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Published 2012-08-17 · Federal Register document 2012-20177

Airworthiness Directives; Eurocopter Deutschland GmbH Helicopters

Publication summary

The FAA is correcting an airworthiness directive (AD) that was published in the Federal Register. That AD applies to Eurocopter Deutschland GmbH Model MBB-BK 117 C-2 helicopters. A page reference of the rotorcraft flight manual in the Required Actions section, paragraph (e)(1)(i), is incorrect. This document corrects that error. 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[264]
Raw source SHA-256
08bffa249ae9a2053bbfc0d74663d089914e83fb91f9bc4c8409ea28239f6875

Correction notice · separate source edition

Recorded publication clauses

AD identifier printed in this edition
2012-12-21
Effective date printed in this edition
Unknown

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

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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Find all recorded historical references to AD 2012-12-21 · 0 printed reference observations in this pinned collection.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: c18e93352d04d16eac6251da821f4dc0a35c249210d5f05e79c021e4d6d67185. Source manifest: 5f5caf9305d8678c69c93d88e99a76095a0714ad16e659b737cb9eeb54100095.

Official source · 2012-08-17

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 160 (Friday, August 17, 2012)]
[Rules and Regulations]
[Page 49705]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2012-20177]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2012-0659; Directorate Identifier 2011-SW-061-AD; 
Amendment 39-17101; AD 2012-12-21]
RIN 2120-AA64


Airworthiness Directives; Eurocopter Deutschland GmbH Helicopters

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; request for comments; correction.

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SUMMARY: The FAA is correcting an airworthiness directive (AD) that was 
published in the Federal Register. That AD applies to Eurocopter 
Deutschland GmbH Model MBB-BK 117 C-2 helicopters. A page reference of 
the rotorcraft flight manual in the Required Actions section, paragraph 
(e)(1)(i), is incorrect. This document corrects that error. In all 
other respects, the original document remains the same.

DATES: This correction is effective August 17, 2012. The effective date 
for AD 2012-12-21 remains July 10, 2012. The last date for submitting 
comments to the final rule; request for comments remains August 24, 
2012.

ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov; or in person at the Docket Operations Office 
between 9 a.m. and 5 p.m., Monday through Friday, except Federal 
holidays. The AD docket contains this AD, any incorporated-by-reference 
service information, the economic evaluation, any comments received, 
and other information. The street address for the Docket Operations 
Office (phone: 800-647-5527) is U.S. Department of Transportation, 
Docket Operations Office, M-30, West Building Ground Floor, Room W12-
140, 1200 New Jersey Avenue SE., Washington, DC 20590.

FOR FURTHER INFORMATION CONTACT: George Schwab, Aviation Safety 
Engineer, FAA, Rotorcraft Directorate, Safety Management Group, 2601 
Meacham Blvd., Fort Worth, TX 76137, telephone (817) 222-5110, email: 
[email protected].

SUPPLEMENTARY INFORMATION: Airworthiness Directive 2012-12-21, 
Amendment 39-17101 (77 FR 37777, June 25, 2012), currently includes the 
following paragraph (e)(1)(i) in the Required Actions section:
    ``(i) ``Emergency and Malfunction Procedures'': pages 3-3 and 3-4, 
and''
    As published, the reference to page 3-4 is incorrect. The correct 
reference is to page 3-3a.
    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.

Correction of Regulatory Text


Sec.  39.13  [Corrected]

    In the Federal Register of June 25, 2012, on page 37779 in the 
second column, paragraph (e)(1)(i) of AD 2012-12-21 is corrected to 
read as follows:
* * * * *
    (i) ``Emergency and Malfunction Procedures'': pages 3-3 and 3-3a, 
and
* * * * *

    Issued in Fort Worth, Texas, on August 9, 2012.
Kim Smith,
Manager, Rotorcraft Directorate, Aircraft Certification Service.
[FR Doc. 2012-20177 Filed 8-16-12; 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 2026-10-09T03:00:36.446952+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

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Source SHA-256
5ad5c4585f68524ad8d75eb6ce80eed04740afbfdf9cbfa449c2d43c4d1ca36c
Text SHA-256
c18e93352d04d16eac6251da821f4dc0a35c249210d5f05e79c021e4d6d67185

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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.

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