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Airworthiness Directives; Fokker Model F28 Mark 0070 and Mark 0100 Series Airplanes

airworthiness · Rule · Final rule. · Published 1998-08-14 · Effective 1998-09-18 · 63 FR 43612

Document

Document number
98-21653
Federal Register citation
63 FR 43612
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Fokker Model F28 Mark 0070 and Mark 0100 Series
Publication date
1998-08-14
Effective date
1998-09-18
FAA docket
Docket No. 97-NM-248-AD

Abstract

This amendment adopts a new airworthiness directive (AD), applicable to all Fokker Model F28 Mark 0070 and Mark 0100 series airplanes, that requires inspection of the wing leading edge sections for the correct amount of bleed air exhaust holes, and corrective actions, 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 malfunction of the wing leading edge thermal anti-ice system, which could result in reduced controllability of the airplane and/or reduced structural integrity of the wing due to overheating.

Source

Authoritative
Federal Register document
Machine
JSON-LD · Markdown