Commonwealth legislation

AD/BEECH 23/46 Amdt 1 - Flight Controls

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Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This airworthiness directive requires owners/operators of specified Beechcraft 19, 23 and 24 series aeroplanes to inspect, lubricate and, if necessary, modify aileron control rod ends in accordance with Beechcraft Mandatory Service Bulletin 2198 Rev 1 (or an approved equivalent). (Requirement)

Compliance is due within 100 flight‑hours after 10 August 1989 or at the next scheduled Maintenance Release; owners/operators pay for and arrange the work, and Amendment 1 merely clarifies the procedure for aircraft with an existing 1 3/8″ inspection hole. (Compliance; Amendment 1)

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Direct links to the current provisions in AD/BEECH 23/46 Amdt 1 - Flight Controls.

AD/BEECH 23/46 Amdt 1 - Flight Controls

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

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Beechcraft 19, 23 and 24 Series Aeroplanes

AD/BEECH 23/46

Amdt 1

Flight Controls 3/90

Applicability: Beechcraft A23-19, 19A, M19A and B19 with S/Nos MB-1 through MB-520. B19 Sport 150 with S/Nos MB-521 through MB-813, MB-815 and MB-816. 23, A23, A23A, B23 and C23 with S/Nos M-1 through M-1361.

C23 Sundowner 180 with S/Nos M-1362 through M-1874, and M-1876 through M- 1879.

A23-24 and A24 with S/Nos MA-1 through MA-368. A24R with S/Nos MC-2 through MC-95.

A24R and B24R Sierra 200 with S/Nos MC-96 through MC-310, MC-312 through MC-448, MC-450 and MC-451.

Requirement: Action in accordance with Beechcraft Mandatory SB 2198 Rev 1, or equivalent approved modification.

Compliance: Within 100 hours time in service after 10 August 1989, or at next scheduled inspection for Maintenance Release after 10 August 1989 whichever occurs later.

Background: The manufacturer considers this Requirement mandatory enabling examination and lubrication of rod ends during routine inspections, reducing the possibility of failure and loss of aileron control.

Amendment 1 references Revision 1 to the Requirement document which clarifies the modification for aircraft with existing 1 3/8" inspection hole.

Source text

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

1 AD/BEECH 23/46 Amdt 1 - Flight Controls