Commonwealth legislation

AD/G1159/31 Amdt 1 - Elevator Trim Tab Outboard Hinge Fittings - Inspection

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

4/10 complexity

This directive requires operators of Gulfstream (Grumman) GII and GIIB aircraft to inspect elevator trim tab outboard hinge fittings—initially before the next flight after 31 July 1982 if not already done—and to carry out repeat inspections until the fittings are repaired or replaced per the referenced service change, issued after reports of cracked fittings.

Operators and maintenance providers bear inspection and repair costs and must obtain the manufacturer service documents to comply.

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Current sections

Direct links to the current provisions in AD/G1159/31 Amdt 1 - Elevator Trim Tab Outboard Hinge Fittings - Inspection.

AD/G1159/31 Amdt 1 - Elevator Trim Tab Outboard Hinge Fittings - Inspection

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

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Gulfstream (Grumman) G1159 and G-IV Series Aeroplanes

AD/G1159/31

Amdt 1

Elevator Trim Tab Outboard Hinge Fittings - Inspection

7/82

Applicability: All model GII and GIIB aircraft.

Document: Grumman Customer Bulletin No. 325 Amendment 1. (FAA AD 82-11-02 Amdt. 39-

4384 refers).

Compliance: 1. Unless already accomplished, before further flight after 31 July 1982 - as detailed in the requirement document.

Repeat inspection as detailed in the requirement document until repair or replacement as detailed in the Aircraft Service Change No. 315.

Background: Manufacturer reports trim tab hinge fitting cracks have occurred. Amendment 1 raised to cover increases in applicability and revisions to repeat inspection, repair or replacement requirements.

Source text

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

1 AD/G1159/31 Amdt 1 - Elevator Trim Tab Outboard Hinge Fittings - Inspection