Airworthiness Directives; Bombardier Model CL-215-1A10 and CL- 215-6B11 Series Airplanes
airworthiness · Rule · Direct final rule; request for comments. · Published 1998-04-10 · Effective 1998-07-09 · 63 FR 17672
Document
Document number
98-9340
Federal Register citation
63 FR 17672
Type
Rule
Action
Direct final rule; request for comments.
Category
airworthiness
Manufacturer
Bombardier Model CL-215-1A10 and CL- 215-6B11 Series
Publication date
1998-04-10
Effective date
1998-07-09
FAA docket
Docket No. 98-NM-05-AD
Abstract
This amendment adopts a new airworthiness directive (AD), that is applicable to certain Bombardier Model CL-215-1A10 and CL-215-6B11 series airplanes. This amendment requires repetitive inspections to detect cracking on certain wing to fuselage frame-angles, and repair, if necessary. This amendment is prompted by issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified in this amendment are intended to detect and correct cracking in the wing to fuselage frame-angles, which could result in reduced structural integrity of the airframe.