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

Airframe Systems (ATA 20-50) Cabin Interiors (ATA 25 + 44)
Overview Product description

Overview

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Introduction

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.
Bombardier Challenger 850, CL-600-2B19
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Product Description

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.

Please contact modification supplier for further details.

STC Status: Revision Level:
STC Date: 05/02/08
Responsible Office: EASA