Airworthiness Directive

AD 98-16-14 63 FR 42205 Active

Federal Aviation Administration · 14 CFR part 39

FR document
98-20837
Amendment
39-10690
Published
1998-08-07
Effective
1998-09-21
Models covered
1
Last live check
2026-09-30
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AD

98-16-14

FR doc 98-20837 · 63 FR 42205

AD 98-16-14Published 1998-08-07Effective 1998-09-21

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Requires replacing the attachment bolts, nuts and washers of the lower fitting of the main landing gear (MLG), and adjusting the torque values of the nuts.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to all Pilatus Britten-Norman Ltd. (Pilatus Britten-Norman) BN- 2, BN-2A, BN-2B, and BN-2T series airplanes. This AD requires replacing the attachment bolts, nuts and washers of the lower fitting of the main landing gear (MLG), and adjusting the torque values of the nuts. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for the United Kingdom. The actions specified by this AD are intended to prevent the bolts that attach the lower fitting of the MLG to the nacelle from becoming threadbound, which could result in structural failure of the MLG with consequent loss of control of the airplane during takeoff, taxi, or landing operations.

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All Britten-Norman BN-2 Islander directives

Applies to 1 model in our index