Commonwealth legislation

AD/LEARJET/16 - Secondary Yaw Damper Servo Cable Clamp Bolt - Inspection

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This AD mandates a one‑time inspection of the secondary yaw damper servo cable clamp bolt on Gates Learjet Model 25 aircraft (S/N 25‑003 to 25‑249), to be completed within 100 hours time‑in‑service after 31 Dec 1978 using Gates Learjet SB 25‑285. Owners/operators must arrange and pay for the inspection (and any repairs); it imposes short‑term costs and maintenance demand to address a specified safety concern.

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AD/LEARJET/16 - Secondary Yaw Damper Servo Cable Clamp Bolt - 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/16 Secondary Yaw Damper Servo Cable

Clamp Bolt - Inspection

Applicability: All model 25 with S/Nos. 25-003 to 25-249. Document: Gates Learjet SB 25-285.

Compliance: Within 100 hours time in service after 31 December 1978.

10/78

Source text

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