Commonwealth legislation

AD/LEARJET 35/9 - Secondary Yaw Damper Servo Cable Clamp Bolt - Inspection

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This airworthiness directive requires a one‑time inspection of the clamp bolt securing the secondary yaw‑damper servo cable on Gates Learjet 35 and 36 airframes within the specified serial‑number ranges.

Operators of those S/Ns must complete the inspection within 100 flight hours after 31 Dec 1978, using Gates Learjet SB 35/36‑22‑2; the AD imposes the obligation but does not allocate costs or specify corrective actions.

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AD/LEARJET 35/9 - 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 35 and 36 Series Aeroplanes

AD/LEARJET 35/9 Secondary Yaw Damper Servo Cable

Clamp Bolt - Inspection

Applicability: All model 35 with S/Nos. 35-001 to 35-182.

All model 36 with S/Nos. 36-001 to 36-038.

Document: Gates Learjet SB 35/36-22-2.

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

12/78

Source text

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