Summary
We are adopting a new airworthiness directive (AD) for certain Hawker Beechcraft Corporation (Type Certificate Previously Held by Raytheon Aircraft Company) Model BAe.125 Series 800A (including C-29A and U-125), and 800B airplanes; and Model Hawker 800 (including variant U-125A) and 800XP airplanes modified in accordance with a certain winglet supplemental type certificate. This AD requires revising the Limitations section of the airplane flight manual (AFM) and installing placards on the instrument panel. This AD was prompted by reports of several instances of severe vibration and wing/aileron oscillations. We are issuing this AD to prevent vibration and wing/aileron oscillations, which could cause structural damage or lead to divergent flutter, and result in loss of integrity of the wing, loss of control of the airplane, and in-flight breakup.
Directive Details
AD Number
FAA-2013-0462
Document Number
2013-14247
Type
Rule
Publication Date
June 17, 2013
Effective Date
July 2, 2013
Affected Manufacturer
Hawker Beechcraft Corporation (Type Certificate Previously Held by Raytheon Aircraft Company)
Criticality
routine
Emergency
No
Docket ID
Docket No. FAA-2013-0462
Topics
Official Documents
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