine 9006; Internet: www.cessna.txtav.com. September 4, 2016 for Item 1 in Table
mounting bracket terminates the repetitive (5) You may view this service information 1 of 33 CFR 165.1123.
inspections required in paragraphs (g)(3)(i) at FAA, Small Airplane Directorate, 901 FOR FURTHER INFORMATION CONTACT: If
Lhorne on DSK30JT082PROD with RULES

and (ii) of this AD only for the replaced Locust, Kansas City, Missouri 64106. For you have questions on this publication,
engine mounting bracket. information on the availability of this
material at the FAA, call (816) 329–4148. In call or email Petty Officer Randolph
(i) Terminating Action addition, you can access this service Pahilanga, Waterways Management,
To terminate the repetitive inspections information on the Internet at http:// U.S. Coast Guard Sector San Diego, CA;
required in paragraphs (g)(3)(i) and (ii) of this www.regulations.gov by searching for and telephone 619–278–7656, email
AD, you may replace all four original engine locating Docket No. FAA–2016–5579. D11MarineEventsSD@uscg.mil.

VerDate Sep<11>2014 13:01 Jul 06, 2016 Jkt 238001 PO 00000 Frm 00003 Fmt 4700 Sfmt 4700 E:\FR\FM\07JYR1.SGM 07JYR1

Document Created: 2018-02-08 07:54:47
Document Modified: 2018-02-08 07:54:47

Category		Regulatory Information
Collection		Federal Register
sudoc Class		AE 2.7: GS 4.107: AE 2.106:
Publisher		Office of the Federal Register, National Archives and Records Administration
Section		Rules and Regulations
Action		Final rule.
Dates		This AD is effective August 11, 2016.
Contact		Gary Park, Aerospace Engineer, Wichita Aircraft Certification Office, 1801 Airport Road, Room 100, Wichita, Kansas 67209; telephone: (316) 946-4123; fax: (316) 946-4107, email: [email protected]
FR Citation		81 FR 44207
RIN Number		2120-AA64
CFR Associated		Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety

81 FR 44207 - Airworthiness Directives; Textron Aviation Inc. Airplanes

DEPARTMENT OF TRANSPORTATIONFederal Aviation Administration

Federal Register Volume 81, Issue 130 (July 7, 2016)

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration