The modification will consist of a composite structure witha metal faceplate wich will be fitted over the center of the existing Glareshield. An area of the existing glareshield will be removed to allow for wires to be routed to the annunciators and (...) Certification Basis Limitations Master Data List R25-0283 Rev. E, dated 17 January 2006AFM Supplement Doc. Nr. R25- 342, Rev. IR dated 24 November 2004 Conditions
Installation of fiberglass tail cone in lieu of metal tail cone.
Installation of Artex C406 (406 MHz) Series emergency locator transmitter, antenna, and remote switch assembly
GPS / Navigation / Communication, Dual Garmin GNS 430/530 AWinstallationThe installation includes GPS antenna and single marker beacon receiver(KMR 675 or 51Z6) installation Certification Basis EASA TCDS IM.A.207The Certification Basis for the original product remains applicable tothis certificate/ approvalThe requirements for environmental protection and the associatedcertificated noise and/ or emissions levels of the original product are (...) Limitations ·,,Master Document List "2053445 DOC" Issue 3 from 20 Jan. 2011·,,Aircraft Flight Manual Supplement for GNS 430/530 AW,VHFCommunication Receiver, VOR/ILS Receiver / GPS Receiver "2053445-AM A"Issue 1 from 01 June 2010·,,Aircraft Flight Manual Supple (...) Conditions None
Installation of quick release nose radome latch mechanisms.
Installation of Garmin Dual GTN-750 SystemRevision 1 adds the TAWS limitation to MSN 550-0672 and revokes theInitial Issue of the approval. Certification Basis The Certification Basis (CB) for the original product remains applicableto this certificate/ approval.The requirements for environmental protection and the associatedcertified noise and/ or emissions levels of the original product areunchanged and remain applicable to this certificate/ approval. Limitations -Scandinavian Avionics, AFM Supplement GTN-750, 2081059-AM A , issue 4,dated 12 June 2013-Scandinavian Avionics, AFM Supplement GMA-35, 2081059-AM B, issue 1,dated 25 February 2013-Scandinavian Avionics, AFM Supplement GWX-70, 2081059-AM C, issue 1, (...) Conditions Periodic Structural Inspection:GPS Antenna, Task No. 34-2081059-02Initial: At next 24 month / 800 hours inspectionThereafter: at every 24 month / 800 hours inspectionGPS Antenna, Task No. 34-2081059-03*Initial: no later than 11.000 LDG (after instal (...)
Installation of nose radome quick release mechanism.