AD/SA-TP/28 - Wing Lift Strut Fretting (Commonwealth) — Barrister AI

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AD/SA-TP/28 - Wing Lift Strut Fretting (Commonwealth) — Barrister AI

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COMMONWEALTHLegislative Instrument

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InstrumentInstrument identification s ApplicabilityApplicability s RequirementRequirement s ComplianceCompliance s BackgroundBackground

Section Whole Act

About this Act

TypeLegislative Instrument

Provisions5

Official source

AD/SA-TP/28 - Wing Lift Strut Fretting

InstrumentInstrument identification

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

British Aerospace (Scottish Aviation) Twin Pioneer Series Aeroplanes

AD/SA-TP/28 Wing Lift Strut Fretting 12/86

ApplicabilityApplicability

All models.

RequirementRequirement

Modify in accordance with Scottish Aviation MNS No 965.

ComplianceCompliance

Prior to the issue of a Certificate of Airworthiness.

BackgroundBackground

This modification is to eliminate fretting on the surface of the wing lift strut at the stabilizer strut fitting.

Provisions

InstrumentInstrument identification s ApplicabilityApplicability s RequirementRequirement s ComplianceCompliance s BackgroundBackground