1AD/BN-2/41 Amdt 1 - Elevator and Flap Control Rods - Inspection

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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 Pilatus Britten-Norman BN-2 Series Aeroplanes

 

AD/BN-2/41

Amdt 1

Elevator and Flap Control Rods - Inspection NK

 

Applicability: All models.

 

Requirement: 1. Inspect elevator and flap control rods for corrosion and rectify in accordance with Britten Norman SB No. BN-2/SB.101.

 

2.    Bonding clips and leads may be removed completely provided that:

 

(a)     Radio system still performs satisfactorily; and

 

(b)     Control rod fork end bearings are of all metal construction.

 

Note: If bearings are fitted with “plastic” inserts it will be necessary for the bonding clips and leads to be replaced.

 

Compliance: Within 100 hours time in service after 31 October 1977.