(1) This regulation applies to a passenger - carrying aeroplane that:
(a) is an aeroplane to which this Subpart applies; and
(b) is required under its type certification basis to have 2 or more emergency exits on each side of the fuselage.
Note: For the definition of type certification basis , see the Dictionary.
(2) However, this regulation does not apply to an aeroplane that:
(a) was in operation before 16 October 1987; and
(b) had an emergency exit configuration installed and approved before 16 October 1987.
(3) The registered operator of an aeroplane to which this regulation applies commits an offence if:
(a) the registered operator:
(i) operates the aeroplane; or
(ii) permits a person to operate the aeroplane; and
(b) the requirement in subregulation (4) is not met while the aeroplane is operating.
(4) The distance between any 2 adjacent emergency exits that lead from the same deck in the aeroplane must be no more than 18.3 m.
(5) For subregulation (4), the distance between 2 adjacent emergency exits is measured between the closest edges of the 2 doors, parallel to the aeroplane's longitudinal axis.
Source FARs section 121.310 modified.
(6) An offence against subregulation (3) is an offence of
strict liability.