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Beechcraft 1900D (Colgan Air flight 9446)

13.7k AeroflotBilibili  1.4 years ago
Auto Credit Based on MAPA's Air Canada Express - Beechcraft1900D

About Colgan Air flight 9446:

On August 23, 2003, Beech 1900D N240CJ underwent a Detail Six phase maintenance check (aft fuselage / empennage). The phase check was interrupted, and the remaining work was deferred on the morning of August 24. Ten revenue flight legs were completed that day, and the Detail Six phase check resumed on the evening of August 24, and concluded on August 26. During the check both elevator trim actuators were replaced. During this procedure the Aircraft Maintenance Manual (AMM) was not strictly followed and the elevator trim tab cable unwound off the forward drum. The forward elevator trim tab cable was then replaced. During the replacement of the cable, the maintenance personnel skipped a step in the AMM. They did not use a lead wire to assist with cable orientation. In addition, the AMM incorrectly depicted the elevator trim drum, and the depiction of the orientation of the cable around the drum was ambiguous.
On the evening of August 26, N240CJ was to be repositioned to Albany. When the flightcrew received the airplane, the captain did not address the recent cable change noted on his maintenance release. The captain also did not perform a first flight of the day checklist, which included an elevator trim check.
Shortly after takeoff from runway 24 the pitch trim control moved from 1.5 to approximately 3 degrees negative (nose down). Ten seconds later the pitch trim control moved to an approximate 7 degree negative position, where it remained for the duration of the flight. The pilot declared an emergency and reported a "runaway trim." The airplane flew in a left turn and reached an altitude of approximately 1,100 feet. The flightcrew subsequently requested to land on runway 33, upon which ATC cleared the flight to land on any runway. While attempting to return to the airport, the plane then pitched nose-down, and impacted the water at an approximate 30-degree angle. The Beech came to rest in approximately 18 feet of water, about 100 yards from the Yarmouth shore.

PROBABLE CAUSE: "The improper replacement of the forward elevator trim cable, and subsequent inadequate functional check of the maintenance performed, which resulted in a reversal of the elevator trim system and a loss of control in-flight. Factors were the flightcrew's failure to follow the checklist procedures, and the aircraft manufacturer's erroneous depiction of the elevator trim drum in the maintenance manual."

General Characteristics

Performance

  • Horse Power/Weight Ratio 0.171
  • Wing Loading 38.1lbs/ft2 (186.1kg/m2)
  • Wing Area 457.9ft2 (42.5m2)
  • Drag Points 5456

Parts

  • Number of Parts 134
  • Control Surfaces 7
  • Performance Cost 572
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    2003年8月23日,山毛榉1900D N240CJ进行了细节六阶段维护检查(后机身/尾翼)。阶段检查中断,剩余工作推迟到8月24日上午。当天完成了10个航班航段,8月24日晚恢复了“六号细节”阶段检查,8月26日结束。在检查过程中,更换了两个电梯内件执行器。在此过程中,没有严格遵守飞机维护手册 (AMM),升降舵配平片电缆从前滚筒上松开。然后更换了前部电梯配平片电缆。在更换电缆期间,维护人员跳过了AMM中的一个步骤。他们没有使用引线来帮助电缆定向。此外,AMM错误地描绘了电梯配平卷筒,并且对卷筒周围电缆方向的描绘是模糊的。
    8月26日晚,N240CJ将重新定位到奥尔巴尼。当机组人员收到飞机时,机长没有解决最近维护释放中注明的电缆变化。机长也没有执行当天的第一次飞行清单,其中包括电梯配平检查。
    从24号跑道起飞后不久,俯仰配平控制从负1.5度变为约3度(机头朝下)。十秒钟后,俯仰配平控制移动到大约 7 度的负位置,并在飞行期间保持该位置。飞行员宣布进入紧急状态并报告了“失控的修剪”。飞机左转飞行,达到大约1,100英尺的高度。机组人员随后要求降落在33号跑道上,ATC批准该航班降落在任何跑道上。在试图返回机场时,飞机随后俯仰,并以大约30度角撞击水面。山毛榉停在距离雅茅斯海岸约100码的大约18英尺深的水中。

    可能的原因:“前向电梯配平电缆更换不当,随后对所执行的维护功能检查不足,导致电梯配平系统反转并在飞行中失去控制。因素是机组人员未能遵循清单程序,以及飞机制造商在维护手册中对电梯配平鼓的错误描述。

    Pinned 1.4 years ago
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    @Footballbadyee111 对

    1.4 years ago
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    ACI新一季的

    1.4 years ago