Airworthiness Directive

AD 98-05-06 63 FR 10299 Active

Federal Aviation Administration · 14 CFR part 39

Requires inspecting the elevator for incorrect rivet lengths and installing new rivets if incorrect rivet lengths are found.

FR document
98-5201
Amendment
39-10367
Published
1998-03-03
Effective
1998-05-29
Models covered
1

Last live check: 2026-08-19

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AD

98-05-06

FR doc 98-5201 · 63 FR 10299

AD 98-05-06Published 1998-03-03Effective 1998-05-29

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 inspecting the elevator for incorrect rivet lengths and installing new rivets if incorrect rivet lengths are found.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain Pilatus Aircraft Ltd. (Pilatus) Model PC-12 airplanes. This AD requires inspecting the elevator for incorrect rivet lengths and installing new rivets if incorrect rivet lengths are found. This AD also requires inspecting the elevator to assure that an excessive gap (more than .004 inches or .1 millimeters (mm)) does not exist in the rivet shanks, and installing a shim between the rib and skin to fill any excessive gap. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Switzerland. The actions specified in this AD are intended to prevent fatigue damage to the elevator, which could result in structural failure and eventual loss of control of the airplane.

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All Pilatus PC-12 directives

Applies to 1 model in our index