Airworthiness Directive

AD 98-08-07 63 FR 17323 Active

Federal Aviation Administration · 14 CFR part 39

FR document
98-9153
Amendment
39-10456
Published
1998-04-09
Effective
1998-04-28
Models covered
1
Last live check
2026-10-03
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AD

98-08-07

FR doc 98-9153 · 63 FR 17323

AD 98-08-07Published 1998-04-09Effective 1998-04-28

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 rudder and elevator pivot arms with parts of improved design.

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 replacing the rudder and elevator pivot arms with parts of improved design. This AD results from reports of cracks in the elevator and rudder trim tab pivot arms on the above- referenced airplanes. The actions specified by this AD are intended to prevent failure of the elevator and rudder caused by fatigue cracking of the pivot arms, which could result in reduced airplane controllability and possible loss of control of the airplane.

More directives for Pilatus PC-7

  1. AD 2020-26-19 Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes 2021-02-22
  2. AD 2021-04-06 Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes 2021-02-12
  3. AD 2019-05-15 Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes 2019-04-03
  4. AD 2018-04-10 Airworthiness Directives; Pilatus Aircraft Limited Airplanes 2018-03-08
  5. AD 2016-17-07 Airworthiness Directives; PILATUS Aircraft Ltd. Airplanes 2016-08-26

All Pilatus PC-7 directives

Applies to 1 model in our index