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2015-10-06 LYCOMING ENGINES (TYPE CERTIFICATE PREVIOUSLY HELD BY TEXTRON LYCOMING DIVISION, AVCO CORPORATION):
Amendment 39-18162; Docket No. FAA-2014-0940; Directorate Identifier 2014-NE-15-AD.

(a) EFFECTIVE DATE

    This AD is effective July 2, 2015.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This AD  applies to  all Lycoming  TIO-540-AJ1A reciprocating  engines
    listed by engine serial number (S/N)  in Figure 1 to paragraph (c)  of
    this AD  and  to any TIO-540-AJ1A reciprocating engine with a replace-
    ment turbocharger mounting bracket installed  that  was  purchased be-
    tween April 5, 2012 and May 29, 2014.
__________________________________________________________________________
      FIGURE 1 TO PARAGRAPH (C) - LYCOMING TIO-540-AJ1A ENGINE S/NS
__________________________________________________________________________
 L-6748-61E          L-13828-61E         L-13832-61E           L-13843-61E
L-13817-61E          L-13831-61E         L-13833-61E           L-13847-61E
L-13819-61E          L-13823-61E         L-13839-61E           L-13855-61E
L-13856-61E          L-13947-61E         L-14011-61E           RL-2551-61E
L-13857-61E          L-13948-61E         L-14013-61E           RL-2848-61E
L-13866-61E          L-13949-61E         L-14014-61E           RL-3450-61E
L-13867-61E          L-13950-61E         L-14015-61E           RL-4138-61E
L-13873-61E          L-13960-61E         L-14017-61E           RL-7243-61E
L-13882-61E          L-13961-61E         L-14024-61E           RL-7512-61E
L-13883-61E          L-13962-61E         L-14025-61E           RL-8435-61E
L-13884-61E          L-13967-61E         L-14026-61E           RL-8767-61E
L-13885-61E          L-13973-61E         L-14028-61E           RL-8914-61E
L-13886-61E          L-13975-61E         L-14034-61E           RL-8979-61E
L-13895-61E          L-13976-61E         L-14054-61E           RL-9399-61E
L-13896-61E          L-13979-61E         L-14055-61E           RL-9466-61E
L-13898-61E          L-13981-61E         L-14056-61E           RL-9618-61E
L-13900-61E          L-13983-61E         L-14057-61E           RL-9663-61E
L-13902-61E          L-13984-61E         L-14062-61E          RL-10098-61E
L-13907-61E          L-13993-61E         L-14063-61E          RL-10194-61E
L-13913-61E          L-13996-61E         L-14066-61E          RL-10249-61E
L-13915-61E          L-13997-61E         L-14067-61E          RL-10615-61E
L-13930-61E          L-13998-61E         L-14069-61E          RL-11011-61E
L-13931-61E          L-13999-61E         L-14071-61E          RL-12121-61E
L-13934-61E          L-14000-61E         L-14076-61E          RL-12163-61E
L-13936-61E          L-14001-61E         L-14077-61E          RL-12343-61E
L-13938-61E          L-14003-61E         RL-1726-61E          RL-13352-61E
L-13939-61E          L-14004-61E         RL-1810-61E          RL-13601-61E
L-13946-61E          L-14005-61E         RL-1862-61E
__________________________________________________________________________

(d) UNSAFE CONDITION

    This AD  was prompted  by several  reports of  cracked engine  exhaust
    pipes. We are issuing this AD to prevent failure of the exhaust system
    due to cracking, which could lead to uncontrolled engine fire, harmful
    exhaust gases entering the cabin resulting in crew incapacitation, and
    damage to the airplane.

