Commonwealth legislation

AD/G159/17 - Wing Front Beam - Wing to Fuselage Fitting - Inspection

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This instrument requires owners/operators of Gulfstream (Grumman) G.159 series aeroplanes to inspect the wing-to-fuselage fittings at butt line 9.0 and "associated areas" per Grumman Gulfstream 1 Service Change No. 190, with the first check within six months after 28 Jan 1972 and repeated at least annually. Any required rework must follow that Service Change or a manufacturer‑approved alternative, with operators bearing costs and the manufacturer controlling approvals.

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Current sections

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AD/G159/17 - Wing Front Beam - Wing to Fuselage Fitting - Inspection

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COMMONWEALTH OF AUSTRALIA CIVIL AVIATION ORDERS CIVIL AVIATION SAFETY AUTHORITY PART 105 SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source GULFSTREAM (GRUMMAN) G.159 SERIES AEROPLANES

AD/G159/17 Wing Front Beam - Wing to Fuselage Fitting -

Inspection

1/72

Applicability: All models.

Requirement: Inspect the wing to fuselage fittings at butt line 9.0 and associated areas as detailed in GRUMMAN GULFSTREAM 1 Service Change No. 190. Rework as necessary as detailed in that Service Change or a variation approved by the manufacturer.

Compliance: Within 6 months after 28 January 1972 and thereafter at intervals not exceeding 1 year.

Source text

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