Commonwealth legislation

AD/LEARJET/6 - Wing Flap System - Inspection

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This Airworthiness Directive requires owners/operators of specified Gates Learjet 24 (s/n 24-100 to 24-296) and Learjet 25 (s/n 25-003 to 25-175) to carry out the wing flap system inspection in Gates Learjet Service Bulletin No. 23/24/25‑257 within 25 hours time‑in‑service after 27 August 1974.

It creates a mandatory, short‑window compliance obligation and shifts technical detail and potential repair costs to operators, who must obtain and follow the referenced service bulletin.

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AD/LEARJET/6 - Wing Flap System - 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 Gates Learjet 24 & 25 Series Aeroplanes

AD/LEARJET/6 Wing Flap System - Inspection 8/74

Applicability: All models: 24 with S/Nos. 24-100 to 24-296. 25 with S/Nos. 25-003 to 25-175. Document: Gates Learjet SB No. 23/24/25-257.

Compliance: Within 25 hours time in service after 27 August 1974.

Source text

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