(e) COMPLIANCE

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

(1) For affected engines with an  S/N listed in  Figure 1 to paragraph (c)
    of this AD with 400 hours or  less time since new (TSN) or time  since
    last overhaul  (TSLO), and  for any  TIO-540-AJ1A reciprocating engine
    with a  replacement turbocharger  mounting bracket  installed that was
    purchased between April 5, 2012 and May 29, 2014, that has accumulated
    400 hours  or less  time-in-service (TIS),  within 25  hours after the
    effective date of this  AD, replace the turbocharger  mounting bracket
    with a part eligible for  installation, and inspect the exhaust  pipes
    for cracks. Use Lycoming Engines Mandatory Service Bulletin (MSB)  No.
    614A, dated October 10, 2014, Exhaust System Disassembly and  Removal,
    paragraphs 1  through 22  to replace  the bracket,  and Exhaust System
    Inspection, paragraphs 1 through 5 to do the inspection.

(2) For affected engines with  an S/N listed in  Figure 1 to paragraph (c)
    of this AD with more than 400  hours TSN or TSLO, and for any  TIO-540
    -AJ1A reciprocating  engine with  a replacement  turbocharger mounting
    bracket installed that was purchased between April 5, 2012 and May 29,
    2014,  that  has accumulated  more  than 400  hours  TIS, replace  the
    turbocharger mounting bracket with  a part eligible for  installation,
    and inspect the exhaust pipes for cracks at the next engine  overhaul,
    separation of the crankcase halves, or twelve years from the effective
    date of this AD, whichever  comes first. Use Lycoming Engines  MSB No.
    614A, dated October 10, 2014, Exhaust System Disassembly and  Removal,
    paragraphs 1  through 22  to replace  the bracket,  and Exhaust System
    Inspection, paragraphs 1 through 5 to do the inspection.

(f) INSTALLATION PROHIBITION

    After the effective date of this AD, do not return to service any  TIO
    -540-AJ1A engine with a turbocharger mounting bracket that was removed
    from an engine identified in Figure 1 to paragraph (c) of this  AD  or
    that was purchased between April 5, 2012 and May 29, 2014.

(g) CREDIT FOR PREVIOUS ACTION

(1) If,  before the effective date of this AD,  you  replaced  the  turbo-
    charger mounting bracket  with one eligible  for installation you  may
    take credit for your prior corrective action.  No further turbocharger
    mounting bracket replacement is required.

(2) If, before the effective date of this AD,  you performed the crack in-
    spection using either of the following:

(i) Lycoming Engines MSB No. 614A,  dated October 10, 2014, Exhaust System
    Inspection, paragraphs 1 through 5, or

(ii) Cessna Service Letter No. SEL-78-01, dated May 30, 2014, you may take
     credit for your prior corrective action. No further inspection is re-
     quired.  However,  you must still replace  the  turbocharger mounting
     bracket.

(h) ALTERNATIVE METHODS OF COMPLIANCE (AMOCS)

    The Manager, New York Aircraft Certification Office, FAA,  may approve
    AMOCs to this  AD. Use the  procedures found in  14 CFR 39.19  to make
    your request.

(i) RELATED INFORMATION

    For more information about this AD,  contact Norm Perenson,  Aerospace
    Engineer,  New  York  Aircraft  Certification  Office,  FAA,  Engine &
    Propeller Directorate,  1600 Stewart Avenue,  Suite 410,  Westbury, NY
    11590; phone: 516-228-7337; fax: 516-794-5531; email: norman.perenson@
    faa.gov.

(j) 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.

(i) Lycoming Engines Mandatory Service Bulletin No. 614A dated October 10,
    2014.

(ii) Reserved.

(3) For  Lycoming Engines service information identified in this AD,  con-
    tact  Lycoming Engines,  652 Oliver Street,  Williamsport,  PA  17701;
    phone: 800-258-3279;  fax: 570-327-7101;  Internet:  www.lycoming.com/
    Lycoming/SUPPORT/TechnicalPublications/ServiceBulletins.aspx.

(4) You  may  view  this  service  information  at FAA, Engine & Propeller
    Directorate, 12 New England Executive Park, Burlington, MA. For infor-
    mation on the availability of this material at the FAA,  call 781-238-
    7125.

