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Published 2012-03-05 · Federal Register document 2012-4604

Airworthiness Directives; Robinson Helicopter Company Helicopters

Publication summary

The FAA is correcting an airworthiness directive (AD) that was published in the Federal Register. That AD applies to Robinson Helicopter Company (Robinson) Model R22, R22 Alpha, R22 Beta, R22 Mariner, R44, and R44 II helicopters. The paragraph reference in paragraph (b) of the Compliance section is incorrect. Paragraph (b) references paragraph (d), when it should reference paragraph (c). This document corrects that error. Additionally, the word "inspection" has been added in paragraph (b) for clarification. 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[63]
Raw source SHA-256
08bffa249ae9a2053bbfc0d74663d089914e83fb91f9bc4c8409ea28239f6875

Correction notice · separate source edition

Recorded publication clauses

AD identifier printed in this edition
2011-12-10
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Find all recorded historical references to AD 2011-12-10 · 0 printed reference observations in this pinned collection.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: 314c18932f6d945496567272cf396d26bfa80a11c9d663c2e056a9a049df9f2d. Source manifest: 63b09f71c35a238edf34935d264a1c3f5b9d271e9617dbe5ef007acc8d2f8d75.

Official source · 2012-03-05

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 43 (Monday, March 5, 2012)]
[Rules and Regulations]
[Pages 12991-12992]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2012-4604]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2011-0588; Directorate Identifier 2010-SW-074-AD; 
Amendment 39-16717; AD 2011-12-10]
RIN 2120-AA64


Airworthiness Directives; Robinson Helicopter Company Helicopters

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; 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 Robinson 
Helicopter Company (Robinson) Model R22, R22 Alpha, R22 Beta, R22 
Mariner, R44, and R44 II helicopters. The paragraph reference in 
paragraph (b) of the Compliance section is incorrect. Paragraph (b) 
references paragraph (d), when it should reference paragraph (c). This 
document corrects that error. Additionally, the word ``inspection'' has 
been added in paragraph (b) for clarification. In all other respects, 
the original document remains the same.

DATES: The effective date of this final rule is March 5, 2012. The 
effective date for AD 2011-12-10 remains July 5, 2011.
    Examining the AD Docket: 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: Eric D. Schrieber, Aerospace Engineer, 
Los Angeles Aircraft Certification Office, Transport Airplane 
Directorate, FAA, 3960 Paramount Blvd., Lakewood, CA 90712; telephone 
(562) 627-5348; email [email protected] (regarding Model R22 
helicopters); or Fred Guerin, Aerospace Engineer, Los Angeles Aircraft 
Certification Office, Transport Airplane Directorate, FAA, 3960 
Paramount Blvd., Lakewood, CA 90712; telephone (562) 627-5232; email 
[email protected] (regarding Model R44 helicopters).

SUPPLEMENTARY INFORMATION: Airworthiness Directive 2011-12-10, 
Amendment 39-16717 (76 FR 35330, June 17, 2011), currently includes the 
following paragraph (b) in the compliance section:
    ``(b) If you find any bare metal in the area of the skin-to-spar 
bond line, before further flight, inspect the blade by following the 
requirements of paragraph (d) of this AD.''
    As published, the reference to paragraph (d) is incorrect. The 
correct reference is to paragraph (c). Paragraph (c) contains the 
inspection requirements, and the incorrect

[[Page 12992]]

reference to paragraph (d) is confusing. We have also added the word 
``inspection'' to clarify that the requirements we are referring to are 
the inspection requirements, not the compliance times.
    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]

0
In the Federal Register of June 17, 2011, on page 35333 in the second 
column, paragraph (b) of AD 2011-12-10 is corrected to read as follows:
* * * * *
    (b) If you find any bare metal in the area of the skin-to-spar bond 
line, before further flight, inspect the blade by following the 
inspection requirements of paragraph (c) of this AD.
* * * * *

    Issued in Fort Worth, Texas, on January 3, 2012.
Lance T. Gant,
Acting Manager, Rotorcraft Directorate, Aircraft Certification Service.
[FR Doc. 2012-4604 Filed 3-2-12; 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 2026-10-09T03:04:15.946297+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.

Open the captured official edition

Source SHA-256
8891294303807adafd036413bc190fe85e14054f0664066c4da19c044849951b
Text SHA-256
314c18932f6d945496567272cf396d26bfa80a11c9d663c2e056a9a049df9f2d

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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.