Text in force at CAR3R-8: from CAR3R-2, effective 12 Aug 1957. OCR text
shall be applicable to multiengine aircraft which are required to comply with the provisions of 8 3.85(»b). -S- (a) Means for each individual engine shall be provided for shutting off or otherwise preventing hazardous quantities of fuel, oil, de-icer, and other flammable fluids fran flowing into, within, or through the engine compartment except that means need not be provided to shut off flow in lines forming an integral part of an engine, Closing the fuel shutoff valve for any engine shall not make any of the fuel supply unavailable to the remaining engines, (b)_ Operation of the shutoff means shall not interfere with the subsequent emergency operation of other equipment, such as feathering the propeller. (c) The shutoff means shall be located outside of the engine compartment unless an high degree of safety is otherwise provided. It shall be show that no hazardous quantity of flammable fluid could drain into the engine compartment after shutting off has been accomplished, (ad) Provisions shall be made to guard against inadvertent operation of the shutoff means and to make it possible for the crew to reopen the shutoff means in flight after it has once been closed, 19. By adding a new 8 3.638 to read as follows:
secs. 601, 603, 52 Stat. 1007, 1009, as amended; 49 U.S.C. 551, 553) . By the Civil Aeronautics Boards /e/ H.C, Mulligan (SEAL) M,C. Mulligan Fart 3 last printed May 15, 1956. Secretary ·