Results for disconnecting translation from French to English

the method may also include connecting the communication link to a second destination; requesting a response from the second destination; and disconnecting the communication link to the second destination if the response from the second destination is not valid.
the method may also include connecting the communication link to a second destination; requesting a response from the second destination; and disconnecting the communication link to the second destination if the response from the second destination is not valid.

(5) each nickel cadmium battery installation shall have provisions to prevent any hazardous effect on structure or essential systems that may be caused by the maximum amount of heat the battery can generate during a short circuit of the battery or of individual cells.(amended 2004/07/16; previous version) (6) nickel cadmium battery installations shall have: (amended 2004/07/16; previous version) (i) a system to control the charging rate of the battery automatically so as to prevent battery overheating; or (ii) a battery temperature sensing and over-temperature warning system with a means for disconnecting the battery from its charging source in the event of an overtemperature condition; or (iii) a battery failure sensing and warning system with a means for disconnecting the battery from its charging source in the event of battery failure.
(b) each drain required by paragraph (a) of this section must: (1) discharge clear of all parts of the aeroplane: (2) have manual or automatic means for positive locking in the closed position; and (3) have a drain valve: (i) that is readily accessible and which can be easily opened and closed; and(ii) that is either located or protected to prevent fuel spillage in the event of a landing with landing gear retracted. 525.1001 fuel jettisoning system (a) a fuel jettisoning system must be installed on each aeroplane unless it is shown that the aeroplane meets the climb requirements of 525.119 and 525.121(d) at maximum take-off weight, less the actual or computed weight of fuel necessary for a 15 minute flight comprised of a take-off, go-around, and landing at the airport of departure with the aeroplane configuration, speed, power, and thrust the same as that used in meeting the applicable take-off, approach, and landing climb performance requirements of this chapter.