Text in force at 25-153: from 25-40, effective 2 May 1977.
(a) Fire extinguishing agents must--
(1) Be capable of extinguishing flame emanating from any burning of fluids or other combustible materials in the area protected by the fire extinguishing system; and
(2) Have thermal stability over the temperature range likely to be experienced in the compartment in which they are stored.
(b) If [any] toxic extinguishing agent is used, provisions must be made to prevent harmful concentrations of fluid of fluid vapors (from leakage during normal operation of the airplane or as a result of discharging the fire extinguisher on the ground or in flight) from entering any personnel compartment, even though a defect may exist in the extinguishing system. This must be shown by test except for built-in carbon dioxide fuselage compartment fire extinguishing systems for which--
(1) Five pounds or less of carbon dioxide will be discharged, under established fire control procedures, into any fuselage compartment; or
(2) There is protective breathing equipment for each flight crewmember on flight deck duty.
[(c) [Deleted]]
42 FR 15044 · Source