Airworthiness Directive

AD 98-08-04 63 FR 17316 Active

Federal Aviation Administration · 14 CFR part 39

Requires inspecting the landing gear rod springs to assure they are made with a wire diameter of 4.

FR document
98-9114
Amendment
39-10453
Published
1998-04-09
Effective
1998-05-26
Models covered
1

Last live check: 2026-08-19

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AD

98-08-04

FR doc 98-9114 · 63 FR 17316

AD 98-08-04Published 1998-04-09Effective 1998-05-26

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 landing gear rod springs to assure they are made with a wire diameter of 4.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to all AERMACCI S.p.A. Models S.208 and S.208A airplanes. This AD requires inspecting the landing gear rod springs to assure they are made with a wire diameter of 4.5 millimeters (mm), and replacing any that have a wire diameter of 4.0 mm. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Italy. The actions specified by this AD are intended to prevent failure of the landing gear caused by an insufficient wire diameter of the rod springs, which could result in loss of control of the airplane during landing operations.

More directives for Aermacchi S.205 / S.208

  1. AD 2013-22-23 R1 Airworthiness Directives; AERMACCHI S.p.A. Airplanes Effective 2014-07-11
  2. AD 2013-22-23 Airworthiness Directives; Aermacchi S.p.A. Airplanes Effective 2013-12-16
  3. AD 98-12-14 Airworthiness Directives; AERMACCHI S.p.A. S.205 Series and Models S.208... Effective 1998-07-18
  4. AD 98-08-06 Airworthiness Directives; AERMACCI S.p.A. S.205 Series and Models S.208 ... Effective 1998-05-26

All Aermacchi S.205 / S.208 directives

Applies to 1 model in our index