Document ID: chunk:federal_register_of_legislation:F2007L04610:body:0:p1
Version: federal_register_of_legislation:F2007L04610
Segment Type: other
Provision Reference: 
Character Range: 0–3813

AIRWORTHINESS DIRECTIVE
For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.001(1) of CASR 1998.  The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.

Robin Aviation Series Aeroplanes
AD/ROBIN/39  State of Design Airworthiness Directives  1/2008 DM

Applicability:  All Robin HR200-100, HR200-120, HR200-120B, HR200-160, HR200-100S, R2160, R2100, R2100A, R2160D, R2112, R2160I and R2120U aircraft.
Requirement:       1. Determine the applicability of the CAA (NZ) Airworthiness Directives (AD) listed in Table 1.

                   2. If it is determined that a CAA (NZ) AD is applicable and has not been previously accomplished, perform the actions required by the CAA (NZ) AD.

                Note 1:  In some cases the CAA (NZ) AD will refer to equivalent French DGAC ADs as a means of compliance with the AD. Table 1 provides a list of those ADs. If the equivalent Direction Générale de l'Aviation Civile (DGAC) AD is reflected in the aircraft log books as been complied with then no further action is required for the equivalent CAA (NZ) AD.
                   TABLE 1
                NZ CAA AD Number  Effective Date     Equivalent DGAC AD  Title
                DCA/R2000/1       29 June 2006       F-1974-052          Aft Fuselage Side Cover Plates
                DCA/R2000/2       29 June 2006       F-1974-138          Battery Protection Fuse - Modification
                DCA/R2000/3       29 June 2006       F-1974-160          VOR Antenna Support Rib  Inspection and Modification
                DCA/R2000/4       29 June 2006       F-1975-054          Engine Flexible Baffles
                DCA/R2000/5       29 June 2006       F-1975-156          Flap Rib Assemblies
                DCA/R2000/6       29 June 2006       F-1975-185          Engine Bearer Attachments
                DCA/R2000/7       29 June 2006       F-1975-230          Fuel Tank Filler Caps
                DCA/R2000/8       29 June 2006       F-1976-078          Cylinder Metallic Baffles
                DCA/R2000/9       29 June 2006       F-1976-167          Aileron Control Cable Bolts
                DCA/R2000/10      29 June 2006       F-1978-075          Flaps with Three Ribs - Inspection and Replacement
                DCA/R2000/11      29 June 2006       F-1980-005          Battery - Inspection and Modification
                DCA/R2000/12      29 June 2006       F-1980-186          Fuel Fittings
                DCA/R2000/18      29 June 2006       F-1989-074R1        Safety Belt Quick-disconnect Link
                DCA/R2000/20      29 June 2006       F-1994-183R1        Fuel Tank Filler Caps
                DCA/R2000/26      29 September 2006  F-1999-114 R3       Manifold Air Intake
                DCA/R2000/29      29 June 2006       F-2000-172          Control Surfaces - Calibration and Balance
                DCA/R2000/35      29 June 2006       F-2002-364          Air Intake Flap Hinge
                DCA/R2000/36      29 June 2006       F-2003-202          Aileron Bellcrank
                DCA/R2000/38      29 June 2006       No Equivalent       Cabin Compartment Barrier - Inspection and Modification
                DCA/R2000/39      31 August 2006     No Equivalent       Fuel Shut - Off Mechanism

                Note 2:  NZ CAA ADs may be accessed via the