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2013-15-04 HARTZELL PROPELLER, INC.:
Amendment 39-17520; Docket No. FAA-2013-0130; Directorate Identifier 2013-NE-07-AD.

(a) EFFECTIVE DATE

    This AD is effective August 30, 2013.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This  AD  applies  to Hartzell  Propeller,  Inc.  propeller models  HC
    -(1,D)2(X,V,MV)20-7, HC-(1,D)2(X,V,MV)20-8, and  HC-(1,D)3(X,V,MV)20-8
    with a propeller hydraulic bladder diaphragm, part number (P/N)  B-119
    -2, without tab, installed.

(d) UNSAFE CONDITION

    This AD was  prompted by failures  of the propeller  hydraulic bladder
    diaphragm and  resulting engine  oil leak.  We are  issuing this AD to
    prevent propeller hydraulic bladder diaphragm rupture, loss of  engine
    oil, damage to the engine, and loss of the airplane.

(e) COMPLIANCE

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

(f) BLADDER DIAPHRAGM REPLACEMENT

(1) Within 12 months after  the  effective  date of this AD,  remove  from
    service the propeller hydraulic bladder diaphragm,  P/N B-119-2, with-
    out tab.

(2) Install  a  redesigned  propeller  hydraulic  bladder  diaphragm,  P/N
    B-119-2, with tab. The  bladder diaphragm, eligible for  installation,
    is identified by  a tab with  a batch/lot number.  The tab is  visible
    after  installation  and  confirms  the  installation  of  the  proper
    redesigned propeller  hydraulic bladder  diaphragm,  P/N B-119-2, with
    tab, in the Hartzell propeller assembly.

(g) INSTALLATION PROHIBITION

    After the effective date  of this AD, do  not install into any  engine
    any hydraulic bladder diaphragm, P/N B-119-2, that is without tab.

(h) ALTERNATIVE METHODS OF COMPLIANCE (AMOCS)

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

(i) RELATED INFORMATION

(1) For  more  information about this AD,  contact  Mark Grace,  Aerospace
    Engineer,  Chicago  Aircraft  Certification  Office,  FAA,  Propulsion
    Branch, 2300  E. Devon  Avenue, Des  Planes, IL  60018; phone: 847-294
    -7377; fax: 847-294-7834; email: mark.grace@faa.gov.

(2) Refer to Hartzell Alert Service Bulletin No. HC-ASB-61-338 for related
    information.

(3) For  service  information  identified  in  this  AD,  contact Hartzell
    Propeller Inc., 1 Propeller Place,  Piqua, OH 45356-2634;  phone:  937
    -778-4379; fax: 937-778-4391; email: techsupport@hartzellprop.com. You
    may view this service information at the FAA, 12 New England Executive
    Park,  Burlington, MA.  For information  on the  availability of  this
    material at the FAA, call 781-238-7125.

(j) MATERIAL INCORPORATED BY REFERENCE

    None.

Issued  in  Burlington,  Massachusetts,  on  July  16,  2013.  Colleen  M.
D’Alessandro, Assistant Manager, Engine & Propeller Directorate,  Aircraft
Certification Service.

FOR FURTHER INFORMATION CONTACT: Mark Grace,  Aerospace Engineer,  Chicago
Aircraft  Certification  Office,  FAA,  Propulsion  Branch,  2300 E. Devon
Avenue,  Des Planes, IL 60018;  phone:  847-294-7377;  fax:  847-294-7834;
email: mark.grace@faa.gov.
PREAMBLE 

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

SUMMARY: We are adopting a new airworthiness directive (AD) for certain
Hartzell Propeller, Inc. propeller models HC-(1,D)2(X,V,MV)20-7, HC-
(1,D)2(X,V,MV)20-8, and HC-(1,D)3(X,V,MV)20-8. This AD was prompted by
failures of the propeller hydraulic bladder diaphragm and resulting
engine oil leak. This AD requires replacement of the propeller
hydraulic bladder diaphragm. We are issuing this AD to prevent
propeller hydraulic bladder diaphragm rupture, loss of engine oil,
damage to the engine, and loss of the airplane.

DATES: This AD is effective August 30, 2013.

ADDRESSES: For service information identified in this AD, contact
Hartzell Propeller, Inc., 1 Propeller Place, Piqua, OH 45356; phone:
937-778-4397; fax: 937-778-4391; email: techsupport@hartzellprop.com.
You may view this service information at the FAA, 12 New England
Executive Park, Burlington, MA. For information on the availability of
this material at the FAA, call 781-238-7125.
The Docket Operations office is located at Docket 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.

Examining the AD Docket

You may examine the AD docket on the Internet at http://www.regulations.
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 AD, the regulatory evaluation,
any comments received, and other information. The address for the
Docket Office (phone: 800-647-5527) provided in the ADDRESSES section.
Comments will be available in the AD docket shortly after receipt.

FOR FURTHER INFORMATION CONTACT: Mark Grace, Aerospace Engineer,
Chicago Aircraft Certification Office, FAA, Propulsion Branch, 2300 E.
Devon Avenue, Des Planes, IL 60018; phone: 847-294-7377; fax: 847-294-
7834; email: mark.grace@faa.gov.

SUPPLEMENTARY INFORMATION:

Discussion

We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 to include an AD that would apply to the specified products.
The NPRM published in the Federal Register on March 26, 2013 (78 FR
18255). The NPRM proposed to require replacement of the propeller
hydraulic bladder diaphragm with a redesigned bladder diaphragm that
includes a tab, visible after installation, which contains the bladder
diaphragm batch/lot number.

Comments

We gave the public the opportunity to participate in developing
this AD. We have considered the comment received. Hartzell Propeller,
Inc. supports the NPRM (78 FR 18255, dated March 26, 2013).

Conclusion

We reviewed the relevant data, considered the comments received,
and determined that air safety and the public interest require adopting
this AD as proposed.

Costs of Compliance

We estimate that this AD will affect about 400 propellers installed
on airplanes of U.S. registry. We also estimate that it will take about
4 hours per propeller to replace the bladder diaphragm. The average
labor rate is $85 per hour. We estimate parts costs at $53 per engine.
Based on these figures, we estimate the cost of this AD on U.S.
operators to be $157,200. 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):