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Published 2011-11-08 · Federal Register document 2011-28861

Airworthiness Directives; Cessna Aircraft Company Airplanes

Publication summary

The FAA is correcting an airworthiness directive (AD) that published in the Federal Register. That AD applies to certain Cessna Aircraft Company (Cessna) Models 150F, 150G, 150H, 150J, 150K, 150L, 150M, A150K, A150L, A150M, F150F, F150G, F150H, F150J, F150K, F150L, F150M, FA150K, FA150L, FRA150L, FA150M, FRA150M, 152, A152, F152, and FA152 airplanes. There is an error in the compliance instructions. 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 2026-09-03T22:23:36.067984+00:00. The title, summary and date are source facts.

Source revision
federal_register_ad_metadata_2011-e3661fa6ab35b428
Source row
results[318]
Raw source SHA-256
e3661fa6ab35b428e6e5ee3716d50c22e985c092328ad8ce2f0f440b962ae0cd

Correction notice · separate source edition

Recorded publication clauses

AD identifier printed in this edition
2009-10-09 R2
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Find all recorded historical references to AD 2009-10-09 R2 · 0 printed reference observations in this pinned collection.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: d465cb97ff19207e5a95a123bd867dcf88d2a488b2f52b8dab2c086ea5140c3a. Source manifest: 69175b28c0aeb314c8075f3451f9681b1c5572896711444ad2afe710b453eda8.

Official source · 2011-11-08

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 76, Number 216 (Tuesday, November 8, 2011)]
[Rules and Regulations]
[Page 69123]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2011-28861]


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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2007-27747; Directorate Identifier 2007-CE-030-AD; 
Amendment 39-16782; AD 2009-10-09 R2]
RIN 2120-AA64


Airworthiness Directives; Cessna Aircraft Company Airplanes

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 certain Cessna 
Aircraft Company (Cessna) Models 150F, 150G, 150H, 150J, 150K, 150L, 
150M, A150K, A150L, A150M, F150F, F150G, F150H, F150J, F150K, F150L, 
F150M, FA150K, FA150L, FRA150L, FA150M, FRA150M, 152, A152, F152, and 
FA152 airplanes. There is an error in the compliance instructions. This 
document corrects that error. In all other respects, the original 
document remains the same.

DATES: This final rule; correction, is effective November 8, 2011. The 
effective date for AD 2009-10-09 R2 remains September 12, 2011.

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: Ann Johnson, Aerospace Engineer, FAA, 
Wichita Aircraft Certification Office, 1801 Airport Road, Room 100, 
Wichita, Kansas 67209; phone: (316) 946-4105; fax: (316) 946-4107; 
email: [email protected].

SUPPLEMENTARY INFORMATION: Airworthiness Directive 2009-10-09 R2, 
Amendment 39-16782 (76 FR 53308, August 26, 2011), currently requires 
either installing a placard prohibiting spins and other acrobatic 
maneuvers in the airplane or replacing the rudder stop, the rudder stop 
bumper, and the attachment hardware with a new rudder stop modification 
kit for certain Cessna Models 150F, 150G, 150H, 150J, 150K, 150L, 150M, 
A150K, A150L, A150M, F150F, F150G, F150H, F150J, F150K, F150L, F150M, 
FA150K, FA150L, FRA150L, FA150M, FRA150M, 152, A152, F152, and FA152 
airplanes.
    As published, the text in the Procedures column of Table 2 in 
paragraph (g)(1) of this AD incorrectly states ``* * * fabricate the 
placard required in paragraph (g)(1)(i) of this AD * * *'', and the 
text should refer to paragraph (g)(1)(ii).
    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 September 12, 2011.

Correction of Regulatory Text


Sec.  39.13  [Corrected]

    In the Federal Register of August 26, 2011, on page 53311, in the 
3rd column, Procedures, paragraph (g)(1), Table 2--Actions, Compliance 
and Procedures, of AD 2009-10-09 R2 is corrected to read as follows:
* * * * *
    A person authorized to perform maintenance as specified in 14 
CFR 43.3 of the Federal Aviation Administration Regulations (14 CFR 
43.3) is required to make the AFM and POH changes, fabricate the 
placard required in paragraph (g)(1)(ii) of this AD, and make an 
entry into the aircraft logbook showing compliance with the portion 
of the AD per compliance with 14 CFR 43.9.
* * * * *

    Issued in Kansas City, Missouri, on November 2, 2011.
John R. Colomy,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2011-28861 Filed 11-7-11; 8:45 am]
BILLING CODE 4910-13-P


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Source SHA-256
f0527fd1ac66433775f22bb909706c04e37573f1d459afefc96d41389fdd2fd1
Text SHA-256
d465cb97ff19207e5a95a123bd867dcf88d2a488b2f52b8dab2c086ea5140c3a

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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.