AD 2009-10-09 R2

final rule

Airworthiness Directives; Cessna Aircraft Company Airplanes

AD Number
2009-10-09 R2
Status
final_rule
Effective Date
Product Category
aircraft
Docket
FAA-2007-27747
FR Citation
(Federal Register Volume 76, Number 216 (Tuesday, November 8, 2011))
Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

Applicability

TypeManufacturerModelDetails
aircraft Cessna Aircraft Company 150F Airworthiness Directives; Cessna Aircraft Company Airplanes
aircraft Cessna Aircraft Company 150G Airworthiness Directives; Cessna Aircraft Company Airplanes
aircraft Cessna Aircraft Company 150H Airworthiness Directives; Cessna Aircraft Company Airplanes
aircraft Cessna Aircraft Company 150J Airworthiness Directives; Cessna Aircraft Company Airplanes
aircraft Cessna Aircraft Company 150K Airworthiness Directives; Cessna Aircraft Company Airplanes
aircraft Cessna Aircraft Company 150L Airworthiness Directives; Cessna Aircraft Company Airplanes
aircraft Cessna Aircraft Company 150M Airworthiness Directives; Cessna Aircraft Company Airplanes
aircraft Cessna Aircraft Company 152 Airworthiness Directives; Cessna Aircraft Company Airplanes
aircraft Cessna Aircraft Company A150K Airworthiness Directives; Cessna Aircraft Company Airplanes
aircraft Cessna Aircraft Company A150L Airworthiness Directives; Cessna Aircraft Company Airplanes
aircraft Cessna Aircraft Company A150M Airworthiness Directives; Cessna Aircraft Company Airplanes
aircraft Cessna Aircraft Company A152 Airworthiness Directives; Cessna Aircraft Company Airplanes
aircraft Cessna Aircraft Company F150F Airworthiness Directives; Cessna Aircraft Company Airplanes
aircraft Cessna Aircraft Company F150G Airworthiness Directives; Cessna Aircraft Company Airplanes
aircraft Cessna Aircraft Company F150H Airworthiness Directives; Cessna Aircraft Company Airplanes
aircraft Cessna Aircraft Company F150J Airworthiness Directives; Cessna Aircraft Company Airplanes
aircraft Cessna Aircraft Company F150K Airworthiness Directives; Cessna Aircraft Company Airplanes
aircraft Cessna Aircraft Company F150L Airworthiness Directives; Cessna Aircraft Company Airplanes
aircraft Cessna Aircraft Company F150M Airworthiness Directives; Cessna Aircraft Company Airplanes
aircraft Cessna Aircraft Company F152 Airworthiness Directives; Cessna Aircraft Company Airplanes
aircraft Cessna Aircraft Company FA150K Airworthiness Directives; Cessna Aircraft Company Airplanes
aircraft Cessna Aircraft Company FA150L Airworthiness Directives; Cessna Aircraft Company Airplanes
aircraft Cessna Aircraft Company FA150M Airworthiness Directives; Cessna Aircraft Company Airplanes
aircraft Cessna Aircraft Company FA152 Airworthiness Directives; Cessna Aircraft Company Airplanes
aircraft Cessna Aircraft Company FRA150L Airworthiness Directives; Cessna Aircraft Company Airplanes
aircraft Cessna Aircraft Company FRA150M Airworthiness Directives; Cessna Aircraft Company Airplanes

Unsafe Condition

The unsafe condition involves the potential for rudder control system failure due to insufficient rudder stop clearance, which could result in structural damage or loss of control during maneuvers beyond normal flight envelope.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Install a placard prohibiting spins and other acrobatic maneuvers, or replace the rudder stop, bumper, and hardware with a new rudder stop modification kit. Update the AFM/POH and logbook entry as required.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Before further flight

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

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.

AI-generated summary from the source AD text. Verify against the official source before acting.

Federal Register Abstract

Rudder Control System

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - 2009-10-09 R2_Correction.pdf
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Document Versions
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DetailsAttachments/Public Comments
AD Number:
2009-10-09 R2
Document Type:
AD Final Rules
Docket Number:
FAA-2007-27747
Subject Heading:
Airworthiness Directives; Cessna Aircraft Company Airplanes
Subject:
Rudder Control System
Status:
Current
Citation:
(Federal Register Volume 76, Number 216 (Tuesday, November 8, 2011))
Citation Publish Date:
11/08/2011
Effective Date:
09/12/2011
Make:
Cessna Aircraft Company
Model:
150F | 150G | 150H | 150J | 150K | 150L | 150M | 152 ...Show more
Product Type:
Aircraft
Product Subtype:
Small Airplane
Affected AD:
Superseded AD:
2009-10-09 R1
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
CORRECTION: (Federal Register Volume 76, Number 216 (Tuesday, November 8, 2011); Page 69123; www.access.gpo.gov/su_docs/aces/aces140.html)
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[Federal Register Volume 76, Number 216 (Tuesday, November 8, 2011)]


[Rules and Regulations]


[Page 69123]


From the Federal Register Online via the Government Printing 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: ann.johnson@faa.gov.


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


1
2


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


§ 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.

Document Text

Show stored source text (verify against official source)
AD Final Rules - 2009-10-09 R2_Correction.pdf
Copy URL
Document Versions
 Feedback
DetailsAttachments/Public Comments
AD Number:
2009-10-09 R2
Document Type:
AD Final Rules
Docket Number:
FAA-2007-27747
Subject Heading:
Airworthiness Directives; Cessna Aircraft Company Airplanes
Subject:
Rudder Control System
Status:
Current
Citation:
(Federal Register Volume 76, Number 216 (Tuesday, November 8, 2011))
Citation Publish Date:
11/08/2011
Effective Date:
09/12/2011
Make:
Cessna Aircraft Company
Model:
150F | 150G | 150H | 150J | 150K | 150L | 150M | 152 ...Show more
Product Type:
Aircraft
Product Subtype:
Small Airplane
Affected AD:
Superseded AD:
2009-10-09 R1
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
CORRECTION: (Federal Register Volume 76, Number 216 (Tuesday, November 8, 2011); Page 69123; www.access.gpo.gov/su_docs/aces/aces140.html)
Automatic Zoom
Actual Size
Page Fit
Page Width
⁨50⁩%
⁨75⁩%
⁨100⁩%
⁨125⁩%
⁨150⁩%
⁨200⁩%
⁨300⁩%
⁨400⁩%
125%
of ⁨12⁩
[Federal Register Volume 76, Number 216 (Tuesday, November 8, 2011)]


[Rules and Regulations]


[Page 69123]


From the Federal Register Online via the Government Printing 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: ann.johnson@faa.gov.


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


1
2


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


§ 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.

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.