作者kaichun1216 (异乡游子)
看板Aviation
标题Re: [问题]空中的速度..跟地面的速度..有不同吗?
时间Tue Jan 9 23:56:50 2007
※ 引述《svuper (mika)》之铭言:
: --------------------------------------------------
: 之前有看过网路上的文章,刚刚搜寻了一下
: 这架747-sp在空中,4号发动机在2月15到2月19的4天中
: 发动机总共熄火了3次
: 2/15 在FL410熄火 降到FL300重新启动
: 2/18 在FL430熄火 降到FL280重新启动
: 2/19 在FL410熄火 失控掉到9000ft
: 所以高度一掉就是3万2千英尺 = =
: 飞机机尾的水平安定面左右都断了一部份
: 我想如果是我可能在机上吓到失禁了吧0rz
以下摘录自NTSB调查报告,严格来说NTSB并不认为发生事故当天四号发动机是熄火
3.1 Finding
1. The flightcrew was properly certificated and qualified.
2. The Changing airspeeds encountered by Flight 006 and the resultant
compensating throttle adjustments were caused by wind speed variations.
3. The No.4 engine did not flame out, but "hung" at about 1.0 EPR.
4. During his attempt to recover the No.4 engine, the flight engineer did
not close the bleed air valve switch before advancing the No. 4 throttle.
5. The other three engines did not lose thrust nor did they flame out.
6. The captain did not disengage the autopilot in a timely manner after
thrust was lost on the No.4 engine. The autopilot effectively masked
the approaching onset of the loss of the airplane.
7. The captain was distracted from his flight monitoring duties by his
participation with the flight engineer in the evaluation of the No.4
engine's malfunction.
8. With the exception of the loss of thrust on the No.4 engine, no other
airplane malfunction affcted the performance of the airplane; the loss
of thrust on the No.4 engine did not contribute to the accident.
9. The captain was also distracted by his attempts to arrest the airplane's
decreasing airspeed, and this also contributed to his failure to detect the
airplane's increasing bank angle.
10. The lateral control deflections required to maintain level flight under
conditions of thrust asymmetry and decreasing airspeed exceeded the
limits of the autopilot's lateral control authority, causing the airplane to
roll and yaw to the right. The captain lost control of the airplane when,
after disengaging the autopilot, he failed to make the proper flight control
corrections to recover the airplane.
11. The damage to the airplane was a result of the acceleration forces and
high airspeeds that occured during the upset and recovery maneuvers.
3.2 Probable Cause
The National Transportation Safety Board determines that the probable cause
of this accident was the captain's preoccupation with an inflight malfunction
and his failure to monitor properly the airplane's flight instruments which
resulted in his losing control of the airplane.
Contributing to the accident was the captain's over-reliance on the autopilot
after the loss of thrust on the No.4 engine.
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※ 发信站: 批踢踢实业坊(ptt.cc)
◆ From: 71.237.67.217
※ 编辑: kaichun1216 来自: 71.237.67.217 (01/09 23:58)
1F:推 svuper:的确,但报告前段也有说到,FE在一开始动过油门...但仪表 01/10 00:25
2F:推 svuper:却显示这影情没有反应,epr维持在1.0 故FE判定4号熄火 01/10 00:28
3F:推 kaichun1216:这场意外的重点并不在发动机熄火不熄火,而是飞行组员 01/10 00:33
4F:→ kaichun1216:後续处理程序不当才造成飞机急降 01/10 00:34