Airworthiness Directive

AD 98-21-35 63 FR 55528 Active

Federal Aviation Administration · 14 CFR part 39

FR document
98-27604
Amendment
39-10843
Published
1998-10-16
Effective
1998-11-23
Models covered
2
Last live check
2026-09-30
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AD

98-21-35

FR doc 98-27604 · 63 FR 55528

AD 98-21-35Published 1998-10-16Effective 1998-11-23

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 replacing the main landing gear left and right actuator clevis assembly.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain Raytheon Aircraft Company (Raytheon) Models A200CT, B200, B200C, B200CT, 200T/B200T, 300, B300, and B300C airplanes. This AD requires replacing the main landing gear left and right actuator clevis assembly. Reports of main landing gear failure on two of the affected airplanes prompted this action. The actions specified by this AD are intended to prevent failure of the actuator clevis assembly in the main landing gear caused by fatigue cracking of the original design part, which could result in loss of control of the airplane during landing operations.

More directives for Beechcraft King Air 200 (Super King Air)

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  2. AD 2010-26-03 Airworthiness Directives; Hawker Beechcraft Corporation Models B200, B20... 2010-12-16
  3. AD 2008-07-10 Airworthiness Directives; Hawker Beechcraft Corporation Models B200, B20... 2008-04-07
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  5. AD 2006-23-02 Airworthiness Directives; Raytheon Aircraft Company Models C90A, B200, B... 2006-11-08

All Beechcraft King Air 200 (Super King Air) directives

Applies to 2 models in our index