Commonwealth legislation

AD/DH114/31 - Rudder Control Pedal Reversal Lever - Inspection

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This directive mandates recurring inspections of the rudder control pedal reversal lever on DH114 (Heron) aeroplanes, requiring the first check within 100 hours time-in-service after 31 March 1971 and thereafter at intervals not exceeding 2400 hours. Operators, owners and maintenance organisations must use Hawker Siddeley TNS Heron (114) No. CF.15 for the inspection procedure. It protects control‑system safety but imposes recurring inspection costs, downtime and reliance on the referenced technical document.

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AD/DH114/31 - Rudder Control Pedal Reversal Lever - 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 DH114 (Heron) Series Aeroplanes

AD/DH114/31 Rudder Control Pedal Reversal Lever - Inspection NK

Applicability: All models.

Document: Hawker Siddeley TNS Heron (114) No. CF.15.

Compliance: Within 100 hours time in service after 31 March 1971 and thereafter at intervals not exceeding 2400 hours time in service.

Source text

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