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Printed page 34. PDF page 47.
Actuators During the tear down examination, the following components were found to be in the stowed or retracted position: � Flight spoiler actuators � Outboard ground spoiler actuators � Inboard ground spoiler actuators � Trailing edge flap ballscrews � LeadingOpen official document at PDF page 47Aircraft Accident Report: SilkAir Flight MI 185, Boeing B737-300, 9V-TRF
Printed page Unnumbered appendix sheet. PDF page 222.
actuator � Thrust reverser actuators The fact that these actuators were found in the stowed or retracted position does not necessarily suggest that their respective systems were not activated during the descent. If the respective systems remained in the stowedOpen official document at PDF page 222Aircraft Accident Report: SilkAir Flight MI 185, Boeing B737-300, 9V-TRF
Printed page 32. PDF page 35.
Actuators During the tear down examination, the following components were found to be in the stowed or retracted position: � Flight spoiler actuators � Outboard ground spoiler actuators � Inboard ground spoiler actuators � Trailing edge flap ballscrews � LeadingOpen official document at PDF page 35NTSB comments on the draft final report of the SilkAir MI 185 accident
Printed page 45. PDF page 58.
trailing and leading edge flaps, as well as engine thrust reversers indicate retracted or stowed positions of the respective systems. � Examination of the main rudder power control unit (including the servo-valve), the yaw damper modulating piston, the rudder trimOpen official document at PDF page 58Aircraft Accident Report: SilkAir Flight MI 185, Boeing B737-300, 9V-TRF
Printed page Unnumbered appendix sheet. PDF page 136.
Note: Fully retracted Fully Retracted N/A Last Fully retracted 2.5 units correspond to Stowed Fully commanded Airplane Nose down retracted Fully Retracted N/A position Fully retracted Electric Limit Stowed Flap Ballscrew position 2 Fully Last or 7; outboard flap, retracteOpen official document at PDF page 136Aircraft Accident Report: SilkAir Flight MI 185, Boeing B737-300, 9V-TRF
Printed page Unnumbered appendix sheet. PDF page 234.
trailing and leading edge flaps, as well as engine thrust reversers indicate retracted or stowed positions ofthe respective systems. � Examination of the main rudder power control unit (including the servo-valve), the yaw damper modulating piston, the rudder trim actuator,Open official document at PDF page 234Aircraft Accident Report: SilkAir Flight MI 185, Boeing B737-300, 9V-TRF