AD/PL 12/4 - Stub Wing Structure - Inspection (Commonwealth) — Barrister AI

Latest Cases Case Lookup LegislationBeta Notebook Research Briefs

AD/PL 12/4 - Stub Wing Structure - Inspection (Commonwealth) — Barrister AI

All legislation

COMMONWEALTHLegislative Instrument

In force

Official source Save

This is the latest official compilation.Check the official source →

Ask a question about this ActPro

InstrumentInstrument identification s ApplicabilityApplicability s RequirementRequirement s ComplianceCompliance

Section Whole Act

About this Act

TypeLegislative Instrument

Provisions4

Official source

AD/PL 12/4 - Stub Wing Structure - Inspection

InstrumentInstrument identification

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

Transavia PL 12 Series Aeroplanes

AD/PL 12/4 Stub Wing Structure - Inspection 12/68

ApplicabilityApplicability

All models.

RequirementRequirement

Inspect the stub wing leading edge tube for cracking in the vicinity of landing gear attachment.

ComplianceCompliance

Within 100 hours time in service after 14 February 1969 and thereafter at intervals not exceeding 100 hours time in service.

Provisions

InstrumentInstrument identification s ApplicabilityApplicability s RequirementRequirement s ComplianceCompliance