Two tyres burst on left main landing gear.
左主轮两个轮胎爆破。
Evidence of leak on right main landing gear.
右侧主起落架有漏油迹象。
The main landing gears retract into body-side bays, indicating the likely presence of F-22-style side weapon bays ahead of them.
主起落架收入机身一侧的起落架舱，这意味着很可能其前面有类似F-22 的机侧武器舱。
A brief introduction to the study of damage tolerance behaviour of one type of main landing gear structure is given in this paper.
扼要地介绍了对某型主起落架结构的损伤容限特性研究。
We struck approach lighting on take-off, two tyres burst on left main landing gear, we have to dump fuel before returning to land.
起飞时撞进近灯，左起落架两个轮胎爆破，返航着陆前需放油。
This paper deals with the cause of crack appearing on main landing gear axis. It shows that the cracks belong to the grinding ones.
本文对主起落架轴裂纹产生的原因进行了分析，裂纹为磨削裂纹。
The standing of fishing rod on the ground is realized by the structure combining a single main landing leg and a movable landing leg.
采用单根主支腿和活动支腿相结合的结构完成插地站立。
Case studies included the monitoring of the central wing and outer panel jointing area, the upper and lower pivots of main landing gears.
论文以中央翼-外翼连接区域和起落架上枢轴接头等关键部位为例，说明实施监测的方法。
This paper analyses the cracking cause, corrosion condition and anticorrosion measurements of the backaxle of aircraftB757 main landing gear.
本文分析了B757飞机右主起落架后轮轴断裂原因、腐蚀状态及防腐措施。
It is discussed that the method of photoelastic embedment (a kind of new model test method) is applied to experimental stress analysis of aircraft main landing gear.
讨论了用光弹性嵌片法(一种新的模型试验方法)进行飞机主起落架的实验应力分析。
Main landing runway three-six right ILS approach, main departure runway three-six left.
着陆使用跑道三六右盲降进近，主起飞跑道三六左。
The Main Landing Gear wheels have multi-disc carbon brakes using Green hydraulic pressure for normal operation and Yellow hydraulic pressure through an alternate braking system.
主起落架机轮使用多盘碳刹车，正常情况使用绿色液压系统，备用刹车使用黄色液压系统。
The Main Landing Gear wheels have multi-disc carbon brakes using Green hydraulic pressure for normal operation and Yellow hydraulic pressure through an alternate braking system.
主起落架机轮使用多盘碳刹车，正常情况使用绿色液压系统，备用刹车使用黄色液压系统。
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