Airworthiness Directive

AD 2003-11-12 68 FR 32629 Superseded

Federal Aviation Administration · 14 CFR part 39

Requires replacement of the wings after a certain operational time.

FR document
03-13384
Amendment
39-13171
Published
2003-06-02
Effective
2003-06-05
Models covered
1

Last live check: 2026-08-19

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AD

2003-11-12

FR doc 03-13384 · 68 FR 32629

AD 2003-11-12Published 2003-06-02Effective 2003-06-05

Superseded by 2017-10-03 Supersedes 2003-03-13

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 replacement of the wings after a certain operational time.

Full official abstract

This document supersedes Airworthiness Directive (AD) 2003-03- 13, which currently establishes a technical service life for MORAVAN a.s. (Moravan) Model Z-242L airplanes by restricting Acrobatic and Utility category operations and requiring replacement of the wings after a certain operational time. AD 2003-03-13 resulted from mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for the Czech Republic. The restrictions required by AD 2003- 03-13 only take account for the aerobatic load spectrum and do not account for the aerobatic frequency. The restrictions also address the life limit of the wings when they should address the life limit of the entire airframe (life limit of the airplane). Although the aerobatic frequency will extend the operational times, it more importantly will ensure that all airplanes (even those that have not reached the operational limits) are not subject to fatigue cracking caused by exceeding the aerobatic frequency. This AD will maintain the restrictions of AD 2003-03-13, but will incorporate the aerobatic frequency and life limit the airplane instead of just the wings. The actions specified by this AD are intended to prevent structural failure of the wing due to fatigue cracking. Such failure could result in a wing separating from the airplane with consequent loss of airplane control.

More directives for Moravan / Zlin Z-143/Z-242

  1. AD 2017-10-03 Airworthiness Directives; ZLIN AIRCRAFT a.s. Airplanes Effective 2017-07-05
  2. AD 2008-12-06 Airworthiness Directives; MORAVAN a.s. Model Z-143L Airplanes Effective 2008-07-16
  3. AD 2008-07-02 Airworthiness Directives; MORAVAN a.s. Model Z-143L Airplanes Effective 2008-03-31
  4. AD 2007-11-19 Airworthiness Directives; MORAVAN a.s. Model Z242L Airplanes Effective 2007-06-05
  5. AD 2003-03-13 Airworthiness Directives; MORAVAN a.s. Model Z-242L Airplanes Effective 2003-03-21

All Moravan / Zlin Z-143/Z-242 directives

Applies to 1 model in our index