Airworthiness Directive

AD 95-04-09 60 FR 12408 Active

Federal Aviation Administration · 14 CFR part 39

FR document
95-4369
Amendment
39-9161
Published
1995-03-07
Effective
1995-04-14
Models covered
1
Last live check
2026-09-30
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AD

95-04-09

FR doc 95-4369 · 60 FR 12408

AD 95-04-09Published 1995-03-07Effective 1995-04-14

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 repetitively inspecting the nose wheel steering drive ring for cracks, and replacing any cracked drive ring.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to Pilatus Britten-Norman BN2A, BN2B, and BN2T Islander and BN2A Mk III Trislander series airplanes that are equipped with a nose wheel steering disconnect system with either a Modification NB/M/503 or Modification NB/M/733 nose undercarriage unit. This action requires repetitively inspecting the nose wheel steering drive ring for cracks, and replacing any cracked drive ring. A report of the rudder pedals jamming in the central position during takeoff on one of the affected airplanes prompted this action. The actions specified by this AD are intended to [[Page 12409]] prevent failure of the nose wheel steering system because of a cracked drive ring, which, if not detected and corrected, could result in the inability to move the rudder pedals.

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All Britten-Norman BN-2 Islander directives

Applies to 1 model in our index