Document ID: chunk:federal_register_of_legislation:F2006B03641:body:0
Version: federal_register_of_legislation:F2006B03641
Segment Type: other
Provision Reference: 
Character Range: 0–1061

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

 Beechcraft 1900 Series Aeroplanes

AD/BEECH 1900/24 Ground Fine Switch 10/98
 Applicability: Model 1900D aeroplanes with serial numbers UE-1 through UE-271 inclusive. Requirement:               Modify the ground idle low pitch stop system by incorporating Raytheon 'Ground
            Fine Switch Installation Kit' No 129-5200-1 in accordance with the Accomplishment
            Instructions of Raytheon Aircraft Mandatory Service Bulletin No 2714 issued June 1997.

            Note: FAA AD 98-13-11 Amdt 39-10599 refers.

 Compliance: Within 800 hours time in service after the effective date of this directive.

            This airworthiness directive becomes effective on 10 September 1998.

            Background:  This directive is intended to prevent a loose or misrigged ground fine switch, which could result in a hard landing causing structural damage to the airframe and possible passenger injury.