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Airworthiness Directives; British Aerospace (Jetstream) Model 4101 Airplanes

airworthiness · Rule · Final rule. · Published 2000-02-03 · Effective 2000-03-09 · 65 FR 5228

Document

Document number
00-2088
Federal Register citation
65 FR 5228
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
British Aerospace (Jetstream) Model 4101
Publication date
2000-02-03
Effective date
2000-03-09
FAA docket
Docket No. 99-NM-309-AD

Abstract

This amendment adopts a new airworthiness directive (AD), applicable to all British Aerospace (Jetstream) Model 4101 airplanes, that requires manufacture and installation of a placard on the left- hand instrument panel in the cockpit to prohibit push-backs of the airplane while the engines are running. In lieu of accomplishing the placard installation, this amendment requires repetitive installation of a new tow bracket sub-assembly that has the serial number and date of installation vibro etched on it. 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 fatigue failure of the towing bracket. Failure of the towing bracket could cause a towing vehicle to collide into the propeller while the airplane engines are running, and consequently, cause damage to the airplane, and injure ground personnel, flight crew, or passengers.

Source

Authoritative
Federal Register document
Machine
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