Commonwealth legislation

AD/BEECH 200/31 Amdt 1 - Elevator Control Horn Attachment

RepealedCTH

This Act has been repealed and is no longer in force. It is retained for historical reference.

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

A mandatory airworthiness directive requiring owners/operators of certain Beechcraft Super King Airs (Model 200: BB‑3–BB‑674; 200C: BL‑1–BL‑8; 200T: BT‑1–BT‑16) to install additional rivets in the elevator control‑horn per Beechcraft Service Instruction No. 1111 Revision 1.

This fixes a connection that can loosen in service and impair pitch control; work must be completed within 100 flight hours after 31 May 1981 if not already done.

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Current sections

Direct links to the current provisions in AD/BEECH 200/31 Amdt 1 - Elevator Control Horn Attachment.

AD/BEECH 200/31 Amdt 1 - Elevator Control Horn Attachment

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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 Beechcraft 200 (Super King Air) Series Aeroplanes

AD/BEECH 200/31

Amdt 1

Elevator Control Horn Attachment 5/81

Applicability: All models 200 with S/Nos BB-3 to BB-674. All models 200C with S/Nos BL-1 to BL-8. All models 200T with S/Nos BT-1 to BT-16.

Requirement: Action in accordance with Beechcraft SI No 1111 Rev 1.

Compliance: Unless already accomplished, within 100 hours time in service after 31 May 1981.

Background: The installation of additional rivets in the elevator control horn attachment has been found necessary under service conditions to prevent looseness developing in this control connection. This amendment adds additional aeroplanes and revises accomplishment instructions.

Source text

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