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.