AD/BEECH 23/35 - Flap Control Assembly

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Legislation au F2006B03749 In force Legislative Instrument

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Beechcraft 19, 23 and 24 Series Aeroplanes

 

AD/BEECH 23/35 Flap Control Assembly 4/78

Applicability: All Models: 23, A23, A23A, B23 & C23 with s/Nos. M-1 to M-1979; A23-19, 19A & B19 with S/Nos. MB-1 to MB-866. A23-24 & A24 with S/Nos. MA-1 to MA-368 and A24R, B24R & C24R with S/Nos. MC-2 to MC-536.

 

Requirement: Action in accordance with Beechcraft SI No. 0940.

 

Note: FAA AD 78-04-01 Amdt. 39-3139 refers.

 

Compliance: 1. Inspect at intervals not exceeding 100 hours time in service until modified.

 

2. Modify before 1 January 1979.

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.