Commonwealth legislation

AD/DH 104/26 - Rudder Control Pedal Reversal Lever - Inspection

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This directive mandates inspection of the rudder control pedal reversal lever on all DH 104 (Dove) aeroplanes, carried out per Hawker Siddeley TNS CT(104) No. 219. The first check is required within 100 hours TIS after 31 March 1971 and thereafter at intervals not exceeding 2400 hours. It creates a recurring maintenance obligation for operators, owners and maintenance organisations, who must schedule, fund and follow the referenced procedure to maintain compliance.

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AD/DH 104/26 - 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 DH 104 (Dove) Series Aeroplanes

AD/DH 104/26 Rudder Control Pedal Reversal Lever - Inspection 2/71

Applicability: All models.

Document: Hawker Siddeley TNS CT(104) No. 219.

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.