(5) 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  Burlington,  Massachusetts,  on  May  12,  2015.  Colleen   M.
D'Alessandro,   Assistant   Directorate   Manager,   Engine   &  Propeller
Directorate, Aircraft Certification Service.

FOR FURTHER INFORMATION CONTACT: Norm Perenson,  Aerospace  Engineer,  New
York Aircraft Certification Office,  FAA,  Engine & Propeller Directorate,
1600 Stewart Avenue, Suite 410, Westbury, NY 11590;  phone:  516-228-7337;
fax: 516-794-5531; email: norman.perenson@faa.gov.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2014-0940; Directorate Identifier 2014-NE-15-AD;
Amendment 39-18162; AD 2015-10-06]
RIN 2120-AA64

Airworthiness Directives; Lycoming Engines Reciprocating Engines
(Type Certificate Previously Held by Textron Lycoming Division, AVCO
Corporation)

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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

SUMMARY: We are adopting a new airworthiness directive (AD) for certain
Lycoming TIO-540-AJ1A reciprocating engines. This AD was prompted by
several reports of cracked engine exhaust pipes. This AD requires
inspection of the engine exhaust pipes for cracks and replacement of
the turbocharger mounting bracket. We are issuing this AD to prevent
failure of the exhaust system due to cracking, which could lead to
uncontrolled engine fire, harmful exhaust gases entering the cabin
resulting in crew incapacitation, and damage to the airplane.

DATES: This AD is effective July 2, 2015.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of July 2,
2015.

ADDRESSES: For service information identified in this AD, contact
Lycoming Engines, 652 Oliver Street, Williamsport, PA 17701; phone:
800-258-3279; fax: 570-327-7101; Internet: www.lycoming.com/Lycoming/SUPPORT/TechnicalPublications/ServiceBulletins.aspx.
You may view this service information at the FAA, Engine & Propeller Directorate,
12 New England Executive Park, Burlington, MA. For information on the
availability of this material at the FAA, call 781-238-7125. It is also
available on the Internet at http://www.regulations.gov by searching
for and locating Docket No. FAA-2014-0940.

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-2014-
0940; 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: Norm Perenson, Aerospace Engineer, New
York Aircraft Certification Office, FAA, Engine & Propeller
Directorate, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone:
516-228-7337; fax: 516-794-5531; email: norman.perenson@faa.gov.

SUPPLEMENTARY INFORMATION:

Discussion

We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would apply to certain Lycoming TIO-540-
AJ1A reciprocating engines. The NPRM published in the Federal Register
on February 2, 2015 (80 FR 5489). The NPRM was prompted by several
reports of cracked engine exhaust pipes. The NPRM proposed to require
inspection of the engine exhaust pipes for cracks and replacement of
the turbocharger mounting bracket. We are issuing this AD to prevent
failure of the exhaust system due to cracking, which could lead to
uncontrolled engine fire, harmful exhaust gases entering the cabin
resulting in crew incapacitation, and damage to the airplane.

Related Service Information Under CFR Part 51

We reviewed Lycoming Engines Mandatory Service Bulletin No. 614A,
dated October 10, 2014. This service bulletin describes procedures for
exhaust system inspection and turbocharger mounting bracket
replacement. It also provides for the return of the turbocharger
mounting bracket to Lycoming. 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 of this AD.

Comments

We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM (80 FR 5489, February 2,
2015) 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.

Costs of Compliance

We estimate that this AD affects about 111 engines installed on
airplanes of U.S. registry. We also estimate that it will take about 8
hours per engine to comply with this AD. The average labor rate is $85
per hour. Parts replacement will cost about $6,782 per engine. Based on
these figures, we estimate the cost of this AD on U.S. operators to be
$828,282. Our cost estimate is exclusive of possible warranty coverage.

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

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 to the extent
that it justifies making a regulatory distinction, 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


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 airworthiness
directive (AD):