Commonwealth legislation

AD/G1159/6 - Vertical Tail Rear Beam Attaching Bolts - Inspection and Modification

RepealedCTH

This Act has been repealed and is no longer in force. It is retained for historical reference.

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This mandatory Airworthiness Directive requires owners/operators of Gulfstream (Grumman) G‑1159 (Gulfstream II) and G‑IV series aircraft to inspect and modify the bolts attaching the vertical tail rear beam to the fuselage to ensure secure tail attachment. Compliance must follow Grumman Gulfstream II Aircraft Service Change No. 139 and be completed within 100 flight hours or three months after 30 November 1972.

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AD/G1159/6 - Vertical Tail Rear Beam Attaching Bolts - Inspection and Modification

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source Gulfstream (Grumman) G1159 and G-IV Series Aeroplanes

AD/G1159/6 Vertical Tail Rear Beam Attaching Bolts - Inspection and Modification

11/72

Applicability: All models.

Document: Grumman Gulfstream II Aircraft Service Change No. 139.

Compliance: Within 100 hours time in service or 3 months after 30 November 1972 whichever occurs first.

Source text

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