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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

135.05.16 Emergency locator transmitter

 

(1) No air service operator shall operate an aeroplane under this Part unless such aeroplane is equipped with—
(a) at least one automatic ELT or two ELTs of any type as prescribed in Document SA-CATS 91;
(b) where the aeroplane is of a type for which the individual certificate of airworthiness was first issued after 1 July 2008—
(i) at least two ELTs, one of which shall be automatic; or
(ii) at least one ELT of any type as prescribed in Document SA-CATS 91, provided that the aeroplane has the capability to autonomously transmit information regarding its position at least once every minute when in distress as prescribed in Document SA-CATS 121.

[Regulation 135.05.16(1) substituted by regulation 16(h) of Notice No. R. 432, GG 40846, dated 19 May 2017 (Sixteenth Amendment of the Civil Aviation Regulations, 2017)]

 

(2) ELT equipment carried in terms of subregulation (1) shall operate and be installed as prescribed in technical standard 91.04.26 of SA-CATS 91.

[Regulation 135.05.16(2) substituted by regulation 31 of Notice No. R. 534, GG 36712, dated 30 July 2013 (Third Amendment to the Civil Aviation Regulations, 2013)]

 

(3) ELTs required to be fitted in terms of this regulation, shall be capable of transmitting on the frequencies 121,5 MHz and 406 MHz simultaneously.

 

(4) Notwithstanding subregulations (1) and (2), an aeroplane may be operated without a serviceable ELT where—
(a) it is operated in accordance with a MEL approved by the Director; or
(b) where a MEL has not been approved by the Director in respect of the aeroplane, the operator—
(i) repairs or removes the EL T at the first aerodrome at which repairs or removal can be accomplished;
(ii) on removal of the ELT from the aeroplane, sends the ELT to a maintenance facility;
(iii) displays on a readily visible placard within the aeroplane cockpit, for the period of removal of the ELT from the aeroplane, a notice stating that the ELT has been removed and setting out the date of removal; and
(iv) installs a serviceable ELT within 5 days after the date of removal.