Section 121.310 14 CFR Ch. I (1-1-19 Edition) have a minimum brightness of at least 160 microlamberts. The color may be reversed if the passenger compartment illumination is essentially the same. On these airplanes, no sign may continue to be used if its luminescence (brightness) decreases to below 100 microlamberts. (c) Lighting for interior emergency exit markings. Except for nontransport category airplanes type certificated after December 31, 1964, each passenger-carrying airplane must have an emergency lighting system, independent of the main lighting system. However, sources of general cabin illumination may be common to both the emergency and the main lighting systems if the power supply to the emergency lighting system is independent of the power supply to the main lighting system. The emergency lighting system must - (1) Illuminate each passenger exit marking and locating sign; (2) Provide enough general lighting in the passenger cabin so that the average illumination when measured at 40inch intervals at seat armrest height, on the centerline of the main passenger aisle, is at least 0.05 foot-candles; and (3) For airplanes type certificated after January 1, 1958, after November 26, 1986, include floor proximity emergency escape path marking which meets the requirements of Section 25.812(e) of this chapter in effect on November 26, 1984. (d) Emergency light operation. Except for lights forming part of emergency lighting subsystems provided in compliance with Section 25.812(h) of this chapter (as prescribed in paragraph (h) of this section) that serve no more than one assist means, are independent of the airplane-s main emergency lighting systems, and are automatically activated when the assist means is deployed, each light required by paragraphs (c) and (h) of this section must comply with the following: (1) Each light must - (i) Be operable manually both from the flightcrew station and, for airplanes on which a flight attendant is required, from a point in the passenger compartment that is readily accessible to a normal flight attendant seat; (ii) Have a means to prevent inadvertent operation of the manual controls; and (iii) When armed or turned on at either station, remain lighted or become lighted upon interruption of the airplane-s normal electric power. (2) Each light must be armed or turned on during taxiing, takeoff, and landing. In showing compliance with this paragraph a transverse vertical separation of the fuselage need not be considered. (3) Each light must provide the required level of illumination for at least 10 minutes at the critical ambient conditions after emergency landing. (4) Each light must have a cockpit control device that has an - on, - - off, - and - armed - position. (e) Emergency exit operating handles. (1) For a passenger-carrying airplane for which the application for the type certificate was filed prior to May 1, 1972, the location of each passenger emergency exit operating handle, and instructions for opening the exit, must be shown by a marking on or near the exit that is readable from a distance of 30 inches. In addition, for each Type I and Type II emergency exit with a locking mechanism released by rotary motion of the handle, the instructions for opening must be shown by - (i) A red arrow with a shaft at least three-fourths inch wide and a head twice the width of the shaft, extending along at least 70Section of arc at a radius approximately equal to three-fourths of the handle length; and (ii) The word - open - in red letters 1 inch high placed horizontally near the head of the arrow. (2) For a passenger-carrying airplane for which the application for the type certificate was filed on or after May 1, 1972, the location of each passenger emergency exit operating handle and instructions for opening the exit must be shown in accordance with the requirements under which the airplane was type certificated. On these airplanes, no operating handle or operating handle cover may continue to be used if its luminescence (brightness) decreases to below 100 microlamberts. (f) Emergency exit access. Access to emergency exits must be provided as 108 VerDate Sep<11>2014 08:20 May 17, 2019 Jkt 247048 PO 00000 Frm 00118 Fmt 8010 Sfmt 8010 Y:\SGML\247048.XXX 247048