Document ID: chunk:federal_register_of_legislation:F2005B00951:body:0:p9
Version: federal_register_of_legislation:F2005B00951
Segment Type: other
Provision Reference: 
Character Range: 20374–23275

beyond the maximum and minimum continuous safe operating limits;
 (c) each take-off and precautionary range shall be marked with a yellow arc;
 (d) each engine speed range that is restricted because of excessive vibration shall be marked with a red arc.

 (5) The aircraft shall contain the following placards:
 (a) "THIS AIRCRAFT HAS BEEN CERTIFICATED IN THE AMATEUR-BUILT CATEGORY";
 (b) except where acrobatic manoeuvres have been permitted under paragraph 3.26 (2) — "NO ACROBATIC MANOEUVRES (INCLUDING SPINS) PERMITTED";
 (c) where the airspeed indicator is not marked with the colour‑code described in paragraph 3.27 (3) — a placard listing the airspeed limitations;
 (d) where the power-plant instruments are not marked with the colour-code described in paragraph 3.27 (4) — a placard listing the powerplant limitations;
 (e) identification of the various functional positions of the controls of the fuel valves or cocks;
 (f) on, or adjacent to, each fuel filler cap — "FUEL" and the minimum fuel grade designation for the engine and the usable capacity of the fuel tank;
 (g) the compass calibrations;
 (h) loading instructions if necessary to ensure that in all conditions of operation the aircraft centre of gravity will remain within limits;
 (i) "NO SMOKING", unless:
 (i) fuel tanks fitted in the cockpit or cabin are isolated by means of vapour and fuel proof enclosures; and
 (ii) the cockpit and cabin linings, flooring and furnishing materials are at least flame resistant; and
 (iii) self-contained ash tray(s) are provided.
4 DOCUMENTS
For an aeroplane which is the first of a type or model to be issued with an Australian certificate of airworthiness the following data and documents shall be submitted for retention by CASA:

 (1) For an aeroplane of Australian design, a report which substantiates that the aircraft complies with the design standards specified in subsection 3 of this section. Unless otherwise agreed to by CASA, the report shall include the following:
 (a) a specification of the aeroplane including its engine(s) and propellers(s);
 (b) a basic applied loads report;
 (c) a justification of all primary structural components, either by means of a detailed stress analysis, or a report of static test, or a report justifying the structure by direct comparison with existing certificated aeroplanes;
 (d) a flight test report.

 (2) For an aeroplane of overseas design:
 (a) evidence of the aircraft's overseas certification and operational status which may take the form of:
 (i) a satisfactory service history recorded by examples of the type in respect of which certificates recognised by CASA as being evidence of the aircraft's airworthiness have been issued by the competent authority in a member state of the International Civil Aviation Organization; or
 (ii) an adequate structural justification together with evidence of a satisfactory service history