Jan. 39, 1940 54 STAT.] NEW ZEALAND-CERTIFICATES OF AIRWORTHINESS Feb. 28 , 1940 (c) With Respect to the First of Each Glass I and Class II Unit to be Imported into New Zealand from the United States not as a Component of a Complete Aircraft: (1) A set of specifications descriptive of the Unit, if not ade- quately included in data previously furnished for the air- craft in which the Unit may be installed or used. (2) A repair manual for the Unit, stating limits of accuracy recommended overhaul times, and similar information, if such a manual has been issued, and if such information is not contained in data previously furnished for the com- plete aircraft in which the Unit may be installed or used. (d) With Respect to Each Class I Unit Imported into New Zealand: (1) A Certificate of Compliance. (2) Information in the nature of Service Bulletins, etc. issued from time to time by the manufacturer pertaining to such aircraft and aircraft Unit subsequent to the shipment thereof. 4. Aircraft, aircraft engines, propellers, and appliances of all de- scriptions shall comply fully either (1) with the applicable provisions of the following Parts of the Civil Air Regulations issued by the competent aeronautical authorities of the United States, as revised to May 31, 1938: Part 04-Airplane Airworthiness Part 13-Aircraft Engine Airworthiness Part 14-Aircraft Propeller Airworthiness Part 15-Aircraft Equipment Airworthiness or (2) with the requirements of said Parts of the Civil Air Regula- tions as revised to May 31, 1938 plus any or all further amendments or revisions thereof, provided that if the competent aeronautical authorities of New Zealand shall have notified the competent aero- nautical authorities of the United States that any such amendments or revisions are not acceptable, or if such further amendments or re- visions have not been communicated to the competent aeronautical authorities of New Zealand sixty (60) days prior to the date of ship- ment of the aircraft Unit, compliance with the amendments or re- visions in question shall not entitle aircraft Units to be imported under these requirements. 5. Provision shall be made in all aircraft for protection against the effect of static electricity while refueling. 6. Provision shall be made in all aircraft to prevent accidental or unauthorized operation of air controls and throttles, and to avoid accidental interference with the ignition switches and fuel shut-off valves. 7. The aircraft structure shall be investigated for and comply with the British center of pressure back (CPB) condition for normal category aircraft. 8. All engines shall be fitted with dual ignition. 9. All ignition switches of the "toggle" type shall be so arranged that ignition is "off" when the knob of the switch is in the downward position. Compliance with Regulations. Designated require- ments. 2269
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