AD 2009-10-09 R2
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| 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 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.
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.
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Retrieved: Apr 8, 2026
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