Published 2013-07-26 · Federal Register document 2013-17664
Airworthiness Directives; Hartzell Propeller, Inc. Propellers
Publication 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.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:42.577882+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2013-a7b684f4a1b4614e
- Source row
- results[226]
- Raw source SHA-256
- a7b684f4a1b4614eef5ec9064d04a70a4701b45b0acd50058e29f235c625e705
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2013-15-04
- Effective date printed in this edition
- 2013-08-30
Read 10 complete recorded clauses
Effective Date
(a) Effective Date
This AD is effective August 30, 2013.
Exact source excerpt. Text positions 6405–6468, end exclusive, in the original decoded publication. SHA-256: 0af614bccd5cc029348ce3980d78c08e54db458caa9bde6f45ba750be98c0dd8
Affected ADs
(b) Affected ADs
None.
Exact source excerpt. Text positions 6468–6497, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0
Applicability wording · Applicability
(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.
Exact source excerpt. Text positions 6497–6754, end exclusive, in the original decoded publication. SHA-256: a5374a285a7c26c90705d7ecde75adbc33d17e5fe0d6dbfa04e147adc33b2ad7
Unsafe Condition
(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.
Exact source excerpt. Text positions 6754–7042, end exclusive, in the original decoded publication. SHA-256: 4d92f150b5189c07882ef9d9a1fe00b883f75da52870778a58420e5809e108b6
Compliance
(e) Compliance
Comply with this AD within the compliance times specified,
unless already done.
Exact source excerpt. Text positions 7042–7144, end exclusive, in the original decoded publication. SHA-256: aa44d65fd8ee8f86413a5efd4e9ceea623e114f021d6b2ff9bddc2320bbbab7d
Bladder Diaphragm Replacement
(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,
without 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.
Exact source excerpt. Text positions 7144–7718, end exclusive, in the original decoded publication. SHA-256: 431738d3c33e4b7935f90d25ce3da193a2707377dae06bc1cdafe62ddda5e8c5
Installation Prohibition
(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.
Exact source excerpt. Text positions 7718–7890, end exclusive, in the original decoded publication. SHA-256: a51cba7c0623c343fef4d25f3816e1788ab49f7b4e72d9234ec684ce55b18834
Alternative Methods of Compliance (AMOCs)
(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.
Exact source excerpt. Text positions 7890–8095, end exclusive, in the original decoded publication. SHA-256: 84bcb60be6a729842149ea98c656907a59f5eb73fbff5f8882c8591b1c3376f0
Related Information
(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: [email protected].
(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:
[email protected]. 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.
Exact source excerpt. Text positions 8095–8856, end exclusive, in the original decoded publication. SHA-256: ff5b205fcb0d83a01cade2b0166f273f0b168ddf387924d160d336d35dba3cbc
Material Incorporated by Reference
(j) Material Incorporated by Reference
None.
Exact source excerpt. Text positions 8856–8907, end exclusive, in the original decoded publication. SHA-256: 9d583edbcf085b1fae94c8be8274ba3ce59b91db7bf15c5f5fd81fff2816eec7
No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.
Find all recorded historical references to AD 2013-15-04 · 0 printed reference observations in this pinned collection.
These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.
Why these observations are shown
They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.
Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: 52445f1e39457f6e945b167640cc99a85b562f4b4e2e8088360e763a875b9f89. Source manifest: cf8a28195ba2c6b774ec289c44b7539bc7f3f95d77f791483563d3a2b24eaabc.
Official source · 2013-07-26
Publication text
This is the complete recorded text of this dated publication.
Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.
Read the complete official publication text
[Federal Register Volume 78, Number 144 (Friday, July 26, 2013)]
[Rules and Regulations]
[Pages 45052-45053]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2013-17664]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2013-0130; Directorate Identifier 2013-NE-07-AD;
Amendment 39-17520; AD 2013-15-04]
RIN 2120-AA64
Airworthiness Directives; Hartzell Propeller, Inc. Propellers
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: [email protected].
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,
[[Page 45053]]
Chicago Aircraft Certification Office, FAA, Propulsion Branch, 2300 E.
Devon Avenue, Des Planes, IL 60018; phone: 847-294-7377; fax: 847-294-
7834; email: [email protected].
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
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 adding the following new airworthiness
directive (AD):
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,
without 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: [email protected].
(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:
[email protected]. 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.
[FR Doc. 2013-17664 Filed 7-25-13; 8:45 am]
BILLING CODE 4910-13-P
Why this text is shown
The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T02:54:01.939434+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.
Open the captured official edition
- Source SHA-256
- 6cfaf8c79511e3d7011088b33eb03694563820d8dee110087efb57113bbcbfd5
- Text SHA-256
- 52445f1e39457f6e945b167640cc99a85b562f4b4e2e8088360e763a875b9f89
Return to the full metadata catalog · Search complete publication text · Explore retained publication text and evidence
Coverage and limits
These are dated publication metadata, recorded clauses and literal source observations. Word, model-label, header and reference matches do not establish current legal effect, manufacturer/model identity, aircraft applicability, installed configuration or compliance.
The collection uses 33 explicit annual source snapshots. Source captures and operative-text qualifications have separate states. Missing information remains unknown.