Airworthiness Directive

AD 2005-12-09 70 FR 34323 Active

Federal Aviation Administration · 14 CFR part 39

FR document
05-11614
Amendment
39-14125
Published
2005-06-14
Effective
2005-07-28
Models covered
1
Last live check
2026-10-01
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AD

2005-12-09

FR doc 05-11614 · 70 FR 34323

AD 2005-12-09Published 2005-06-14Effective 2005-07-28

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 you to repetitively inspect the nose landing gear (NLG) assembly, paying special attention to the NLG swivel tube and the engine truss in the area of the NLG attachment, for cracks and damaged (defective) welding seams.

Full official abstract

The FAA adopts a new airworthiness directive (AD) for all GROB-WERKE (GROB) Model G120A airplanes. This AD requires you to repetitively inspect the nose landing gear (NLG) assembly, paying special attention to the NLG swivel tube and the engine truss in the area of the NLG attachment, for cracks and damaged (defective) welding seams. If you find cracks or defects during any inspection, this AD requires you to replace the cracked or defective part. This AD results from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. We are issuing this AD to detect and correct cracks and defects in the NLG assembly, which could result in failure of the NLG. This failure could lead to a hard landing and/or loss of control of the airplane during landing operations.

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Applies to 1 model in our index