Replaced L main wheel in postflight, check OK.
航后更换左主轮，检查正常。
Postflight check found L AFT NAV light not on.
航后检查发现左后航行灯不亮。
Postflight check found L main gear exposed threads due wearing.
航后检查发现左主轮磨损见线。
Postflight check found a hydraulic line of L LDG leakage out of limits.
航后检查发现左起落架一液压管漏油超标。
Postflight check found L outboard main wheel exposed threads due punctured.
航后发现左外主轮扎伤见线。
Postflight check found L outboard brake ASSY indicating pin worn out of limits.
航后检查发现左外刹车组件指示销磨损超标。
Postflight found nose gear mirror too low, check found due charging valve csn't lock, leak air.
航后发现前起落架镜面太低，结果发现是充气活门锁不死漏气所致。
Conclusion It provided further evidence that peripheral effector mechanism might play an important role in the genesis of postflight orthostatic intolerance.
结论对飞行后立位耐力降低的外周效应器机制假说提出了新的实验证据。
The mechanism of postflight cardiovascular deconditioning has been considered as an important problem in the field of gravitational physiology that merits paying great attention to.
航天飞行后心血管失调的发生机理及其对抗措施研究对实现新世纪载人航天目标及阐明微重力心血管影响基本规律具有重要的理论与实际意义。
The mechanism of postflight cardiovascular deconditioning has been considered as an important problem in the field of gravitational physiology that merits paying great attention to.
航天飞行后心血管失调的发生机理及其对抗措施研究对实现新世纪载人航天目标及阐明微重力心血管影响基本规律具有重要的理论与实际意义。
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