Airworthiness Directives; Bombardier Model CL-215-1A10 and CL- 215-6B11 Series Airplanes; Correction
airworthiness · Rule · Direct final rule; correction. · Published 1998-05-04 · Effective 1998-07-09 · 63 FR 24389
Document
Document number
98-11560
Federal Register citation
63 FR 24389
Type
Rule
Action
Direct final rule; correction.
Category
airworthiness
Manufacturer
Bombardier Model CL-215-1A10 and CL- 215-6B11 Series
Publication date
1998-05-04
Effective date
1998-07-09
FAA docket
Docket No. 98-NM-05-AD
Abstract
This document corrects an error that appeared in amendment 39- 10458 that was published in the Federal Register on April 10, 1998 (63 FR 17672). The error resulted in the inadvertent omission of the applicability statement of the amendment. This amendment 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.