Document ID: chunk:federal_register_of_legislation:F2017C01038:body:0:p11
Version: federal_register_of_legislation:F2017C01038
Segment Type: other
Provision Reference: 
Character Range: 25313–28155

marking and locating sign – non-transport category turbo-propeller
       29.1 If a turbo-propeller powered non-transport category aeroplane was type certificated after 31 December 1964, each passenger emergency exit marking and each locating sign must have white letters 25 mm high on a red background 50 mm high.
       29.2 Each locating sign must be self-illuminated, electrically or otherwise, with a minimum brightness:
(a) on installation of 0.51 cd/m²; and
(b) that does not decrease in service below 0.32 cd/m².
       29.3 The colours mentioned in subsection 29.1 may be reversed for electrically self‑illuminated signs if this will increase the illumination of the exit.

30 Alternative standards — emergency exit marking and locating sign
       If a passenger emergency exit marking or locating sign does not comply with the relevant requirements of subsection 27.1, 28.1 or 29.1, it must be a universal exit symbol that complies with the means of compliance set out in EASA AMC 25.812 (b) (1) and (2) as in force on 19 September 2007.

31 Emergency exit operating handle marking, illumination and instructions
       31.1 For each passenger emergency exit, the following must be conspicuously marked on the interior of the aeroplane:
(a) the location of the operating handle for the exit; and
(b) the opening instructions for the handle, including, if covered, the handle-cover removal instructions.
       31.2 The marking must be:
(a) on, or near, each passenger emergency exit; and
(b) readable from a distance of 762 mm.
       31.3 Each passenger emergency exit operating handle must be:
(a) self-illuminated with a minimum brightness:
 (i) on installation of 0.51 cd/m²; and
 (ii) that does not decrease in service below 0.32 cd/m²; or
(b) conspicuously located and illuminated by the aeroplane's emergency lighting including in conditions of occupant crowding at the exit.
       31.4If the application for the type certificate for a transport category aeroplane was filed before 1 May 1972, for each Type II or larger passenger emergency exit with a locking mechanism released by rotary motion of a handle, the instructions for opening must be shown by:
(a) a red arrow with a shaft at least 19 mm wide and a head twice the width of the shaft, extending along at least 70 degrees of arc at a radius approximately equal to three quarters of the handle length; and
(b) the word OPEN in red capital letters at least 25 mm high on a contrasting background placed horizontally adjacent to the arrowhead to show the open position of the handle.
Subdivision 2.5 Interior emergency lighting, including FPEEPM

32 Application — CASR 90.225 (1) (b) and 90.230 (2) (b)
       The standards set out in this Subdivision apply for paragraphs 90.225 (1) (b) and 90.230 (2) (b) of CASR 1998.

33 Passenger-carrying aeroplanes
       The