Document ID: chunk:federal_register_of_legislation:F2006B07306:body:0
Version: federal_register_of_legislation:F2006B07306
Segment Type: other
Provision Reference: 
Character Range: 0–815

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

 Aerospatiale (Socata) TB9 and TB10 (Tobago) Series Aeroplanes

AD/TB10/4 Wing Flap Deflection - Modification 5/82

 Applicability: All TB10 aircraft from S/No. 1 up to and including S/No. 239. Document:  Rallye TB SB No. 10 GR.27.17.
            Note: Upon incorporation of this modification aircraft flight manuals should have amendment 4 incorporated and the contents of amendment 3 removed.

 Compliance: Before certification.

            Background:  In order to maintain adequate longitudinal stability with full flap extended, maximum flap extension has been reduced from 32o to 25o30'. Additionally the forward C.G. limit is amended to 11% M.A.C. or .949m.