Airworthiness Directives; Bombardier Model DHC-8-100 and -300 Series Airplanes
airworthiness · Rule · Final rule. · Published 2000-06-13 · Effective 2000-07-18 · 65 FR 37014
Document
Document number
00-14313
Federal Register citation
65 FR 37014
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Bombardier Model DHC-8-100 and -300 Series
Publication date
2000-06-13
Effective date
2000-07-18
FAA docket
Docket No. 98-NM-380-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to certain Bombardier Model DHC-8-100 and -300 series airplanes, that requires revising the Aircraft Log Book to correct the airplane Production Modification List; performing an inspection to determine which bonded skin panels on the airplane require bonding integrity inspections (BII); and revising the Airworthiness Limitations List of the Approved Maintenance Plan to include the BII requirements. This amendment also requires, for certain airplanes, repetitive ultrasonic bond inspections to detect disbonding of airplane skin panels, and repair, if necessary. This amendment is prompted by issuance of mandatory continuing airworthiness information by a foreign civil airworthiness authority. The actions specified by this AD are intended to prevent damage to bonded skin panels to go undetected, which could result in failure of the bonded skin panels, and consequent loss of controllability of the airplane.