Overview

STC Number
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Contact Details
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Introduction

Installation of a EGPWS Mk. VIII system in accordance with the Engineering Order Doc.: 2017016-EO-02 Issue 2 or later EASA approvedrevision. Certification Basis Limitations Conditions 1. AFM Supplement Document No. 2017016-AM-02 Issue 2 orlater EASA approved revisions.2. Maintenance Requirements and Instruction for Continuous Airworthiness Doc. 2017016-CA-02.


Textron Hawker Beechcraft Hawker 400, Beechjet 400, MU-300 Diamond I, II
€ RFQ

Product Description

Installation of a EGPWS Mk. VIII system in
accordance with the Engineering Order Doc.:
2017016-EO-02 Issue 2 or later EASA
approvedrevision.

Certification Basis


Limitations


Conditions
1. AFM Supplement Document No.
2017016-AM-02 Issue 2 orlater EASA
approved revisions.2. Maintenance
Requirements and Instruction for Continuous
Airworthiness Doc. 2017016-CA-02.

Please contact modification supplier for further details.

STC Status: Revision Level: REV. 1
STC Date: 15/02/08
Responsible Office: EASA