Airworthiness Directive

AD 2011-03-04 76 FR 6525 Active

Federal Aviation Administration · 14 CFR part 39

FR document
2011-2008
Amendment
39-16588
Published
2011-02-07
Effective
2011-03-14
Models covered
1
Last live check
2026-09-30
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AD

2011-03-04

FR doc 2011-2008 · 76 FR 6525

AD 2011-03-04Published 2011-02-07Effective 2011-03-14

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 repetitive inspections of the rudder hinges and the rudder hinge brackets for damage, i.

Full official abstract

We are superseding an existing airworthiness directive (AD) for the products listed above. AD 2009-09-09 currently requires repetitive inspections of the rudder hinges and the rudder hinge brackets for damage, i.e., cracking, deformation, and discoloration. If damage is found during any inspection, AD 2009-09-09 also requires replacing the damaged rudder hinge and/or rudder hinge bracket. This new AD retains the inspection requirements of AD 2009-09-09, adds airplanes to the Applicability section, and adds a terminating action for the repetitive inspection requirements. This AD resulted from the manufacturer developing a modification that terminates the repetitive inspections and from the manufacture adding airplane serial numbers into the Applicability section. We are issuing this AD to detect and correct damage in the rudder hinges and the rudder hinge brackets, which could result in failure of the rudder. This failure could lead to loss of control.

More directives for Cessna 350/400 Corvalis

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  3. AD 2009-09-09 Airworthiness Directives; Cessna Aircraft Company (Type Certificate Prev... 2009-04-30
  4. AD 2007-07-06 R1 Airworthiness Directives; Cessna Aircraft Company (Type Certificate Prev... 2008-10-31
  5. AD 2007-07-06 Airworthiness Directives; Columbia Aircraft Manufacturing (Previously th... 2007-04-03

All Cessna 350/400 Corvalis directives

Applies to 1 model in our index