Airworthiness Directive

AD 99-01-07 Amendment 39-10974

Federal Aviation Administration · 14 CFR part 39

FR document
98-34382
Amendment
39-10974
Published
1998-12-31
Models covered
1
Last live check
Not yet re-verified
AD

99-01-07

FR doc 98-34382

AD 99-01-07Published 1998-12-31Effective 1999-03-19

Requires installing additional stringers at the lower fuselage skin panels between the main and rear spar frames.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain British Aerospace Jetstream Model 3101 airplanes. This AD requires installing additional stringers at the lower fuselage skin panels between the main and rear spar frames. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for the United Kingdom. The actions specified in this AD are intended to correct a strength deficiency in the area of the lower fuselage skin panels between the main rear spar frames, which, if not corrected, could result in reduced or loss of control of the airplane during maximum speed limit operations.

Applies to 1 model in our index