AD 2011-18-07
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| engine | Wytwornia Sprzetu Komunikacyjnego | PZL-10W | Airworthiness Directives; WYTWORNIA SPRZETU KOMUNIKACYJNEGO (WSK) "PZL-RZESZOW''--SPOLKA AKCYJNA (SA) PZL--10W Turboshaft Engines |
Unsafe Condition
Excessive wear on spline teeth of the fuel metering pump shaft.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect spline teeth on the fuel metering pump shaft for excessive wear.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 50 flight hours after the effective date.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
WSK PZL-10W series turboshaft engines.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
The FAA is correcting an airworthiness directive (AD) that published in the Federal Register. That AD applies to the products listed above. The effective date in paragraph (a) of the Amended section of the AD is incorrect. This document corrects that error. In all other respects, the original document remains the same.
Document Text
Show stored source text (verify against official source)
[Federal Register Volume 76, Number 200 (Monday, October 17, 2011)]
[Rules and Regulations]
[Page 64003]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2011-26274]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2011-0760; Directorate Identifier 2011-NE-10-AD;
Amendment 39-16789; AD 2011-18-07]
RIN 2120-AA64
Airworthiness Directives; WYTWORNIA SPRZETU KOMUNIKACYJNEGO (WSK)
``PZL-RZESZOW''--SPOLKA AKCYJNA (SA) PZL-10W Turboshaft Engines
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; correction.
-----------------------------------------------------------------------
SUMMARY: The FAA is correcting an airworthiness directive (AD) that
published in the Federal Register. That AD applies to the products
listed above. The effective date in paragraph (a) of the Amended
section of the AD is incorrect. This document corrects that error. In
all other respects, the original document remains the same.
DATES: This final rule is effective October 17, 2011. The effective
date of AD 2011-18-07 remains October 4, 2011.
ADDRESSES: You may examine the AD docket on the Internet at <a href="http://www.regulations.gov">http://www.regulations.gov</a>; 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: James Lawrence, Aerospace Engineer,
Engine Certification Office, FAA, Engine & Propeller Directorate, 12
New England Executive Park, Burlington, MA 01803; e-mail:
<a href="/cdn-cgi/l/email-protection#d4beb5b9b1a7fab8b5a3a6b1bab7b194b2b5b5fab3bba2"><span class="__cf_email__" data-cfemail="701a111d15035e1c110702151e1315301611115e171f06">[email protected]</span></a>; phone: 781-238-7176; fax: 781-238-7199.
SUPPLEMENTARY INFORMATION: Airworthiness Directive 2011-18-07,
Amendment 39-16789 (76 FR 57900, September 19, 2011), currently
requires a one time inspection of spline teeth on the fuel metering
pump shaft for excessive wear, for WSK PZL-10W series turboshaft
engines.
As published, paragraph (a) of the Amended section is incorrect.
No other part of the preamble or regulatory information has been
changed; therefore, only the changed portion of the final rule is being
published in the Federal Register.
The effective date of this AD remains October 4, 2011.
Correction of Regulatory Text
Sec. 39.13 [Corrected]
0
In the Federal Register of September 19, 2011, on page 57901, in the
third column, paragraph (a) of AD 2011-18-07 is corrected to read as
follows:
(a) This airworthiness directive (AD) becomes effective October
4, 2011.
Issued in Burlington, Massachusetts, on October 4, 2011.
Peter A. White,
Manager, Engine and Propeller Directorate, Aircraft Certification
Service.
[FR Doc. 2011-26274 Filed 10-14-11; 8:45 am]
BILLING CODE 4910-13-P
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.