European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA ...
European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA ...
European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA ...
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TCDS IM.A.070 Page 31/49<br />
Issue 04, 16 December 2010<br />
Environmental Standards:<br />
Noise ICAO Annex 16 Volume I (See <strong>EASA</strong> TCDSN IM.A.070)<br />
Fuel Venting & Emissions ICAO Annex 16 Volume II<br />
Elect to Comply Requirements: †<br />
� Hydraulic System Proof Pressure Testing<br />
Reference CRI F-14<br />
Additional National Requirements for Type Certification:<br />
� As defined in GIV CRI A-01 Addendum 1.<br />
Means of Compliance (MOC) or Interpretative Material: †<br />
� Electronic Flight Displays (JAA AMJ 25.11 & SAE ARP 4256)<br />
Reference CRI F-06<br />
� Complex Electronic Hardware (JAA Draft Guidance leaflet ‘Recognition of<br />
EUROCAE document ED-80: Design assurance guidance for airborne electronic<br />
hardware’)<br />
Reference CRI F-07<br />
� Software Design Assurance (JAA AGM Section 1, Part 3, Leaflet 4 ‘Recognition of<br />
EUROCAE ED-12B/RTCA DO-178B’)<br />
Reference CRI F-08<br />
� Systems for Specified Operational Use (Various, see CRIs)<br />
Reference CRI F-01<br />
� Equipment, Systems & Installation (JAA NPA 25F-281)<br />
Reference CRI F-09<br />
� Flight in Icing Conditions (JAA/TGM/25/02)<br />
Reference CRI F-15<br />
� Aeroplane System Wiring<br />
Reference CRI F-17<br />
� Head Up Display System<br />
Reference CRI F-04<br />
� Oxygen Requirements (JAR OPS 1.770, 1.780)<br />
Reference CRI F-16<br />
� Installation of IFE Systems (JAA TGL No.17)<br />
Reference CRI F-20<br />
� In Seat Power Supply Systems (JAA/TGM/25/10)<br />
Reference CRI F-23<br />
� Category 2 Go-Around Performance (JAR AWO 243, NPA AWO-5)<br />
Reference CRI K-01<br />
� Landing Distance using Head-Up Guidance System (JAR AWO 342)<br />
Reference CRI K-02<br />
� Floor Path Emergency Escape Path Marking System (JAR 25.812)<br />
Reference CRI D-15<br />
� All Weather Operation for Category 2 (JAR AWO Change 2) – Post TC<br />
Reference CRI F-05<br />
� Wheels and tyres Failure Analysis<br />
Reference CRI D-14<br />
� Engine Rotor Non-containment and Critical Flight Control Systems<br />
Reference CRI E-04<br />
† New <strong>EASA</strong> items raised specifically for the GIV-X project (i.e. over and above those<br />
applied by FAA and applicable to the basic FAA build standard, which are not
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