Federal Register of Legislation - Australian Government

Primary content

AD/BELL 222/37 - Tail Rotor Pitch Change Mechanism

Authoritative Version
AD/BELL/222/37 Airworthiness Directives/Pt 105 — Aircraft as made
Tail Rotor Pitch Change Mechanism
Administered by: Infrastructure, Transport, Regional Development and Communications
Exempt from sunsetting by the Legislation (Exemptions and Other Matters) Regulation 2015 s12 item 15
Registered 06 Jul 2007
Tabling HistoryDate
Tabled HR07-Aug-2007
Tabled Senate07-Aug-2007
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Legislative Instrument
 
F2007L02132 : Authoritative PDF Document : 0.2MB Primary Document Icon F2007L02132 : ZIP Document : 10KB
1 page
 

Explanatory Statement
 
F2007L02132ES : PDF Document : 9KB Primary Document Icon F2007L02132ES : ZIP Document : 4KB
1 page