BOMBARDIER CHALLENGER 850, CL-600-2B19 MODIFICATIONS (109)

Removal of Divan Seating Restriction

Installation of an arrester block cushion onto the upper surface of the forward divan cabinet, which allows the removal of an existing restriction on the occupation of the forwardmost seating position on the side facing divan, The change also removes existing placards which limited the seat position as “Not to be occupied during Taxi. Take-off or Landing”.

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Introduction of Wireless Local Area Network.

An Airborne Wireless Local Area Network Unit (AWLU), comprising a CNX-200 Network

Accelerator and two S-band antennas provides, in conjunction with the satellite communication system, onboard data networking for computers and other electronic devices used by both passengers and crew. Access to the Local Area Network (LAN) is via wireless connection or four LAN ports located at the left-hand seat 2, right-hand seat 2, left-hand outboard seat 4, and left-hand seat 5.

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Introduction of a Corporate Interior

Installation of corporate passenger interior configuration into Bombardier CL600-2B16 (605 variant).

 

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Interior alteration and reconfiguration to a passenger seating capacity of...

Interior alteration and reconfiguration to a passenger seating capacity of 14

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CL-600-2B19 - Cabin Completion - 16 PAX Certification Basis Limitations...

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 (...)

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CL-600-2B19 Cabin Completion - 13 PAX Certification Basis Limitations Supplemental...

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 (...)

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CL-600-2B19 - Cabin Completion - 15 PAX # Configuration D....

CL-600-2B19 - Cabin Completion - 15 PAX # Configuration D. Certification Basis Limitations 1. Supplement Type Definition Document STDD00-05/12M, issue 04, dated November 13, 2007, or later approved revision2. Configuration Identification Document CID-15- 01619-LHT,issue 03, dated November 2, 2007, or later approved revisionConfigurat (...) Conditions 1. Certification Basis of Change: JAR-25 Change 13, additionally:Configuration A and B*:CRI D-01, Side facing Divan (Deviation)CRI F-01, Executive Power Systems (Guidance Material)JAA TGL No. 17, Passenger service and In-Flight Entertainment (IFE (...)

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Installation of Structural Provisions for Cabin Completion Certification Basis Limitations...

Installation of Structural Provisions for Cabin Completion Certification Basis Limitations LHT Declaration of Compliance No. 1611 dated 29 January 2008LHT Supplemental Type Definition Document No. STDD00- 07/05M, Issue 1 dated 29 January 2008 Conditions 11. For all flights with "Green Aircraft" and Structural Provisions for cabin completion" (293,7 [kg]) installed the installation of Ferry- Kit M/S TC 601R16990 (867 [kg]) is necessary.2. With the installation of Ferry- Kit M/S TC 601R16990 (867 [kg]) the aircraft will stay in C.G. envelope.

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Cabin Completion Certification Basis Limitations Lufthansa Technik Supplemental Type Definition...

Cabin Completion Certification Basis Limitations Lufthansa Technik Supplemental Type Definition Document No.STDD00-07/07M Issue 01 dated 13/02/08 or later approved revision.Airplane Flight Manual Supplement No. A-00-07/693-AFM Issue 01 or later approved revision. Conditions 1. Installation of "CL-600-2B19 - Installation of structural provisions for cabin completion", approved with EASA STC No. EASA.A.S.03097 is required prior to the installation of this STC.2. The limitation Installation of Ferry-Kit M/S TC 601R (...)

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Installation of an Executive Interior Certification Basis EASA IM.A.023The Certification...

Installation of an Executive Interior Certification Basis EASA IM.A.023The Certification Basis for the original product and the followingadditional or alternative airworthiness requirements are applicable tothis certificate/ approvalCRI H- 01The requirements for environmental protection and the associatedce (...) Limitations Configuration 1:EASA STC No. 10027223 Revision 1 dated 08 February 2010.FAA STC No. ST01730NY-D dated 14 January 2011.PATS Aircraft, LLC Master Drawing List 6049-0001-MDL, revision F dated01 July 2009.PATS Aircraft, LLC. Airplane Flight Manual Suppl (...) Conditions In this installation the maximum passenger seating capacityis limitedto 15.

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