Commonwealth legislation

AD/AMD 10/18 - Wing-to-Fuselage Junction - Inspection

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

The directive mandates a one‑off inspection of the wing‑to‑fuselage junction on Falcon 10 aircraft (S/N 1–70, 73–75) per AMD S.B. F10‑0205, required because of reported corrosion from deteriorated sealing compound.

Owners/operators must arrange and pay for the inspection and any repairs by the compliance deadline (31 March 1985).

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AD/AMD 10/18 - Wing-to-Fuselage Junction - Inspection

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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 AMD Falcon 10 Series Aeroplanes

AD/AMD 10/18 Wing-to-Fuselage Junction - Inspection 7/84

Applicability: All model Falcon 10 with S/Nos 1 to 70, 73, 74 and 75. Requirement: AMD S.B. F10-0205.

Note: Consigne De Navigabilite No. 84-41-19(B) refers.

Compliance: Prior to 31 March 1985.

Background: Corrosion of wing recesses and wing to fuselage attachments has been reported due to deterioration of the original recess filling and sealing compound.

Source text

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