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Textron Hawker Beechcraft Hawker 400, Interior Modification

Airframe Systems (ATA 20-50) Communication (ATA 23) Cabin Interiors (ATA 25 + 44) Structure (ATA 51-57)
Overview Product description

Overview

STC Number
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STC Date
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Contact Details
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Introduction

Change in interior seating arrangement, addition of sink toexisting rear lavatory, fabrication and installation of RH fwd cabinet,revision of existing LH fwd cabinet, revision tointerior finishing details, and addition of new fuselage antenna. Certification Basis Limitations Installation according Phoenix Aero Aviation Engineering Ltd. Engineering Service Bulletin PA-ESB-06-002 Issue 1, Rev. Original approved 28 April 2006 or later approved revision.Operation must be in accordance with Phoenix Aero Aviation Engineering (...) Conditions 1. This Installation is limited to the Serial No. RK-37 (Registration SE-DRS).2. Compatibility of this modification with other previously approved modifications must be determinedby the installer.

Your needs

 An addition of a sink to the existing rear lavatory, fabrication and installation of RH fwd cabinet, revision of existing LH fwd cabinet, revision to interior finishing details, and addition of new fuselage antenna.

Your benefits

More storage and ammenities are added to the aircraft.
Textron Hawker Beechcraft Hawker 400, Beechjet 400, MU-300 Diamond I, II
€ RFQ

Product Description

Change in interior seating arrangement,
addition of sink toexisting rear lavatory,
fabrication and installation of RH fwd
cabinet,revision of existing LH fwd cabinet,
revision tointerior finishing details, and
addition of new fuselage antenna.

Certification Basis


Limitations
Installation according Phoenix Aero Aviation
Engineering Ltd. Engineering Service Bulletin
PA-ESB-06-002 Issue 1, Rev. Original
approved 28 April 2006 or later approved
revision.Operation must be in accordance
with Phoenix Aero Aviation Engineering (...)

Conditions
1. This Installation is limited to the Serial No.
RK-37 (Registration SE-DRS).2.
Compatibility of this modification with other
previously approved modifications must be
determinedby the installer.

Please contact modification supplier for further details.

STC Status: Revision Level:
STC Date: 19/12/06
Responsible Office: EASA

 

Your benefits

More storage and ammenities are added to the aircraft.