Acts Online
GT Shield

Civil Aviation Act, 2009 (Act No. 13 of 2009)

Regulations

Civil Aviation Regulations, 2011

Part 135 : Air Transport Operations - Carriage of less than 20 passengers or cargo

Subpart 5 : Aeroplane Instruments and Equipment

135.05.4 Altitude alerting system

 

(1) A large turbine-engine aeroplane shall only be operated if it is equipped with—

 

(a) an altitude alerting system capable of—
(i) alerting flight deck crew members upon approaching preselected altitude in either ascent or descent in sufficient time to establish level flight at such preselected altitude; and
(ii) alerting flight deck crew members when deviating above or below a preselected altitude by at least an aural signal.

 

(b) a pressure-altitude reporting transponder which operates in accordance with the requirements provided in Par1 and is capable of—
(i) providing pressure-altitude information with a resolution of 25ft, or better from its aeroplane data source; and
(ii) automatically providing information on its airborne or on-ground status of using a Mode S transponder.

 

Note 1: This regulation will improve the effectiveness of airborne collision avoidance systems as well as air traffic services that employ Mode S radar. In particular, tracking processes are significantly enhanced with a resolution of 7.62m (25 ft), or better.

 

Note 2: Mode C replies of transponders always report pressure altitude in 30.50m (100 ft) increments irrespective of the resolution of the data source.

 

[Regulation 135.05.4 substituted by section 22(b) of the Thirty-Third Amendment of the Civil Aviation Regulations, 2026, Notice No. 7844, GG55226, dated 21 August 2026 and shall come into operation upon Publication in the Government Gazette, save for Part 92, which shall come into operation upon the Proclamation by the President of the Civil Aviation Amendment Act, 2021 (Act No. 22 of 2021]