AD/FU24/43 - Installation of Crash Axes
1AD/FU24/43 - Installation of Crash Axes
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text Airparts (NZ) Ltd. FU 24 Series Aeroplanes
AD/FU24/43 Installation of Crash Axes 9/71
Applicability: All models.
Requirement: 1. Aircraft engaged in agricultural operations - Install a crash axe on the left hand inner side of the cockpit immediately below the canopy opening.
- Aircraft fitted out for passenger carrying in the fuselage - Install a crash axe on the left hand inner side of the cockpit immediately below the canopy opening, and another on the inside surface of the cargo door.
Compliance: Within 100 hours time in service after 30 September 1971.