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Version Superseded: 25/08/2016
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117.—(1) This article applies to [F2A to A commercial air transport aeroplanes], public transport aeroplanes and public transport helicopters registered in the United Kingdom.
(2) Subject to paragraph (5), whenever an aeroplane or helicopter to which this article applies is carrying passengers, every exit from the aeroplane or helicopter and every internal door in the aeroplane or helicopter must be in working order.
(3) Subject to paragraph (4), during take-off and landing and during any emergency, every exit and door in the aeroplane or helicopter must be kept free of obstruction and must not be fastened by locking or otherwise so as to prevent, hinder or delay its use by passengers.
(4) In the case of—
(a)an exit which, in accordance with arrangements approved by the CAA either generally or in relation to a class of aeroplane or helicopter or a particular aeroplane or helicopter, is not required for use by passengers, the exit may be obstructed by cargo;
(b)a door between the flight crew compartment and any adjacent compartment to which passengers have access, the door may be locked or bolted if the commander of the aeroplane or helicopter so determines, for the purpose of preventing access by passengers to the flight crew compartment;
(c)any internal door which is so placed that it cannot prevent, hinder or delay the exit of passengers from the aeroplane or helicopter in an emergency if it is not in working order, paragraph (3) does not apply.
(5) Subject to compliance with paragraph (6), if one, but not more than one, exit from an aeroplane or helicopter becomes inoperative at a place where it is not reasonably practicable for it to be repaired or replaced, nothing in this article prevents that aeroplane or helicopter from carrying passengers until it next lands at a place where the exit can be repaired or replaced.
(6) This paragraph is complied with if—
(a)the number of passengers carried and the position of the seats which they occupy are in accordance with arrangements approved by the CAA either in relation to the particular aeroplane or helicopter or to a class of aeroplane or helicopter; and
(b)in accordance with arrangements so approved, the inoperative exit is fastened by locking or otherwise, the words ‘exit’ or ‘emergency exit’ are covered, and the exit is marked by a red disc at least 23 centimetres in diameter with a horizontal white bar across it bearing the words ‘No Exit’ in red letters.
Textual Amendments
F1Words in art. 117 heading substituted (10.1.2015) by The Air Navigation (Amendment) (No. 4) Order 2014 (S.I. 2014/3302), arts. 1(1), 31
F2Words in art. 117(1) substituted (10.1.2015) by The Air Navigation (Amendment) (No. 4) Order 2014 (S.I. 2014/3302), arts. 1(1), 31
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