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Published 2012-11-06 · Federal Register document 2012-26772

Airworthiness Directives; BRP-Powertrain GmbH & Co KG Rotax Reciprocating Engines

Publication summary

The FAA is correcting an airworthiness directive (AD) that was published in the Federal Register. That AD applies to BRP-Powertrain GmbH & Co KG Rotax 912 F2; 912 F3; 912 F4; 912 S2; 912 S3; and 912 S4 reciprocating engines. The word "not" was improperly omitted from the Installation Prohibition section of the AD, thereby changing the prohibition in the AD. This correction reinserts "not" into the paragraph to correct the omission. In all other respects, the original document remains the same.

Why this record is shown

Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:39.502075+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2012-08bffa249ae9a205
Source row
results[348]
Raw source SHA-256
08bffa249ae9a2053bbfc0d74663d089914e83fb91f9bc4c8409ea28239f6875

Correction notice · separate source edition

Recorded publication clauses

AD identifier printed in this edition
2012-16-13
Effective date printed in this edition
Unknown

This correction is a separate source edition; it is not counted as a new adopted rule.

No adopted-clause structure was recorded for this source edition. Read the complete text; no applicability conclusion has been inferred.

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Find all recorded historical references to AD 2012-16-13 · 0 printed reference observations in this pinned collection.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: 7076585aafe08e6b8b825f56a1683bdb6734adeca604e713ab962087350382a9. Source manifest: caa2cc2a21120cf1b5b740f0066c4db3efbebe556f8d11987ca61a7a31043a93.

Official source · 2012-11-06

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 77, Number 215 (Tuesday, November 6, 2012)]
[Rules and Regulations]
[Pages 66534-66535]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2012-26772]


=======================================================================
-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2012-0603; Directorate Identifier 2012-NE-17-AD; 
Amendment 39-17160; AD 2012-16-13]
RIN 2120-AA64


Airworthiness Directives; BRP-Powertrain GmbH & Co KG Rotax 
Reciprocating Engines

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; correction.

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

SUMMARY: The FAA is correcting an airworthiness directive (AD) that was 
published in the Federal Register. That AD applies to BRP-Powertrain 
GmbH & Co KG Rotax 912 F2; 912 F3; 912 F4; 912 S2; 912 S3; and 912 S4 
reciprocating engines. The word ``not'' was improperly omitted from the 
Installation Prohibition section of the AD, thereby changing the 
prohibition in the AD. This correction reinserts ``not'' into the 
paragraph to correct the omission. In all other respects, the original 
document remains the same.

DATES: This final rule is effective November 6, 2012. The effective 
date for AD 2012-16-13 (77 FR 51462, August 24, 2012) remains September 
10, 2012.

ADDRESSES: 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) 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: Alan Strom, Aerospace Engineer, Engine 
Certification Office, FAA, Engine & Propeller Directorate, 12 New 
England Executive Park, Burlington, MA 01803; email: 
[email protected]; phone: 781-238-7143; fax: 781-238-7199.

SUPPLEMENTARY INFORMATION: Airworthiness Directive 2012-16-13, 
amendment 39-17160 (77 FR 51462, August 24, 2012), currently requires 
replacing the pressure side fuel hose on certain fuel pumps and 
inspecting the carburetors connected to those fuel pumps for 
contamination within 5 flight hours after the effective date of this AD

[[Page 66535]]

for BRP-Powertrain GmbH & Co KG Rotax 912 F2; 912 F3; 912 F4; 912 S2; 
912 S3; and 912 S4 reciprocating engines.
    As published, the text of paragraph (g)(3), Installation 
Prohibition, is incorrect.
    No other part of the preamble or regulatory information is in 
error; therefore, only the changed portion of the final rule is being 
published in the Federal Register.
    The effective date of this AD remains September 10, 2012.

Correction of Regulatory Text


Sec.  39.13  [Corrected]

0
In the Federal Register of August 24, 2012, on page 51464, in the 1st 
column, paragraph (g)(3) of AD 2012-16-13 is corrected to read as 
follows:
* * * * *
    (3) After the effective date of this AD, do not approve for return 
to service any product or article with a fuel hose removed from a P/N 
893114 fuel pump with an S/N listed in Table 1 to paragraph (c) of this 
AD.
* * * * *

    Issued in Burlington, Massachusetts, on October 24, 2012.
Colleen M. D'Alessandro,
Assistant Manager, Engine & Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. 2012-26772 Filed 11-5-12; 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 2026-10-09T02:58:59.639710+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

Open the captured official edition

Source SHA-256
b51de925c06678ca62ad573c8eece43ea5820e1826c3731ae599564d79f59f21
Text SHA-256
7076585aafe08e6b8b825f56a1683bdb6734adeca604e713ab962087350382a9

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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.