Airworthiness Directive

AD 98-12-14 63 FR 31107 Active

Federal Aviation Administration · 14 CFR part 39

FR document
98-15084
Amendment
39-10570
Published
1998-06-08
Effective
1998-07-18
Models covered
1
Last live check
2026-10-01
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AD

98-12-14

FR doc 98-15084 · 63 FR 31107

AD 98-12-14Published 1998-06-08Effective 1998-07-18

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 flap cable pulley bracket for correct alignment and correcting any misalignment; inspecting the flap control cable for wear (nicks, cuts, frays, etc.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain AERMACCHI S.p.A. (AERMACCHI) S.205 series and Models S.208 and S.208A airplanes. This AD requires inspecting the flap cable pulley bracket for correct alignment and correcting any misalignment; inspecting the flap control cable for wear (nicks, cuts, frays, etc.), and replacing the flap control pulley bracket and flap control cable if worn. 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 flap control failure, which could result in loss of control of the airplane.

More directives for Aermacchi S.205 / S.208

  1. AD 2013-22-23 R1 Airworthiness Directives; AERMACCHI S.p.A. Airplanes 2014-07-11
  2. AD 2013-22-23 Airworthiness Directives; Aermacchi S.p.A. Airplanes 2013-11-14
  3. AD 98-08-06 Airworthiness Directives; AERMACCI S.p.A. S.205 Series and Models S.208 ... 1998-04-10
  4. AD 98-08-04 Airworthiness Directives; AERMACCI S.p.A. Models S.208 and S.208A Airpla... 1998-04-09

All Aermacchi S.205 / S.208 directives

Applies to 1 model in our index