Commonwealth legislation

AD/SC7/16 - Wing Lower Skin/Wing Lift Strut Fairing - Inspection

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

Operators of Short SC7 (Skyvan) series 3, 3A and 3M must carry out recurring inspections of the wing lower skin and wing lift strut fairing placement, beginning within 100 hours TIS after 30 April 1980 and repeating at intervals not exceeding 100 hours until the aeroplane is modified per the manufacturer’s service bulletin. The rule, funded by operators, aims to detect mislocated fairings before they cause progressive structural wing damage.

JSON API

Deep dive

Want the full deep dive?

Zoe can write the in-depth analysis on top of the summary above: how it works, who it affects and what each part actually does.

Current sections

Direct links to the current provisions in AD/SC7/16 - Wing Lower Skin/Wing Lift Strut Fairing - Inspection.

AD/SC7/16 - Wing Lower Skin/Wing Lift Strut Fairing - Inspection

meta-content-style-type: text/css meta-content-type: application/xhtml+xml; charset=utf-8 meta-generator: Aspose.Words for .NET 22.10.0

?xml version="1.0" encoding="utf-8" standalone="no"?>

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source Short SC7 (Skyvan) Series Aeroplanes

AD/SC7/16 Wing Lower Skin/Wing Lift Strut Fairing - Inspection 2/80

Applicability: All Skyvan series 3, 3A and 3M. Document: Shorts SB No. 57-63.

Compliance: Within 100 hours time in service after 30 April 1980 and thereafter at intervals not exceeding 100 hours time in service until modified in accordance with SB No. 57-64.

Background: Damage to the wing lower skin can occur over a period of time due to incorrect location of the wing lift strut fairing.

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.