Commonwealth legislation

AD/SWSA226/41 - Flight Control, Control Column - Modification

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Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This AD mandates a modification to the flight control column cable pulley system on specified Fairchild (Swearingen) SA226/SA227 serial-numbered aircraft, to be done per Swearingen SB27-022. It was issued after a reported pulley failure causing loss of lateral control.

Affected owners/operators must complete the work within 300 hours TIS after 28 Feb 1982, bear costs and downtime, and have no alternative compliance options in the text.

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AD/SWSA226/41 - Flight Control, Control Column - Modification

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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 Fairchild (Swearingen) SA226 and SA227 Series Aeroplanes

AD/SWSA226/41 Flight Control, Control Column - Modification 2/82

Applicability: All model SA226-T S/N T201 to T290. All model SA226-AT S/N AT001 to AT066 and all model SA226-TC S/N TC201 to TC225.

Document: Swearingen SB27-022.

Note: FAA AD 81-26-04 Amendment 39-4284 refers.

Compliance: Within 300 hours time in service after 28 February, 1982.

Background: There has been a failure of the control column cable pulley system with subsequent loss of lateral control reported overseas.

Source text

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