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Airplanes with a third attitude instrument system usable through flight attitudes of 360 degrees of pitch and roll and installed in accordance with the instrument requirements prescribed in § 121.305(j) of this chapter; and If VOR navigation equipment is required under paragraph (d)(2) of this section, no person may operate a U. S.-registered civil aircraft within the 50 states and the District of Columbia at or above FL 240 unless that aircraft is equipped with approved DME or a suitable RNAV system. 9A.4 Subject to paragraph 9A.5, a navigation computer’s data base referred to in paragraph 9A.3 must be current and provided by a person who is an approved supplier for the purposes of paragraph 233 (1) (h) of the Regulations.(a) before each flight, the computer’s database navigation fixes, and the coordinates, frequencies, status (as applicable), and suitability of navigation facilities, required for the intended route must be verified by approved sources of navigation information other than the navigation computer database itself; and(c) despite paragraph 9A.5, an RNAV departure, arrival or approach procedure must not be used if it is one that has been changed in the latest AIRAC cycle and the aircraft’s navigation computer database is not current for the change; and(d) if an aircraft is to commence, or continue, a flight with a navigation computer database that is not current for the AIRAC cycle, the operator or the pilot in command must advise air traffic control before the flight commences, or on first contact during continued flight.9A.11 In the case of a single pilot operation, manually entered data in a navigation computer must be checked against other aeronautical information, such as current maps and charts carried in the aircraft in accordance with paragraph 233 (1) (h) of the Regulations. document RTCA/DO-260A titled Minimum Operational Performance Standards for 1090 MHz Automatic Dependent Surveillance – Broadcast (ADS-B) and Traffic Information Services – Broadcast (TIS‑B), dated 10 April 2003.
3A.6 Subject to paragraph 3A.7, an Australian registered aircraft may be operated without compliance with the flight and navigation equipment requirements in subsections 3 and 4 of this Order if it can show compliance with an equivalent level of safety, as determined by the type certificating authority for the aircraft, taking into consideration its intended operation.(e) in the case of single pilot regular public transport operations, earphones for the pilot with boom or throat microphone and a press to transmit control on the control column.
means the Aeronautical Information Regulation And Control cycle, in accordance with Annex 15, Aeronautical Information Services (AIS), of the Chicago Convention, which documents and defines a series of common dates, and an associated standard aeronautical information publication procedure, for each Convention State.
9A.3 If particulars of way points and navigation aids that are published in maps and charts required to be carried in the aircraft under paragraph 233 (1) (h) of the Regulations are included in a navigation computer’s data base, then those particulars must be in a form that cannot be modified by the aircraft operator or flight crew members.
9.4 An aeroplane required to be fitted with a ground proximity warning system shall not depart with that equipment unserviceable from an aerodrome where facilities are available to repair or replace the ground proximity warning system and in no case shall an aeroplane be operated with its ground proximity warning system unserviceable for a period exceeding 24 hours from the time the equipment was determined to be unserviceable.
9A.1 This subsection applies in relation to navigation computers in an aircraft for use with an RNAV system or GNSS and sets out CASA’s directions for the purposes of regulation 232A of the Regulations.5.1 An aircraft with a flight compartment windshield may only be operated under the V. 6.7 An aircraft required to be fitted with a flight data recorder system and/or a cockpit voice recorder system may operate with an unserviceable recorder system for a period of 21 days commencing on the day on which the system was determined to be unserviceable providing that: 7.1 Piston engined aircraft and unpressurised turbine engine aircraft operating above 15 000 feet in controlled airspace under Instrument Flight Rules (except night V. C.) shall be equipped with an altitude alerting system.