Airworthiness Directives; Aerospatiale Model ATR42-300 and ATR42- 320 Series Airplanes
airworthiness · Rule · Final rule; request for comments. · Published 1997-12-23 · Effective 1998-01-07 · 62 FR 66980
Document
Document number
97-33509
Federal Register citation
62 FR 66980
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Aerospatiale Model ATR42-300 and ATR42- 320 Series
Publication date
1997-12-23
Effective date
1998-01-07
FAA docket
Docket No. 97-NM-283-AD
Abstract
This amendment supersedes an existing airworthiness directive (AD), applicable to all Aerospatiale Model ATR42-300 and ATR42-320 series airplanes, that currently requires repetitive ultrasonic inspections to detect fatigue cracks of the lower lugs of the barrel of the main landing gear (MLG); and replacement of cracked lower lugs with new or serviceable parts, and a follow-on inspection. This amendment expands the applicability of the existing AD. This action also provides for an optional terminating action, which, if accomplished, terminates the repetitive inspection requirement. This amendment is prompted by issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified in this AD are intended to detect and correct fatigue cracking of the lower lugs of the barrel of the MLG, which could lead to the collapse of the MLG.