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

Airframe Systems (ATA 20-50) Cabin Interiors (ATA 25 + 44) Structure (ATA 51-57)
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Overview

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Introduction

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

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 (...)

Please contact modification supplier for further details.

STC Status: Revision Level:
STC Date: 29/03/07
Responsible Office: EASA