Airworthiness Directive

AD 2006-13-11 71 FR 35778 Active

Federal Aviation Administration · 14 CFR part 39

Requires you to inspect the aileron assembly for correct configuration and modify as necessary.

FR document
06-5587
Amendment
39-14664
Published
2006-06-22
Effective
2006-08-07
Models covered
1

Last live check: 2026-08-19

This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.
AD

2006-13-11

FR doc 06-5587 · 71 FR 35778

AD 2006-13-11Published 2006-06-22Effective 2006-08-07

Supersedes 2002-21-08

Supersedence is read from the Federal Register text of the newer AD — the FAA publishes no structured field for it — and names only ADs held in our index.

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 you to inspect the aileron assembly for correct configuration and modify as necessary.

Full official abstract

We are adopting a new airworthiness directive (AD) that supersedes AD 2002-21-08, which applies to certain Pilatus Aircraft Ltd (Pilatus) Model PC-6 airplanes. AD 2002-21-08 currently requires you to inspect the aileron assembly for correct configuration and modify as necessary. Since we issued AD 2002-21-08, the FAA determined the action should also apply to all the models of the PC-6 airplanes listed in the type certificate data sheet of Type Certificate (TC) No. 7A15 that were produced in the United States through a licensing agreement between Pilatus and Fairchild Republic Company (also identified as Fairchild Industries, Fairchild Heli Porter, or Fairchild-Hiller Corporation). In addition, the intent of the applicability of AD 2002-21-08 was to apply to all the affected serial numbers of the airplane models listed in TC No. 7A15. This AD retains all the actions of AD 2002-21-08, adds those Fairchild Republic Company airplanes to the applicability of this AD, and lists the individual specific airplane models. We are issuing this AD to correct improper aileron assembly configuration, which could result in failure of the aileron mass balance weight. Such failure could lead to loss of control of the airplane.

More directives for Pilatus PC-6 Porter

  1. AD 2021-24-22 Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes Effective 2022-01-25
  2. AD 2021-11-08 Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes Effective 2021-07-12
  3. AD 2020-16-02 Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes Effective 2020-09-09
  4. AD 2020-11-06 Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes Effective 2020-06-30
  5. AD 2019-10-07 Airworthiness Directives; Pilatus Aircraft Ltd. Airplanes Effective 2019-07-10

All Pilatus PC-6 Porter directives

Applies to 1 model in our index