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1 Whenever the first inspection of a repair has to be done at a given threshold equal to 60 000 Flight Cycles / 75 000 Flight Hours with the information 'TBD' for Interval and Method, this threshold value can be considered equivalent to 46 875 Flight Cycles / 100 000 Flight Hours for Aircraft after Modification 37734K11572 (Service Bulletin List 00-1198). This is applicable to the A320-200 Weight Variant: 000, 001, 002, 003, 004, 005, 006, 007, 008, 009, 010 and 013.
2 Airbus is in the process of removing any reference to maintenance check intervals from the SRM. Until this is complete the statement below should be applied to all temporary Allowable Damage Limits and Repairs that reference maintenance checks. Temporary Allowable Damage Limits and Repairs are justified for a limited number of flight cycles, flight hours or calender time. When limits are given in maintenance "letter" check intervals associated with FC, FH or calender time, the airworthiness limit is the one given in FC, FH or calendar time, the "maintenance" check being only a recommendation associated with that airworthiness limit.
3 When modification or service bulletin differences are extensive and the preceding method of reflecting effectivity becomes cumbersome, thus distracting from the continuity of subject matter, additional data sections are established. These additional data sections are further identified by the introduction of a configuration code (CONFIG-1, CONFIG-2, etc...) following the Chapter/Section/Subsection. Configuration codes are always in ascending, sequential numerical order, i.e., CONFIG-1, CONFIG-2, CONFIG-3, etc...
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云翊航空/11-12月执照和机型培训计划
A320驾驶舱面板指南【01】
M9题库
天津鸿图春季特惠班火热招生ing
发表于 2016-12-29 10:49:13
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