Commonwealth legislation

AD/LEARJET/3 - Rudder Pedal Heel Plates - Inspection

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Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This Airworthiness Directive mandates a one-time inspection of rudder pedal heel plates on specified Gates Learjet 24 and 25 aircraft, to be carried out per Gates Learjet Service Bulletin No. 23/24/25-244 within 100 hours time-in-service after 31 July 1973. It affects owners/operators of the listed serial-numbered aircraft, who must schedule the inspection and bear the cost; technical and corrective actions are delegated to the referenced service bulletin.

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AD/LEARJET/3 - Rudder Pedal Heel Plates - 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/3 Rudder Pedal Heel Plates - Inspection 6/73

Applicability: All model 24 with S/Nos. 24-100 to 24-266 and model 25 with S/Nos. 25-003 to 25-

Document: Gates Learjet SB No. 23/24/25-244.

Compliance: Within 100 hours time in service after 31 July 1973.

Source text

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