CL-600-2B19 - Cabin Completion - 16 PAX Certification Basis Limitations Supplemental Type Definition Document STDD00-06/06M, Issue 01, dated March 27, 2007 or later approved revisionsAeroplane Flight Manual Supplement A-00-06/461-AFM, Issue 01, dated January 05, 2007 or later approved revisionsInstructions forContinued (...) Conditions 1. Certification Basis of the Change: JAR-25 Change 13, addtionally: CRI F-01, Executive Power System (Guidance Material)CRI D-01, Side Faching Divans (Deviation)CRI D-04, Door between passenger compartments with integrated blocking functionality (D (...)

CL-600-2B19 Cabin Completion - 13 PAX Certification Basis Limitations Supplemental Type Definition Document STDD00-06/11M, Issue 01, dated September 18, 2007 or later approved revisionAeroplane Flight Manual Supplement A-00-07/580-AFM, Issue 01, dated June 13, 2007 or later approved revision.Instructions forContinued (...) Conditions 1. Certification Basis of Change: JAR-25 Change 13, additionally:CRI D-01, Side- Facing DivanCRI D-04, Door between passenger compartment with integrated blocking functionalityCRI D-05, Isolated compartmentCRI F-01, Executive Power SystemJAA TGM Leaf (...)

Installation of Structural Provisions for AeroH Antenna system Certification Basis Limitations LHT Declaration of Compliance No. 1613 dated 22 January 2008LHT Supplemental Type Definition Document No. STDD-07/06M dated 22 January 2008 Conditions 1. For all flights with "Green Aircraft" and Structural Provisions for AeroH Antenna System" (2,5 [kg]) installed the installationof Ferry-Kit M/S TC 601R16990 (867 [kg]) is necessary.2. With the installation of Ferry-Kit M/S TC 601R16990(867 [kg]) (...)

Installation of a two tank Auxiliary Fuel System. Certification Basis Limitations -FAA STC No. ST00365NY-D dated 29 January 2007.-Configuration 3. Installation of structural provisions only, for a two(2) Cell Auxiliary Fuel System within the fuselage pressure vesselforward of the baggage compartment in accordance with PATS Aircr (...) Conditions 1. PATS Aircraft, LLC Airplane Flight Manual Supplement No.200, Rev. IRFAA approved January 5, 2007 is required with configuration 5.2. PATS, Inc. Aircraft Maintenance Manual Supplement No. 1, Report No.TO-417, Revision 3 dated May 23, 1995 or later (...)

Revisions to Auxiliary Fuel System Structural Provisions Certification Basis IM.A.023The Certification Basis for the original product and the followingadditional or alternative airworthiness requirements are applicable tothis certificate/ approval.CRI H- 01The requirements for environmental protection and the associatedcertif (...) Limitations EASA STC No. 10027222 dated 15 September 2009.FAA STC No. ST00365NY- D dated 14 January 2011.Configuration 6. Installation of a two tank Auxiliary Fuel System withinthe fuselage pressure vessel forward of the baggage compartment inaccordance with PAT (...) Conditions PATS Aircraft, LLC. Airplane Flight Manual Supplement No. 200, RevisionB, FAA approved 11 June 2009, is required with configurations 5 and 6.

Ladder Stowage Certification

Basis Limitations - Transport Canada STC SA07-4 -

Elisen Technologies Inc. Master Data List MDL-29R2-648, Revision NC, dated 21 January 2007, or later Transport Canada approvedrevision. 

Main wheel stowage

Certification Basis Limitations - Transport Canada STC SA07-6

Elisen Technologies Inc. Master Data List MDL-29R2-653, Revision NC, dated 21 January 2007, or later Transport Canada approvedrevision. 

Equipment Bay Forward Catwalk, Project No. 29R2-709. Certification Basis Limitations MDL-29R2-709 revision NC or later approved revision.Instructions for continued Airworthiness ICA-29R2-709 Revision NC or later approved revision. Conditions

Iridium Antenna Installation

Certification Basis Limitations - Transport Canada STC SA07-9 -

Elisen Technologies Inc. Master Data List MDL-29R2-639, Revision NC, dated 21 January 2007 or later Transport Canada approved revision. 

Equipment Bay Stowage Box, Project No. 29R2-710.

Certification Basis Limitations MDL-29R2-710 revision NC or later approved revision.

Instructions for continued airworthiness ICA-29R2-710 revision NC or later approved revision.

Conditions Prior to installation of this modification the installer must determine that the interrelationship between this modification and any other previously installed modification will introduce no adverse effect upon the airworthiness of the product. The (...)