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Airworthiness Directive

AD 2009-10-09 R2 76 FR 53308 Active

Federal Aviation Administration · 14 CFR part 39

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 rudder stop modification kit.

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FR document
2011-21210
Amendment
39-16782
Published
2011-08-26
Effective
2011-09-12
Models covered
1

Last live check: 2026-08-19

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AD

2009-10-09 R2

FR doc 2011-21210 · 76 FR 53308

AD 2009-10-09 R2Published 2011-08-26Effective 2011-09-12

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

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 rudder stop modification kit.

1 correction to this AD FAA · 2011-11-08

Correction published 2011-11-08

Issued by
Federal Aviation Administration
Published
2011-11-08
Document
Federal Register 2011-28861 · Final rule; correction

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.

A correction restates part of an AD that was published incorrectly. It is not an additional requirement and it does not change the AD number or its effective date.

Source: Federal Register document 2011-28861, retrieved 2026-08-15

Read this correction on Federal Register (opens in a new tab)
Full official abstract

We are revising an existing airworthiness directive (AD) for 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. That AD 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 rudder stop modification kit. This new AD requires a change to the modification kit and removal of a small amount of material from the rudder horn assembly for those that have not yet complied with the existing AD or for those who can not comply with the existing AD (because they were unable to obtain full rudder travel with the existing kits). This AD was prompted by operators who have reported difficulty in obtaining full rudder travel with the existing modification kit. We are issuing this AD to revise the kits to use longer rivets and allow a small amount of material to be removed from the rudder horn assembly, which allows operators to obtain full rudder travel.

More directives for Cessna 150/152

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  2. AD 2009-10-09 R1 Airworthiness Directives; Cessna Aircraft Company 150 and 152 Series Air... Effective 2009-12-11
  3. AD 2009-10-09 Airworthiness Directives; Cessna Aircraft Company 150 and 152 Series Air... Effective 2009-06-17
  4. AD 2008-22-18 Airworthiness Directives; Cessna Aircraft Company 150 Series Airplanes Effective 2008-12-09
  5. AD 2004-19-01 Airworthiness Directives; Cessna Aircraft Company 120, 140, 140A, 150, F... Effective 2004-11-01

All Cessna 150/152 directives

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)

Applies to 1 model in our index