Airworthiness Directive

AD 2002-22-03 Amendment 39-12927

Federal Aviation Administration · 14 CFR part 39

FR document
02-27418
Amendment
39-12927
Published
2002-11-01
Models covered
1
Last live check
Not yet re-verified
AD

2002-22-03

FR doc 02-27418

AD 2002-22-03Published 2002-11-01Effective 2002-12-20

Requires you to repetitively inspect the main landing gear front attachment brackets for cracks, and, if cracks are found, install improved-design brackets.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain PILATUS Aircraft Ltd. (Pilatus) Model PC-7 airplanes. This AD requires you to repetitively inspect the main landing gear front attachment brackets for cracks, and, if cracks are found, install improved-design brackets. Installing the improved-design brackets terminates the required inspections. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Switzerland. The actions specified by this AD are intended to detect and correct cracks in the main landing gear front attachment brackets, which could result in failure of the brackets. Such failure could lead to the main landing gear leg detaching from the wing main spar.

Applies to 1 model in our index