Airworthiness Directive

AD 2000-02-21 Amendment 39-11539

Federal Aviation Administration · 14 CFR part 39

FR document
00-2088
Amendment
39-11539
Published
2000-02-03
Models covered
1
Last live check
Not yet re-verified
AD

2000-02-21

FR doc 00-2088

AD 2000-02-21Published 2000-02-03Effective 2000-03-09

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.

Full official 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.

Applies to 1 model in our index